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⚠ Pending professional review

This course plan, its lessons and its assessments has not yet been verified by a certified examiner or master technician in the trade or by a certification or approval body. It is a study draft and may contain errors. Do not use it as instructions for work on a job site or on live equipment. Always follow your instructor, your supervising professional, and current official references and regulations.

VoTechWorks program approval and accreditation are still in progress. Credentials are issued only by the certifying bodies named in each program, after their own exams.

Aviation Maintenance

8 courses · 3,600 clock hours · 18–24 mo full-time. Grading is competency-based: each course requires the written exam, a competent skills demonstration with zero safety faults, a signed log, and a passed safety audit; percentage weights only rank performance above the competency floor.

~~$66,715~~ COMPLIMENTARYprogram tuition

8courses

67lessons

3,600hours

27assessments

Development progressPlanCourses, lessons and assessments written for this tradeLessons67 of 67 lesson pages writtenPractice534 practice questionsResources118 reference entries (study list)Review0 lesson pages reviewed by a licensed professional

Study now: 67 lesson pages are open (lesson titles below are links).

TRN-AVIA22-01 Universal core

Universal Core: Safety, Math, Communication & Career for Aviation Maintenance

148 hr · ~~$1,185~~ COMPLIMENTARY

This foundational course equips aviation maintenance students with the safety protocols, mathematical skills, technical literacy, and professional habits required throughout the A&P program and on the job. Students earn OSHA 10 recognition and CPR/First Aid certification while building the trade-specific numeracy and documentation skills that underpin every subsequent course. Lessons are mapped to FAA A&P General knowledge areas including safety, ground operation, mathematics, and regulations.

Outcomes

Apply OSHA 10 general industry hazard-recognition principles and aviation-specific safety practices, including lockout/tagout and proper PPE selection, to simulated hangar scenarios.
Perform trade math operations—fractions, decimals, percentages, ratios, basic algebra, area, volume, and unit conversion between US customary and SI units—with at least 80% accuracy on graded problems.
Read, interpret, and extract correct maintenance data from FAA-approved aircraft maintenance manuals, Airworthiness Directives, and illustrated parts catalogs.
Produce legible, complete, and properly signed maintenance record entries using standard aviation abbreviations and required regulatory content.
Demonstrate proficient use of aviation digital tools including electronic logbooks, maintenance tracking software, and authoritative online databases (FAA, manufacturers).
Develop an individualized career plan identifying FAA A&P certification pathways, required experience hours, and at least three local or regional employer targets.

Course text

How the course runs. 7 blocks: Aviation Workplace Safety and OSHA 10; First Aid, CPR, and Aviation Emergency Response; Trade Mathematics for Aviation Maintenance; Technical Reading: Manuals, ADs, and Regulatory Documents; Aviation Maintenance Documentation and Records; Digital Tools and Information Systems for Aviation Maintenance; Career Readiness and FAA Certification Pathways.

What competent looks like. Apply OSHA 10 general industry hazard-recognition principles and aviation-specific safety practices, including lockout/tagout and proper PPE selection, to simulated hangar scenarios. Perform trade math operations—fractions, decimals, percentages, ratios, basic algebra, area, volume, and unit conversion between US customary and SI units—with at least 80% accuracy on graded problems. Read, interpret, and extract correct maintenance data from FAA-approved aircraft maintenance manuals, Airworthiness Directives, and illustrated parts catalogs. Produce legible, complete, and properly signed maintenance record entries using standard aviation abbreviations and required regulatory content. Demonstrate proficient use of aviation digital tools including electronic logbooks, maintenance tracking software, and authoritative online databases (FAA, manufacturers). Develop an individualized career plan identifying FAA A&P certification pathways, required experience hours, and at least three local or regional employer targets.

Lessons · 7 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Aviation Workplace Safety and OSHA 10	26	theory	Students will identify and correctly respond to the major OSHA general industry hazard categories present in aviation maintenance facilities, including chemical, electrical, fall, and noise hazards, and will complete the OSHA 10 card requirement.	Complete the OSHA 10 General Industry online or instructor-led modules, taking the end-of-section quizzes and receiving the completion card upon passing all segments. Walk a simulated hangar bay and complete a written Job Hazard Analysis (JHA) form, identifying at least eight distinct hazards, their risk level, and the corresponding control measure (elimination, PPE, procedure). Practice lockout/tagout (LOTO) procedure on a de-energized ground support unit mock-up: affix personal lock, verify zero energy, complete the LOTO log entry, and restore the unit under instructor observation.	OSHA 10 General Industry course materials, OSHA 29 CFR 1910 reference summaries, blank JHA forms, LOTO kit (personal locks, tags, hasp), simulated aircraft ground power unit, FAA Advisory Circular AC 00-34 (Aircraft Ground Handling and Servicing) for context	Verified OSHA 10 completion card plus 80% score on instructor-written hazard-identification quiz (20 items); LOTO practical checked against a signed competency checklist—all five critical steps must be performed correctly to pass.
2	First Aid, CPR, and Aviation Emergency Response	16	lab	Students will demonstrate hands-only and full CPR/AED sequences and bleeding control techniques to American Heart Association or Red Cross standard, earning a recognized CPR/First Aid card.	Complete an accredited CPR, AED, and First Aid course (classroom or blended); practice adult and child CPR cycles on manikins until achieving correct compression depth and rate verified by the AED trainer unit's feedback. Practice severe-bleeding control using tourniquet application and wound-packing technique on simulated wound trainers, timing application to within two minutes. Role-play an aviation hangar emergency scenario: a coworker is unresponsive near a running APU—students activate EMS, manage bystanders, retrieve the AED, and complete a full response cycle while an instructor records decision points on a skills checklist.	CPR manikins (adult and child), AED trainer, tourniquet trainers, wound-packing simulators, gloves and face shields, American Heart Association or Red Cross provider guide, scenario script	Valid CPR/First Aid card issued by an accredited provider (100% required—no partial credit); scenario skills checklist scored by instructor with all critical steps marked satisfactory to pass.
3	Trade Mathematics for Aviation Maintenance	30	practice	Students will solve aviation maintenance math problems—including fractions, decimals, percentages, ratio and proportion, basic algebra, area, volume, and metric/US unit conversions—with 80% or greater accuracy, mirroring the math content tested on the FAA A&P General written exam.	Work through a graded problem set of 40 items drawn from FAA A&P General knowledge area categories: perform arithmetic on mixed-number torque specifications, calculate fuel volume in gallons and liters, and convert between inch-pound and Newton-meter torque values. Use a manual and a scientific calculator to solve three realistic word problems: determine the correct drill size for a rivet hole given a fraction-inch specification, compute the total surface area of a control surface requiring sealant, and find an unknown resistance value in a simple series circuit using Ohm's Law. Play a timed peer-competition card game (instructor-prepared 'Wrench Math' flash cards) covering 60 mixed question types; students record wrong answers and rework them independently before the next class session.	Scientific calculator, FAA-H-8083-30 Aviation Maintenance Technician Handbook – General (Chapter 1, Mathematics), instructor-prepared problem sets, conversion reference card, graph paper	Two graded problem sets (40 items each) averaged together; minimum 80% to pass; any student below 80% on the first set receives one remediation session before the second set.
4	Technical Reading: Manuals, ADs, and Regulatory Documents	24	theory	Students will correctly locate, read, and extract required maintenance data from an FAA-approved Aircraft Maintenance Manual (AMM), an Airworthiness Directive (AD), and an Illustrated Parts Catalog (IPC), demonstrating understanding of document hierarchy and legal authority.	Given a printed or PDF AMM chapter, answer a 15-question instructor worksheet requiring students to locate the correct task card, identify the tools listed, record the torque specification, and state the interval for an inspection item. Retrieve and read two actual ADs (one airframe, one engine) from the FAA AD database; for each, complete a one-page summary identifying the subject aircraft, reason for the AD, required action, compliance time, and method of compliance. Compare a manufacturer's Service Bulletin to the corresponding AD, and in a brief written paragraph explain the regulatory difference between a mandatory AD and a recommended service bulletin—include which document governs and why.	Printed AMM excerpt (training aircraft or FAA sample), FAA Airworthiness Directive database access (rgl.faa.gov), IPC excerpt, FAA Order 8900.1 excerpts on maintenance records, instructor worksheet, laptops or tablets	Completed AMM worksheet scored against instructor answer key (80% minimum); AD summaries checked for all five required elements—both must contain all five elements for a passing grade.
5	Aviation Maintenance Documentation and Records	20	practice	Students will compose legally sufficient aircraft maintenance record entries, return-to-service statements, and discrepancy write-ups using correct regulatory language, standard abbreviations, and required signatures, meeting the content standard referenced in 14 CFR Part 43.	Review sample compliant and non-compliant logbook entries side by side; in pairs, identify and list every deficiency in each non-compliant entry, then rewrite it correctly. Write three original maintenance record entries from scenario cards (oil change, replaced landing light, 100-hour inspection sign-off), ensuring each entry includes date, aircraft description, work performed, reference to the applicable maintenance manual, and the technician's signature and certificate number field. Role-play a maintenance release scenario: student presents a completed record to the 'inspector' (instructor) who asks clarifying questions; student defends each entry element and corrects any flagged items on the spot.	14 CFR Part 43 Appendix B (maintenance record entries) printed reference, sample logbook pages (compliant and non-compliant sets), scenario cards, blank paper logbook forms, black pens	Three written entries scored on a rubric (5 required elements each = 15 total points); minimum 12/15 (80%) and zero safety-critical omissions to pass; entries with missing return-to-service language are automatic resubmit.
6	Digital Tools and Information Systems for Aviation Maintenance	16	demo	Students will navigate FAA regulatory databases, manufacturer digital maintenance platforms, and a representative electronic maintenance tracking system to locate required data and enter a simulated work order accurately.	Follow a step-by-step instructor demonstration of the FAA Dynamic Regulatory System (DRS) and rgl.faa.gov; then independently locate a specific regulation, a current AD, and an approved Supplemental Type Certificate (STC) using only a task card with the required item descriptions. Log into a demonstration instance of an electronic maintenance management system (such as a training version of a common MRO platform); enter a simulated work order including aircraft tail number, discrepancy description, corrective action, part number, and technician ID, then print the completed work order. Evaluate three aviation information websites for reliability using an instructor-provided checklist covering source authority, publication date, and regulatory backing; present a one-paragraph written finding on which sources are acceptable for maintenance decision-making and why.	Laptops or tablets with internet access, FAA website bookmarks (rgl.faa.gov, FAA DRS), demo MRO software credentials, instructor task cards, source-evaluation checklist	Correct retrieval of all three items on the FAA database task card (all three required to pass); completed work order checked against answer key with all required fields populated and no safety-critical data errors.
7	Career Readiness and FAA Certification Pathways	16	field	Students will construct an individualized career development plan that correctly describes FAA A&P certification eligibility requirements, maps their program hours to those requirements, and identifies concrete next steps including at least three employer targets.	Participate in a panel discussion with two or three invited local A&P mechanics and one avionics technician; prepare and ask at least two written questions beforehand, then write a one-page reflection summarizing career insights and how the guest experience affects their personal plan. Complete a resume and cover letter tailored to an entry-level aviation maintenance position posting; submit for instructor feedback and revise at least once based on written comments. Produce a one-to-two-page Career Development Plan (CDP) that includes: (a) a table mapping program course hours to FAA 14 CFR Part 65 experience requirements, (b) the FAA FSDO nearest to the student's intended work location, (c) three potential employer contacts with rationale, and (d) a 24-month milestone timeline from program start to sitting the A&P written exams.	14 CFR Part 65 Subpart D printed reference, FAA FSDO directory, sample resume template, guest speaker bios, internet access for employer research, CDP template	CDP scored on a four-criterion rubric (regulatory accuracy, completeness, employer research quality, timeline realism); minimum 3 out of 4 criteria rated satisfactory AND resume accepted by instructor after at most one revision cycle.

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Safety and Regulatory Knowledge Exam	Written exam	25%	80% (32/40 items correct)	A 40-item multiple-choice exam covering OSHA hazard categories, LOTO procedures, PPE selection, first-aid decision-making, and aviation workplace safety regulations drawn from lesson content and FAA A&P General knowledge areas. Students must achieve 80% or better; those who do not pass may attempt one retake after a documented remediation session. Accuracy · Safety · Communication · Professionalism
Trade Math and Technical Reading Exam	Written exam	25%	80% (32/40 items correct)	A 40-item exam combining 25 math computation problems (fractions, unit conversions, area, volume, basic algebra at aviation maintenance level) and 15 reading-comprehension questions requiring students to extract data from a provided AMM excerpt and an AD. A minimum score of 80% is required; calculation work must be shown for partial-credit consideration on math items. Accuracy · Safety · Communication · Professionalism
Maintenance Record Documentation Project	Project	25%	Minimum 80% on rubric AND zero safety-critical omissions	Students receive a scenario packet describing three completed maintenance tasks and must produce a compliant logbook entry, a proper return-to-service statement, and a discrepancy write-up for each task. Entries are scored on a rubric covering regulatory content, correct use of required fields, legibility, and use of standard abbreviations; any entry missing a legally required element (date, description, reference, or authorization) must be corrected and resubmitted before a final grade is assigned. Accuracy · Safety · Communication · Professionalism
Career Plan Oral Defense	Oral / panel	25%	Satisfactory rating on all three rubric domains	Each student presents their Career Development Plan in a 10-minute oral defense before a two-person panel (lead instructor and one industry advisor or program coordinator), followed by five minutes of questions. The panel evaluates regulatory knowledge accuracy (correct citation of FAA experience requirements), professional communication quality, and the realism and specificity of the career timeline; all three domains must receive a satisfactory rating for the student to pass the course. Accuracy · Safety · Communication · Professionalism

TRN-AVIA22-02 Trade course

Airframe Systems and Structures

548 hr · ~~$14,205~~ COMPLIMENTARY

This course covers the theory, inspection, repair, and maintenance of aircraft airframe structures and systems as defined by FAA Title 14 CFR Part 65 Airframe knowledge and skill requirements. Students work on representative aircraft and components to develop the hands-on proficiency required for the FAA Airframe written, oral, and practical tests. Emphasis is placed on airworthiness standards, proper documentation, and safe shop practices throughout every task.

Outcomes

Inspect, repair, and approve aircraft wood, fabric, metal, composite, and welded structures using FAA-accepted methods and materials to airworthy standards.
Service, troubleshoot, and return to service aircraft hydraulic, pneumatic, landing gear, fuel, environmental, and flight-control systems following manufacturer and regulatory requirements.
Read and apply aircraft maintenance manuals, structural repair manuals, Airworthiness Directives, and FAA advisory circulars to plan and document airframe maintenance tasks.
Perform required inspections and complete maintenance records, logbook entries, and FAA Form 337s accurately and in compliance with 14 CFR Part 43.
Identify and apply correct personal protective equipment, lockout/tagout procedures, and hazardous-material controls for all airframe shop and field tasks.
Demonstrate the oral and practical skill proficiency required to pass the FAA Airframe practical test in each system area.

Course text

How the course runs. 12 blocks: Airframe Shop Safety and Regulatory Foundation; Aircraft Structures: Wood and Fabric; Sheet Metal Structures: Theory and Layout; Sheet Metal Fabrication and Riveting; Welding Identification and Composite Structures; Aircraft Landing Gear Systems; Hydraulic and Pneumatic Systems; Fuel Systems; Environmental and Pressurization Systems; Flight Control Systems; Aircraft Inspections, Airworthiness, and Documentation; Airframe Systems Integration and FAA Practical Test Readiness.

What competent looks like. Inspect, repair, and approve aircraft wood, fabric, metal, composite, and welded structures using FAA-accepted methods and materials to airworthy standards. Service, troubleshoot, and return to service aircraft hydraulic, pneumatic, landing gear, fuel, environmental, and flight-control systems following manufacturer and regulatory requirements. Read and apply aircraft maintenance manuals, structural repair manuals, Airworthiness Directives, and FAA advisory circulars to plan and document airframe maintenance tasks. Perform required inspections and complete maintenance records, logbook entries, and FAA Form 337s accurately and in compliance with 14 CFR Part 43. Identify and apply correct personal protective equipment, lockout/tagout procedures, and hazardous-material controls for all airframe shop and field tasks. Demonstrate the oral and practical skill proficiency required to pass the FAA Airframe practical test in each system area.

Lessons · 12 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Airframe Shop Safety and Regulatory Foundation	32	theory	Students will identify applicable safety standards, PPE requirements, lockout/tagout procedures, and the FAA regulatory framework governing airframe maintenance before touching any aircraft component.	Complete OSHA General Industry hazard identification walkthrough of the airframe shop, tagging each identified hazard with the controlling standard (OSHA 1910 or 1926 as applicable) on a shop-floor map worksheet. Demonstrate a full lockout/tagout sequence on a simulated hydraulic test bench—apply energy-isolation devices, verify zero energy state, and restore the system—while an instructor evaluates each step against a written checklist. Research one current Airworthiness Directive relevant to a training aircraft in the shop, summarize its applicability, compliance method, and required logbook entry, and present a two-minute verbal summary to the class.	OSHA 29 CFR 1910 and 1926 standards, 14 CFR Parts 21, 39, 43, 65, 91; FAA Advisory Circular AC 43.13-1B and -2B; school lockout/tagout kit; shop PPE station (safety glasses, hearing protection, nitrile gloves, chemical-resistant gloves, respirator); shop training aircraft	Written safety quiz covering PPE selection, lockout/tagout steps, and regulatory hierarchy—minimum passing score 75%; lockout/tagout performance checklist—all critical steps must be marked satisfactory
2	Aircraft Structures: Wood and Fabric	40	lab	Students will inspect, repair, and fabric-cover a representative wooden airframe component using FAA-accepted techniques and materials per AC 43.13-1B chapters on wood and fabric.	Inspect a wood wing rib sample for moisture damage, delamination, compression failures, and glue-joint integrity using AC 43.13-1B acceptance criteria; record findings on a standardized inspection form. Fabricate a scarf-joint splice repair on a damaged spruce spar section, select correct adhesive, apply proper clamping pressure per manufacturer data, and cure the assembly; measure finished dimensions against tolerance. Apply a two-bay fabric patch on a practice panel using heat-shrink fabric—clean, prime, attach, shrink, brush two coats of dope, and check tautness with a fabric tensiometer—recording each step on a maintenance work order.	Spruce spar stock, aircraft-grade plywood, urea or resorcinol adhesive, heat-shrink polyester fabric, nitrate and butyrate dope, fabric tensiometer, dope brush set, AC 43.13-1B, steel rule, calipers, C-clamps, respirator with organic-vapor cartridges	Completed inspection form with correct go/no-go decisions verified by instructor; scarf joint meets dimensional tolerance within 1/32 in and passes visual delamination check; fabric patch exhibits correct tautness per tensiometer reading and shows no bubbles, wrinkles, or lifting—rated satisfactory/unsatisfactory by instructor
3	Sheet Metal Structures: Theory and Layout	44	theory	Students will calculate bend allowance, setback, and flat-pattern layout for aircraft-grade aluminum parts and identify rivet types, sizes, and spacing rules before performing any forming or riveting operations.	Given three part drawings with specified bend radii and material thickness, calculate bend allowance and setback using the K-factor formula and verify results against the sheet metal calculator; check answers with the instructor before proceeding. Identify 12 rivet samples by head style, material, and designation (MS and AN number systems) using FAA reference charts; record identifications on a datasheet and self-check against answer key. Lay out a flat-pattern development for a Z-channel bracket on 0.040-in 2024-T3 sheet using scribers and combination squares, then verify layout dimensions against the drawing before any cutting occurs.	Aircraft sheet metal textbook, AC 43.13-1B Chapter 4, rivet identification sample set, 2024-T3 aluminum sheet stock, combination square, scriber, sheet metal calculator, rivet spacing charts, part drawings	Bend-allowance and setback calculations within 0.005 in of instructor answer key; all 12 rivet IDs correct (minimum 10 of 12 to pass); flat-pattern layout dimensions within 1/32 in of drawing—instructor verifies before material is cut
4	Sheet Metal Fabrication and Riveting	56	lab	Students will fabricate a multi-piece aluminum assembly using hand-formed bends, drilled and countersunk holes, and driven solid rivets that meet aircraft airworthiness acceptance criteria.	Form the Z-channel bracket laid out in Lesson 3 using a cornice brake; check flange angles with a protractor and bend radius with a radius gauge, correcting any springback before moving to hole layout. Drill, ream, and countersink a 20-hole pattern in the assembly, cleco-clamp mating parts, then drive AN426 flush rivets to correct shop-head dimensions and check each rivet with a rivet gauge for head diameter and height. Inspect the completed assembly for cracks, improper driven-head dimensions, sheet waviness, and edge distance using AC 43.13-1B criteria; classify each discrepancy as acceptable, repairable, or reject, and record results on an inspection record.	Cornice brake, drill press, pneumatic rivet gun, bucking bars, cleco clamps, AN426 flush rivets, 2024-T3 sheet stock, rivet gauge, protractor, radius gauge, countersink cage, deburring tool, AC 43.13-1B	All shop-head dimensions within AN tolerance (checked with rivet gauge); no cracks at holes; edge distance and pitch meet AC 43.13-1B minimums; instructor rates the assembly satisfactory/unsatisfactory on a 10-point criteria checklist—minimum 8 of 10 criteria satisfactory
5	Welding Identification and Composite Structures	44	demo	Students will identify weld types, evaluate weld quality against visual acceptance criteria, and perform a wet layup composite repair on a representative fiberglass or carbon-fiber panel following a structural repair manual procedure.	Examine 10 welded 4130 steel tube joint samples; classify each as acceptable, defective (identify specific defect—porosity, undercut, crack, incomplete fusion), or rejectable using AC 43.13-1B weld criteria and record decisions on an inspection sheet. Watch an instructor demonstration of oxy-acetylene and TIG welding on 4130 steel coupons; identify flame types, filler selection, and safety controls (fire blankets, ventilation, flash shield use), then record observations in a lab notebook. Perform a two-ply wet layup fiberglass repair on a pre-damaged training panel following the shop SRM procedure—cut plies on bias, wet-out cloth, apply, vacuum-bag, and cure; record cure temperature and time on the work order.	4130 chromoly weld sample set, AC 43.13-1B, oxy-acetylene and TIG welding equipment, fire blanket, welding curtain, face shield, fiberglass cloth, epoxy resin and hardener, peel ply, vacuum bag film, breather cloth, vacuum pump, digital thermometer, SRM excerpt	Weld inspection sheet—minimum 8 of 10 correct classifications; lab notebook observation entries complete and accurate as verified by instructor; cured composite panel shows no dry spots, delamination, or voids on visual and tap-test inspection—satisfactory/unsatisfactory rating by instructor
6	Aircraft Landing Gear Systems	48	lab	Students will inspect, service, and operationally test a retractable landing gear system—including hydraulic actuators, up/down locks, and position-indicating switches—and complete a logbook entry for the task.	Perform a landing gear retraction test on the training aircraft or full-scale trainer using the manufacturer's functional test procedure; observe sequencing, door clearances, and indicator light operation, and record all measurements and observations on the work order. Remove, inspect, and reinstall an oleo-pneumatic strut; check strut extension, fluid level, and nitrogen servicing per the aircraft maintenance manual; compare measured values to AMM limits and annotate the service sheet. Complete a simulated FAA-format maintenance logbook entry for the landing gear inspection task, including aircraft make/model/serial, date, description of work, reference to manual, part numbers, and the required regulatory return-to-service statement.	Training aircraft or landing gear functional trainer, aircraft maintenance manual, hydraulic service cart, nitrogen servicing cart, strut extension gauge, drip pan, torque wrench set, logbook entry form (FAA format), PPE (safety glasses, nitrile gloves)	All AMM functional test steps completed in sequence with correct measurements recorded; strut extension and fluid level within AMM limits; logbook entry includes all required elements per 14 CFR Part 43—instructor rates entry complete/incomplete; minimum satisfactory on all three activities
7	Hydraulic and Pneumatic Systems	48	lab	Students will troubleshoot, bleed, and service a representative aircraft hydraulic system, interpret a hydraulic schematic, and identify component functions and failure modes to airworthy standards.	Trace a hydraulic schematic for a training system; label each component (pump, reservoir, actuator, check valve, relief valve, selector valve, filter) and draw fluid flow paths for gear-down and gear-up cycles in different colors on a printed schematic worksheet. Using an injected fault (simulated external leak, introduced by instructor), connect a hydraulic test stand to a training rig, pressurize the system to operating pressure, locate the leak source using UV dye and inspection light, and depressurize before repair. Bleed a brake system using the pressure-bleeding method per AMM procedure; verify pedal feel, check fluid level, and inspect caliper and line fittings for leaks; record fluid type, quantity added, and test results on the service record.	Hydraulic training rig, hydraulic test stand, aircraft-grade hydraulic fluid (correct specification for training rig), UV dye kit, brake pressure bleeder, torque wrench, schematic worksheet, AMM excerpt, drip pan, nitrile gloves, safety glasses	Schematic labeling 100% correct (instructor key); fault located and correctly identified before any repair; bleed procedure completed per AMM with no residual leaks; instructor rates each activity satisfactory/unsatisfactory—minimum satisfactory on all three
8	Fuel Systems	44	lab	Students will inspect, service, and operationally check a representative aircraft fuel system—including tanks, vents, sumps, selectors, and boost pumps—and identify fuel contamination and airworthiness hazards.	Drain and inspect fuel tank sumps and strainer for water and sediment contamination using a clear container and color-comparison card; record fuel color, odor, sample quantity, and pass/fail determination for each sump on a fuel-sampling log. Perform a fuel system operational check—activate boost pump, verify fuel-quantity indication, operate fuel selector through all positions, and check for leaks at connections and fittings per AMM procedure; annotate every step on the work order. Given a scenario card describing fuel contamination (wrong fuel grade introduced), apply the AMM and aircraft POH defueling and decontamination procedure, including required bonding and grounding steps, fire extinguisher placement, and proper fuel disposal documentation.	Training aircraft or fuel system trainer, aircraft AMM, POH excerpt, fuel sampling containers, color-comparison card, fuel sampling log forms, bonding cable and reel, portable fire extinguisher, drip pans, nitrile gloves, work order forms	Fuel sample log correctly completed with accurate pass/fail determinations; operational check worksheet complete with no missed steps; contamination scenario: all bonding/grounding steps performed in correct order, fire extinguisher positioned, disposal documented—rated satisfactory/unsatisfactory by instructor
9	Environmental and Pressurization Systems	40	theory	Students will explain the operating principles of aircraft heating, ventilation, pressurization, oxygen, and ice-protection systems and identify inspection, servicing, and safety requirements for each.	Using a cutaway diagram of a turbine-powered cabin-pressurization system, trace bleed-air flow from engine to outflow valve and label all components; calculate cabin altitude for a given differential pressure value using the standard formula and check with instructor. Research and present to a small group the servicing requirements for one type of aircraft oxygen system (gaseous high-pressure), including cylinder hydrostatic test interval, charging procedure, contamination hazards, and applicable regulations. Inspect a wing leading-edge pneumatic de-ice boot on the training aircraft for cracks, delamination, and proper bonding per the AMM; complete the inspection checklist and make an airworthy/unairworthy determination with written justification.	Pressurization system cutaway diagram, differential-pressure formula reference, training aircraft with pneumatic boots, AMM excerpts for environmental and ice-protection systems, oxygen system service manual excerpt, inspection checklist forms, PPE	Component labeling and pressure calculation checked by instructor—minimum 80% correct; oxygen system presentation covers all required topics as verified against a five-point rubric; boot inspection checklist complete with correct airworthiness determination—satisfactory/unsatisfactory rating
10	Flight Control Systems	52	lab	Students will rig, inspect, and operationally verify primary and secondary flight control systems on a training aircraft to manufacturer travel limits and free-play tolerances.	Using a protractor rigging board and tensiometer, measure aileron, elevator, and rudder cable tension; compare readings to AMM limits at the stated temperature; record readings and make a go/no-go determination for each cable run. Rig aileron travel to AMM-specified up and down deflection angles using a digital inclinometer; adjust turnbuckles in the correct direction, safety-wire to standard aviation practice, and verify final travel is within tolerance. Inspect control cables for corrosion, broken wires, kinks, and proper swage-fitting attachment per AC 43.13-1B criteria; classify each discrepancy and record results on an inspection report with a recommended action for each finding.	Training aircraft, cable tensiometer, digital inclinometer, rigging protractor board, turnbuckle tool, safety-wire and pliers, torque wrench, AC 43.13-1B, aircraft AMM, inspection report forms, PPE	Cable tension measurements recorded correctly and within AMM limits; aileron travel within AMM tolerance after rigging (checked with inclinometer by instructor); safety-wire meets standard inspection criteria; cable inspection report complete with correct classifications—minimum satisfactory rating on all three activities
11	Aircraft Inspections, Airworthiness, and Documentation	60	field	Students will conduct a simulated 100-hour inspection on a training aircraft, prioritize findings by airworthiness status, and produce complete inspection records, a discrepancy list, and a return-to-service entry compliant with 14 CFR Part 43.	Following the school-provided 100-hour inspection checklist (aligned with the AMM), perform a full exterior and interior inspection of the assigned training aircraft, physically checking each item and recording condition—airworthy, repairable, or unairworthy—with supporting measurement data. Compile a formal discrepancy list from inspection findings, prioritizing items that would prevent return to service, and write a corrective-action plan for each discrepancy that references the applicable AMM, AC, or regulatory source. Complete a full-format 14 CFR Part 43 Appendix D maintenance record entry for the 100-hour inspection, including all required data fields; instructor compares entry against a sample correct logbook entry for completeness and regulatory accuracy.	Training aircraft, 100-hour inspection checklist, aircraft AMM and logbooks, AC 43.13-1B, 14 CFR Part 43 text, discrepancy list form, logbook entry form, borescope, flashlight, mirror, torque wrench, calipers, PPE	Inspection checklist 100% completed with all items marked; discrepancy list identifies all pre-planted discrepancies (instructor verification against planted-fault key—minimum 80% found); logbook entry contains all required elements per Part 43 Appendix D—satisfactory/unsatisfactory rating
12	Airframe Systems Integration and FAA Practical Test Readiness	40	practice	Students will demonstrate oral and practical proficiency across all major airframe system areas by completing a mock FAA Airframe oral and practical scenario set evaluated against FAA Airframe Practical Test Standards.	Rotate through six timed oral-question stations (structures, hydraulics, fuel, landing gear, flight controls, environmental/pressurization), answering instructor questions drawn from the FAA Airframe Oral and Practical Standards guide; record questions missed for targeted review. Complete two full practical task cards selected by the instructor from the FAA Airframe PTS—perform the task without assistance, document it on a work order, and present findings and the completed record to the instructor as if before a Designated Airworthiness Representative. Conduct a final self-assessment using the FAA Airframe PTS task list, marking each task as confident, needs review, or not-yet-practiced; develop a written study plan for any not-yet-practiced or needs-review items prior to the certification exam preparation course.	FAA Airframe Practical Test Standards (current edition), FAA Airframe Knowledge Test Supplement, training aircraft and associated shop equipment for all system areas covered in the course, work order forms, logbook entry forms, oral question bank	Oral station performance: minimum 75% of questions answered correctly across all six stations; practical task cards: both tasks rated satisfactory by instructor against PTS acceptable performance standards; self-assessment plan submitted and reviewed by instructor—completion required to pass lesson

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Airframe Systems Written Knowledge Exam	Written exam	25%	Minimum score of 75% (must pass each of the four content domains: structures, systems, inspection/documentation, and regulations)	A 100-question multiple-choice written examination drawn from the FAA Airframe knowledge test content areas, covering wood and fabric, metal and composite structures, welding, hydraulics, pneumatics, fuel, landing gear, flight controls, environmental systems, and 14 CFR documentation requirements. Students must achieve 75% overall and demonstrate minimum competence in each domain; a domain score below 70% requires targeted remediation before the student may sit the FAA Airframe written test. Standard met · Safety · Time · Quality/finish · Documentation
Airframe Practical Skills Demonstration	Skills demonstration	45%	All tasks rated Satisfactory; any Unsatisfactory rating on a safety-critical step results in immediate stop and required remediation before retest	The student performs three instructor-selected practical tasks drawn from different airframe system areas (at minimum one structural repair task and one systems task), completing each task without coaching, within a reasonable time, using correct tools and references, and producing required documentation. Tasks are evaluated against FAA Airframe Practical Test Standards acceptable performance criteria by the lead instructor; the student must explain the regulatory basis for each procedure when asked. Standard met · Safety · Time · Quality/finish · Documentation
Lab Log and Maintenance Records Portfolio	Log	15%	Minimum of 80% of required entries rated Complete and Accurate; no return-to-service entry may contain a regulatory non-compliance and remain unrevised	Students submit the complete collection of work orders, inspection records, discrepancy lists, and logbook entries generated throughout the 12 lessons, organized chronologically and indexed by system area. The instructor reviews each entry for completeness, accuracy of technical data, proper reference citations, and compliance with 14 CFR Part 43 recording requirements; incomplete or non-compliant entries are returned for correction and re-submission before final rating. Standard met · Safety · Time · Quality/finish · Documentation
Airframe Shop Safety Performance Check	Safety audit	15%	100% on all safety-critical steps; any missed critical safety step (lockout/tagout, grounding, PPE selection, fire prevention) is an automatic fail requiring full retest	An unannounced or end-of-course safety observation conducted while the student performs a routine airframe maintenance task; the evaluator uses a standardized 20-item checklist covering PPE use, lockout/tagout application, hazardous-material handling, housekeeping, and tool and equipment safety to confirm that safe practices observed in training are maintained without prompting in a normal work context. Standard met · Safety · Time · Quality/finish · Documentation

TRN-AVIA22-03 Trade course

Powerplant Systems: Reciprocating and Turbine Engine Theory, Maintenance, and Overhaul

548 hr · ~~$14,205~~ COMPLIMENTARY

This course develops the knowledge and hands-on skills required to inspect, troubleshoot, repair, and overhaul aircraft powerplant systems, including reciprocating and turbine engines, engine instruments, fuel metering, ignition, lubrication, and exhaust systems. Students apply FAA-accepted maintenance practices using current manufacturer manuals, FAA Advisory Circulars, and 14 CFR Part 65 standards throughout every task. Lesson content maps directly to the FAA Powerplant mechanic certification areas tested on the FAA written, oral, and practical examinations.

Outcomes

Inspect, troubleshoot, and perform maintenance on reciprocating and turbine engines in accordance with manufacturer maintenance manuals and FAA-accepted practices, documenting all work in the maintenance record.
Identify and correctly service engine fuel metering, ignition, lubrication, cooling, and exhaust systems, applying appropriate PPE and hazardous-material controls throughout.
Perform engine run-up and ground operational tests, interpret engine instrument readings, and identify discrepancies requiring corrective action.
Read and apply technical data including airworthiness directives, service bulletins, illustrated parts catalogs, and type certificate data sheets to powerplant maintenance decisions.
Demonstrate safe engine removal, installation, and rigging procedures, and complete all required FAA maintenance records and logbook entries accurately.
Map each maintenance task to the applicable FAA Powerplant mechanic knowledge and practical test subject areas, demonstrating exam-level understanding of regulations governing powerplant work.

Course text

How the course runs. 12 blocks: Powerplant Safety, Regulations, and Maintenance Documentation; Reciprocating Engine Theory and Construction; Reciprocating Engine Inspection, Disassembly, and Reassembly; Engine Fuel Metering Systems: Carburetors and Fuel Injection; Engine Ignition Systems: Magnetos, Harnesses, and Spark Plugs; Engine Lubrication and Cooling Systems; Engine Exhaust Systems, Turbocharging, and Supercharging; Turbine Engine Theory, Types, and Construction; Turbine Engine Inspection, Troubleshooting, and Compressor Wash; Engine Fuel Control, Indicating Systems, and Engine Monitoring; Engine Removal, Installation, and Ground Run-Up; FAA Powerplant Certification Subject Review and Practical Test Standards Integration.

What competent looks like. Inspect, troubleshoot, and perform maintenance on reciprocating and turbine engines in accordance with manufacturer maintenance manuals and FAA-accepted practices, documenting all work in the maintenance record. Identify and correctly service engine fuel metering, ignition, lubrication, cooling, and exhaust systems, applying appropriate PPE and hazardous-material controls throughout. Perform engine run-up and ground operational tests, interpret engine instrument readings, and identify discrepancies requiring corrective action. Read and apply technical data including airworthiness directives, service bulletins, illustrated parts catalogs, and type certificate data sheets to powerplant maintenance decisions. Demonstrate safe engine removal, installation, and rigging procedures, and complete all required FAA maintenance records and logbook entries accurately. Map each maintenance task to the applicable FAA Powerplant mechanic knowledge and practical test subject areas, demonstrating exam-level understanding of regulations governing powerplant work.

Lessons · 12 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Powerplant Safety, Regulations, and Maintenance Documentation	36	theory	Students will identify OSHA and FAA safety requirements specific to powerplant work, apply lockout/tagout and PPE selection for engine maintenance hazards, and correctly complete FAA maintenance record entries and logbook sign-offs.	Review OSHA standards for fuel, oil, and exhaust hazards in a shop environment; students identify correct PPE for each powerplant task category on a written hazard-matching worksheet. Practice lockout/tagout procedures on a training engine stand: de-energize magnetos using the grounding procedure, placard the aircraft, and verify zero energy before a simulated inspection. Complete sample FAA maintenance record entries and a 337 major repair form for a hypothetical engine cylinder replacement, then peer-review for regulatory accuracy against 14 CFR Part 43 requirements.	14 CFR Parts 43, 65, and 91 (current edition); FAA AC 43.13-1B; OSHA lockout/tagout standard; sample maintenance logbooks; PPE (nitrile gloves, safety glasses, hearing protection); FAA Form 337 samples	Written quiz on safety rules, PPE selection, and documentation requirements; students must score 70% or higher and correctly complete one sample logbook entry without errors to pass.
2	Reciprocating Engine Theory and Construction	48	theory	Students will describe the four-stroke operating cycle, explain how engine displacement, compression ratio, and valve timing affect power output, and identify all major reciprocating engine components and their function.	Label a cutaway diagram of a horizontally opposed reciprocating engine, identifying crankshaft, connecting rods, pistons, cylinders, camshaft, accessory section, and sump, then write one sentence on each component's function. Calculate engine displacement and compression ratio using stroke, bore, and clearance volume data from a manufacturer specification sheet, comparing results against published values. Trace the path of intake charge and exhaust gases through an engine model or diagram during a guided instructor demonstration, identifying the timing of each valve event relative to piston position.	Cutaway or sectioned reciprocating engine (horizontally opposed type); manufacturer overhaul manual; FAA-H-8083-32 Aviation Maintenance Technician Handbook – Powerplant; engineering calculator	Students correctly label all major components on an unlabeled diagram (100% required) and answer a 20-question written quiz on engine theory with a minimum score of 70%.
3	Reciprocating Engine Inspection, Disassembly, and Reassembly	60	lab	Students will perform a top-overhaul-level inspection of a reciprocating engine cylinder assembly using manufacturer tolerances, record findings on an inspection worksheet, and reassemble components to published torque values.	Remove a cylinder from a training engine following the manufacturer maintenance manual procedure; inspect cylinder bore, barrel, head fins, and valve guides using telescoping gauges, micrometers, and a borescope, recording all measurements against service limits. Inspect piston, piston rings, and wrist pin for wear using go/no-go gauges and a micrometer; classify each part as serviceable, repairable, or unserviceable per the overhaul manual limits table. Reinstall the cylinder with a new base gasket, torque cylinder hold-down nuts to manufacturer specification in the correct sequence using a calibrated torque wrench, and complete a written inspection record with signature.	Training reciprocating engine on stand; manufacturer overhaul manual; calibrated torque wrench set; telescoping gauges; outside micrometer set; borescope; ring compressor; new cylinder base gasket; inspection record forms; PPE	All measurements recorded to the correct decimal place; pass/fail decision for each part must match instructor key; torque values and sequence verified by instructor against manual; lab log entry signed off; 100% of steps performed correctly with no safety violations.
4	Engine Fuel Metering Systems: Carburetors and Fuel Injection	44	demo	Students will trace fuel flow through float-type carburetor and continuous-flow fuel injection systems, explain the function of mixture control and acceleration circuits, and identify common malfunctions and their symptoms.	Instructor disassembles a float-type carburetor on a workbench; students identify each circuit (main metering, idle, accelerating pump, mixture control, and float), explain its operating condition, and record findings in their lab log. Using a manufacturer maintenance manual, trace the fuel path from the fuel servo inlet to each injector nozzle on a fuel-injected engine or schematic, noting the role of the flow divider and verifying nozzle flow uniformity concepts. Diagnose four simulated fuel metering malfunctions (e.g., rich idle, lean mixture at altitude, rough running on one cylinder, and carburetor ice indication) using symptom cards and a fault-isolation flowchart, then document corrective action.	Bench-mounted float carburetor (serviceable training unit); continuous-flow fuel injection system (training unit or sectioned display); fuel system schematic posters; manufacturer maintenance manual; FAA-H-8083-32; PPE including fuel-resistant gloves	Students correctly trace and label fuel flow on a system schematic (100% of major circuits identified) and correctly identify and explain corrective action for at least three of four simulated malfunctions; instructor sign-off required.
5	Engine Ignition Systems: Magnetos, Harnesses, and Spark Plugs	44	lab	Students will inspect, time, and test a magneto and ignition harness, clean and gap spark plugs to manufacturer specifications, and verify ignition system integrity using appropriate test equipment.	Remove a magneto from a training engine, inspect breaker points or electronic trigger assembly per the overhaul manual, set internal timing (E-gap) using a timing light and degree wheel or equivalent electronic timing tool, and document procedure in the lab log. Inspect an ignition lead harness for chafing, cracking, and terminal condition; use a high-tension lead tester to check each lead for resistance and insulation breakdown per the manufacturer's acceptable limits. Remove, clean with approved cleaning method, visually inspect, gap, and reinstall dual-plug spark plugs; rotate plug positions per manufacturer rotation schedule; complete a spark plug inspection record with all measurements and serviceable determination.	Training engine with accessible magneto; magneto timing light or electronic timing tool; degree wheel; high-tension lead tester; spark plug gapping tool; spark plug cleaning equipment (abrasive blast type); manufacturer overhaul manual; calibrated torque wrench; lab log forms; PPE	Magneto timing verified by instructor within manufacturer's specified degree tolerance; harness resistance readings recorded and evaluated correctly; all spark plug gaps within ±0.001 inch of specification; lab log complete and signed off by instructor; zero safety violations.
6	Engine Lubrication and Cooling Systems	36	theory	Students will explain wet-sump and dry-sump lubrication system operation, describe the function of oil cooling, filtering, and pressure regulation components, and identify cooling system design differences between air-cooled and liquid-cooled reciprocating engines.	Trace oil flow from sump through pump, filter, pressure relief valve, cooler, and return on a dry-sump system diagram; annotate normal pressure and temperature operating ranges from a manufacturer specification sheet. Inspect an oil filter element from a training engine following the manufacturer's procedure, cut open the filter, check for metal contamination, and classify the findings using the FAA AC 43.13-1B guidance on metal particle analysis. Complete a written case study on an air-cooled engine with elevated cylinder head temperature indications; identify probable causes (blocked cooling fins, baffling damage, lean mixture, timing) and correct troubleshooting sequence per the applicable maintenance manual.	Dry-sump lubrication system training board or schematic; oil filter cutter; magnifying loupe; oil filter from training engine (used); FAA AC 43.13-1B; manufacturer maintenance manual; oil system diagram posters; PPE (nitrile gloves)	Students correctly annotate oil flow and component function on diagram with 100% accuracy on component identification; metal particle classification from oil filter inspection matches instructor key; written case study scored at 70% or higher.
7	Engine Exhaust Systems, Turbocharging, and Supercharging	36	demo	Students will inspect exhaust system components for cracks, leaks, and security using dye penetrant and visual methods, explain turbocharger and supercharger operating principles, and identify airworthiness concerns related to exhaust system failures.	Instructor demonstrates dye penetrant inspection on an exhaust stack: apply cleaner, penetrant, developer, and interpret indications; students then perform the same procedure on a second exhaust component and record results on an NDT inspection record. Identify all components of a turbocharger system on a training unit or schematic (compressor, turbine, wastegate, controller, and intercooler if applicable), explain the role of each, and trace exhaust gas and induction air paths. Review three accident/incident case studies involving exhaust system failures leading to carbon monoxide intrusion or engine compartment fires; identify the missed inspection points and write a corrective maintenance procedure for each scenario.	Exhaust stacks and muffler (training units, some with seeded cracks); dye penetrant inspection kit (Type I or Type II per applicable standard); turbocharger training unit or cutaway display; exhaust system schematics; accident/incident case study handouts; PPE (gloves, safety glasses)	Dye penetrant indications correctly identified and reported on NDT record (must find all seeded indications); turbocharger component identification 100% correct on diagram; case study written responses evaluated by instructor for completeness — minimum 70% score required.
8	Turbine Engine Theory, Types, and Construction	48	theory	Students will explain the Brayton thermodynamic cycle, compare the design and application of turbojet, turbofan, turboprop, and turboshaft engines, and identify the major sections and materials of a turbine engine.	Draw and label a turbojet engine cross-section from memory after a structured lecture, identifying inlet, compressor stages, diffuser, combustion section, turbine stages, and exhaust nozzle, then compare against a reference diagram and self-correct. Using FAA-H-8083-32, compare compression ratios, bypass ratios, and specific fuel consumption data for turbojet versus high-bypass turbofan engines; present a two-minute summary explaining why high-bypass fans dominate commercial aviation. Complete a materials identification exercise matching common turbine engine materials (nickel superalloys, titanium, composites) to their application zones within the engine and the property that makes them suitable for that zone.	FAA-H-8083-32 Aviation Maintenance Technician Handbook – Powerplant; cutaway turbine engine display or large-scale poster; turbine engine manufacturer general familiarization manual (e.g., publicly available training edition); engineering calculator	Completed cross-section diagram with all major sections and components labeled correctly (minimum 80% of items correct); written quiz on Brayton cycle, engine types, and materials scored at 70% or higher.
9	Turbine Engine Inspection, Troubleshooting, and Compressor Wash	52	lab	Students will perform a borescope inspection of turbine engine hot-section and compressor components, evaluate findings against serviceable limits, conduct a compressor wash, and document results in a maintenance record.	Using a video borescope, inspect accessible compressor and turbine blades on a training engine for nicks, dents, tip rubs, cracks, and FOD damage; record each finding with its location (stage, blade number, clock position) and evaluate against the manufacturer's allowable damage limits chart. Perform an on-wing compressor wash following the manufacturer's procedure: dilute wash fluid per specification, apply through the inlet, collect and dispose of effluent per shop environmental procedures, and record the wash in the maintenance log. Troubleshoot four instructor-simulated turbine engine malfunctions (e.g., high exhaust gas temperature, low oil pressure, compressor stall indication, hung start) using a fault isolation manual flowchart and document the diagnosis and recommended corrective action.	Training turbine engine (on stand or mounted); video borescope with recording capability; compressor wash kit and approved wash fluid; manufacturer maintenance manual and allowable damage limits tables; fault isolation manual; maintenance record forms; PPE (hearing protection, eye protection, chemical-resistant gloves)	All borescope findings accurately recorded with location and serviceable/unserviceable determination matching instructor key; compressor wash performed in correct sequence with no environmental violations; at least three of four fault-isolation diagnoses correct; lab log signed off.
10	Engine Fuel Control, Indicating Systems, and Engine Monitoring	44	practice	Students will explain the operation of turbine engine fuel control units and FADEC systems, interpret engine instrument indications (EGT, N1, N2, torque, oil pressure and temperature), and identify out-of-limit conditions requiring maintenance action.	Using a turbine engine fuel system schematic and manufacturer training material, trace fuel from the tank selector through the boost pump, fuel control unit (hydromechanical or FADEC-controlled), flow divider, and fuel nozzles, annotating control inputs at each stage. Work through a set of 15 engine instrument scenario cards (each showing a combination of EGT, N1, oil pressure, and oil temperature values); for each scenario determine whether readings are normal, advisory, or requiring immediate action per the aircraft flight manual limitations section. Set up a simulated engine data trend-monitoring spreadsheet using provided sample data points over ten flights; plot EGT and oil consumption trends, identify which flight shows the beginning of an adverse trend, and write a maintenance recommendation.	Turbine fuel system schematic posters; FADEC training module (manufacturer e-learning or printed training guide); engine instrument scenario card set; sample engine trend monitoring data; aircraft flight manual limitations section (representative GA turbine or regional aircraft); spreadsheet software or graph paper	Fuel flow path annotation 90% accurate per instructor check; instrument scenario cards: 12 of 15 correct interpretations required; trend monitoring exercise: correct identification of adverse trend flight and appropriate maintenance recommendation — scored by instructor rubric, minimum 70%.
11	Engine Removal, Installation, and Ground Run-Up	56	field	Students will demonstrate safe engine removal and installation procedures on a training aircraft or engine-change trainer, perform a post-installation run-up following the appropriate checklist, and record all work in the maintenance log.	As a team (two to three students) remove a reciprocating engine from a training airframe following the manufacturer maintenance manual: disconnect fuel, oil, electrical, and control connections in the correct sequence; support the engine with an approved hoist or engine stand, and document each disconnected item on the removal checklist. Install a serviceable engine, reconnect all systems, safety-wire fasteners as required, and complete an installation inspection using the manufacturer's return-to-service checklist, verifying all fluid levels, control travel, and security of attachments. Under instructor supervision at a designated engine run area, perform a cold-start pre-oil (if applicable), start the engine following the POH/AFM checklist, conduct a static run-up to check magneto drop (reciprocating) or idle/takeoff power parameters, note any discrepancies, and complete the maintenance log entry including an operational check notation.	Training airframe with reciprocating engine; engine hoist rated for the engine weight; engine stand; manufacturer maintenance manual and installation checklist; calibrated torque wrench set; safety wire and safety wire pliers; oil and fuel servicing equipment; fire extinguisher (on-site during run-up); hearing protection and eye protection; maintenance logbook	All removal and installation steps performed in manual sequence with no missed connections — instructor verifies against checklist (100% of safety-critical items correct); run-up checklist completed and discrepancies, if any, correctly identified; maintenance log entry complete with correct regulatory language — instructor sign-off required before any run-up proceeds.
12	FAA Powerplant Certification Subject Review and Practical Test Standards Integration	44	theory	Students will map all course content to the FAA Powerplant Mechanic Airman Certification Standards subject areas, identify personal knowledge gaps through a diagnostic practice written exam, and demonstrate exam-level oral question responses in a structured review.	Complete a full-length timed FAA powerplant practice written examination (60 questions drawn from the FAA Powerplant knowledge test question bank); score the exam, categorize missed questions by subject area, and create an individual study plan targeting weak areas. In pairs, conduct a 20-minute oral Q&A session using the FAA Powerplant Practical Test Standards as the question framework; one student plays examiner, the other applicant, then switch roles; instructor monitors and provides feedback on answer completeness and use of technical references. For each of the major powerplant practical test projects (e.g., reciprocating engine cylinder inspection, turbine engine inspection, fuel system service, ignition system inspection), students compile a reference card listing the applicable regulation, accepted practice source, and key inspection criteria they would cite during an oral exam.	FAA Airman Certification Standards – Mechanic (current edition); FAA Powerplant knowledge test question bank (FAA published or approved test prep software); FAA-H-8083-32; 14 CFR Part 65; student-compiled reference cards from prior lessons	Practice written exam scored and review plan submitted — no numeric pass required for this diagnostic use, but all questions missed must be reviewed and corrected; oral session: instructor evaluates responses using ACS task criteria — student must demonstrate at least satisfactory (ACS standard) on 80% of tasks reviewed; reference cards reviewed for accuracy by instructor.

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Powerplant Systems Written Knowledge Examination	Written exam	25%	Minimum score of 70% (42 of 60 questions correct)	A 60-question closed-book multiple-choice exam drawn from FAA Powerplant knowledge test subject areas covering reciprocating and turbine engine theory, fuel metering, ignition, lubrication, exhaust, engine instruments, and applicable regulations. Questions are mapped to FAA Airman Certification Standards subject codes to replicate the format students will encounter on the official FAA written test. Standard met · Safety · Time · Quality/finish · Documentation
Powerplant Practical Skills Demonstration	Skills demonstration	45%	All safety-critical steps rated Satisfactory; overall task average of Satisfactory or above on the ACS rating scale; no Unsatisfactory ratings on any single critical task	Students perform three examiner-selected practical tasks — one from reciprocating engine maintenance (such as cylinder inspection and reassembly), one from turbine engine maintenance (such as borescope inspection and findings evaluation), and one from engine systems (such as magneto timing or fuel system service) — using the FAA Powerplant Practical Test Standards task criteria as the evaluation rubric. The instructor acts as the oral and practical examiner, asking task-relevant oral questions during each task. Standard met · Safety · Time · Quality/finish · Documentation
Powerplant Maintenance Lab Log Portfolio	Log	15%	All 12 required lab log entries present, signed, and complete; no missing measurements or undocumented decisions; technical accuracy verified by instructor on all entries	Students submit a compiled lab log documenting every hands-on and laboratory activity completed during the course, including inspection findings, measurements, serviceable/unserviceable determinations, torque values, and maintenance record entries. Each entry must reference the applicable maintenance manual page or regulatory basis for the action taken and must be written as it would appear in an FAA-compliant maintenance record. Standard met · Safety · Time · Quality/finish · Documentation
Powerplant Safety Compliance Check	Safety audit	15%	Zero critical safety violations observed across the entire course; all lockout/tagout, PPE, and hazardous-material handling procedures performed correctly on every evaluated lab day	Throughout the course the instructor maintains a running safety observation record for each student, evaluating PPE selection and use, magneto grounding procedures before engine work, fuel and oil handling, fire extinguisher awareness during run-up, and correct torque and safety-wire practices. Any single critical safety violation (defined as an action with immediate potential for personal injury or aircraft damage) results in an automatic unsatisfactory for that lab session and requires a mandatory remediation module before the student continues hands-on work. Standard met · Safety · Time · Quality/finish · Documentation

TRN-AVIA22-04 Trade course

Avionics: Aircraft Electrical, Instrument, and Communication Systems

548 hr · ~~$14,205~~ COMPLIMENTARY

This course develops competency in the installation, inspection, troubleshooting, and maintenance of aircraft electrical systems, flight instruments, navigation and communication equipment, and digital avionics as required for FAA Airframe and Powerplant certification. Students apply electrical theory, read wiring diagrams and maintenance manuals, and use calibrated test equipment to perform work to airworthiness standards. Lessons are sequenced from foundational electrical principles through integrated avionics systems, with every task performed under applicable FAA regulations and manufacturer specifications.

Outcomes

Apply Ohm's Law and circuit analysis to diagnose faults in aircraft DC and AC electrical systems using multimeters, oscilloscopes, and circuit-breaker panels.
Inspect, rig, and functionally test aircraft flight instruments including pitot-static, gyroscopic, and magnetic compass systems to manufacturer and regulatory tolerances.
Install and operationally verify communication and navigation avionics (VHF comm, VOR, ILS, GPS, transponder) in accordance with applicable wiring diagrams and FAA/TSO requirements.
Troubleshoot and repair aircraft lighting systems, warning and indication circuits, and autopilot interface wiring using systematic fault-isolation procedures.
Complete all required maintenance records, FAA Form 337s (where applicable), and return-to-service documentation accurately and legibly.
Demonstrate safe electrical work practices including energy-control (lockout/tagout), ESD protection, and correct use of PPE for every avionics task.

Course text

How the course runs. 12 blocks: Electrical Fundamentals and Safe Work Practices in Avionics; Aircraft Wiring, Connectors, and Fabrication; Aircraft DC Power Distribution: Buses, Circuit Breakers, and Switches; Aircraft AC Power Systems, Alternators, and Inverters; Pitot-Static Systems and Air Data Instruments; Gyroscopic Instruments: Attitude, Heading, and Turn Indicators; Magnetic Compass and Electronic Flight Display Systems; VHF Communication Systems: Installation and Checkout; Navigation Systems: VOR, ILS, GPS, and ADS-B; Transponders, Audio Panels, and Intercom Systems; Aircraft Lighting, Warning Systems, and Autopilot Interface; Avionics System Integration, Documentation, and Return to Service.

What competent looks like. Apply Ohm's Law and circuit analysis to diagnose faults in aircraft DC and AC electrical systems using multimeters, oscilloscopes, and circuit-breaker panels. Inspect, rig, and functionally test aircraft flight instruments including pitot-static, gyroscopic, and magnetic compass systems to manufacturer and regulatory tolerances. Install and operationally verify communication and navigation avionics (VHF comm, VOR, ILS, GPS, transponder) in accordance with applicable wiring diagrams and FAA/TSO requirements. Troubleshoot and repair aircraft lighting systems, warning and indication circuits, and autopilot interface wiring using systematic fault-isolation procedures. Complete all required maintenance records, FAA Form 337s (where applicable), and return-to-service documentation accurately and legibly. Demonstrate safe electrical work practices including energy-control (lockout/tagout), ESD protection, and correct use of PPE for every avionics task.

Lessons · 12 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Electrical Fundamentals and Safe Work Practices in Avionics	39.5	theory	Students will explain voltage, current, resistance, and power relationships using Ohm's Law and identify all required PPE and lockout/tagout procedures before touching any aircraft electrical system.	Solve a 20-problem worksheet applying Ohm's Law and Watt's Law to series, parallel, and series-parallel circuits typical of aircraft loads, correcting errors through peer review. Walk through a posted lockout/tagout procedure for a training aircraft with the master switch and avionics bus, then demonstrate proper application of locks and tags on the actual trainer. Match a set of 30 electrical symbols on an aircraft wiring diagram excerpt to their component descriptions in the FAA Aviation Maintenance Technician Handbook—Airframe (FAA-H-8083-31) and record findings in a lab notebook.	FAA-H-8083-31 (Airframe Handbook), FAA-H-8083-32 (Powerplant Handbook), NFPA 70E reference card, multimeters, lockout/tagout kit, wiring diagram excerpts, PPE (safety glasses, insulating gloves rated for aircraft voltage), whiteboard	Written 20-question circuit-analysis quiz scored at 80% or higher; instructor observation confirms correct PPE donned and lockout/tagout applied without prompting before any hands-on step.
2	Aircraft Wiring, Connectors, and Fabrication	45	lab	Students will fabricate a four-circuit aircraft wiring harness segment — including correct wire gauge selection, splicing, terminal crimping, and connector assembly — that passes continuity and insulation-resistance tests to MIL-SPEC and manufacturer tolerances.	Use an aircraft electrical load analysis chart and the FAA wire-sizing guidelines in AC 43.13-1B to select correct wire gauges for four different current loads, documenting the selection rationale in writing. Fabricate a wiring harness segment using aircraft-grade wire, heat-shrink tubing, D-sub connectors, and a ratchet crimper; verify each crimp with a pull-test gauge to manufacturer-specified minimum pull force. Perform continuity testing with a multimeter and insulation resistance testing with a megohmmeter on the completed harness, recording all readings on an inspection worksheet and identifying any wire that falls outside limits.	Aircraft-grade wire (various gauges), wire stripper, ratchet crimper, pull-test gauge, heat-shrink tubing, heat gun, D-sub connectors and pins, multimeter, megohmmeter, AC 43.13-1B, MIL-DTL-22992 reference sheet, safety glasses, ESD wrist strap and mat	All four circuits pass continuity check (no opens, no shorts); insulation resistance meets minimum threshold per AC 43.13-1B; harness visually passes instructor inspection for chafing protection and secure terminations — all three criteria required for pass.
3	Aircraft DC Power Distribution: Buses, Circuit Breakers, and Switches	43	demo	Students will trace a multi-bus DC power distribution schematic, identify the function of essential, avionics, and battery buses, and correctly reset or replace a tripped circuit breaker on a training panel in accordance with maintenance manual procedures.	Color-code a printed aircraft electrical schematic by bus segment (battery bus, main bus, avionics bus, essential bus), annotating each component's rated current and the circuit breaker protecting it. Instructor demonstrates fault insertion (open circuit, short circuit) on a live training panel; students then use a multimeter in voltage-drop and current-draw mode to locate the inserted fault, recording each diagnostic step. Following a simulated maintenance discrepancy write-up, students replace a circuit breaker on the training panel, torque the terminal screw to specification, and complete a sample maintenance logbook entry.	Aircraft electrical training panel with bus bars, circuit breakers, and toggle switches; multimeter; torque screwdriver; aircraft wiring schematic set; circuit breaker assortment; maintenance logbook sample forms; AC 43.13-1B; safety glasses; lockout/tagout kit	Student locates each of two instructor-inserted faults within 15 minutes using documented step-by-step voltage-drop method; logbook entry reviewed by instructor and accepted as complete and legible — both required for pass.
4	Aircraft AC Power Systems, Alternators, and Inverters	39.5	theory	Students will describe the operating principles of aircraft alternators, voltage regulators, and static and rotary inverters, and calculate AC circuit quantities (voltage, current, impedance, power factor) for single-phase aircraft loads.	Complete a structured reading assignment in FAA-H-8083-31 Chapter 9, then answer 15 short-answer questions on alternator output regulation, over-voltage protection, and split-bus architecture without notes, self-grading against an answer key. Using an oscilloscope connected to a bench alternator simulator, measure output voltage, frequency, and waveform shape under no-load and loaded conditions, sketching waveforms and recording data on a lab sheet. In small groups, calculate impedance, current, and power factor for three sample AC circuits representing aircraft avionics loads, then present calculations to the class for peer verification.	FAA-H-8083-31, bench alternator/generator simulator, oscilloscope, multimeter (AC setting), scientific calculator, AC circuit calculation worksheet, projector for group presentations, safety glasses	Oscilloscope measurement readings within ±5% of instructor-measured reference values; AC calculation worksheet scored at 80% or higher — both required for pass.
5	Pitot-Static Systems and Air Data Instruments	47	lab	Students will inspect a pitot-static system for leaks and blockages, connect a pitot-static tester, and verify altimeter, airspeed indicator, and vertical speed indicator readings against reference values within the tolerances specified in FAR Part 91 and the instrument manufacturer's data.	Perform a pre-test visual inspection of pitot-static plumbing, alternate static port, and drain points on a training airframe, recording findings on a standardized inspection checklist and tagging any discrepancies. Connect a calibrated pitot-static tester (ramp tester) to the aircraft system and perform a static system leak test, an airspeed indicator functional check, and an altimeter accuracy check at two altitude settings, recording all readings and comparing to manufacturer limits. Identify and document two instructor-inserted discrepancies (one leak, one out-of-tolerance altimeter reading), complete a sample FAA Form 337 for a hypothetical altimeter swap, and discuss the regulatory basis for the 24-month altimeter and transponder check requirement.	Training aircraft or airframe section with complete pitot-static system, calibrated pitot-static ramp tester, inspection mirror, flashlight, airspeed indicator, altimeter, VSI, manufacturer's instrument calibration data sheets, FAA Form 337 blanks, 14 CFR Part 91 excerpt (§91.411 and §91.413), safety glasses	Leak test results recorded correctly with pass/fail determination matching instructor reference; all instrument readings compared to tolerance and discrepancies correctly identified; Form 337 accepted by instructor as complete — all three required for pass.
6	Gyroscopic Instruments: Attitude, Heading, and Turn Indicators	43	demo	Students will explain the gyroscopic principles underlying the attitude indicator, heading indicator, and turn coordinator, and perform an operational check of each instrument, identifying erection time, precession errors, and vacuum/electric supply requirements.	Using a free-spinning gyroscope demonstration unit, observe and describe rigidity in space and precession, recording observations with diagrams in the lab notebook, then match each property to its application in a flight instrument. Instructor demonstrates engine-run or vacuum pump operation on a training aircraft; students time gyroscope erection from cold start, measure suction gauge reading, and compare to manufacturer's normal operating range, recording data on a structured data sheet. Troubleshoot two instructor-assigned written scenarios (one vacuum system fault, one electric gyro fault) by listing probable causes in order of likelihood and identifying the diagnostic steps and tools needed, then discuss findings with the class.	Free-spinning gyroscope demonstration unit, training aircraft or gyro instrument trainer with vacuum and electric gyro instruments, suction gauge, stopwatch, multimeter, manufacturer maintenance manuals for installed instruments, lab notebooks, whiteboard, safety glasses	Erection time and suction reading recorded and correctly compared to limits; two troubleshooting scenarios answered with correct priority sequence of probable causes, verified by instructor discussion — both required for pass.
7	Magnetic Compass and Electronic Flight Display Systems	43	lab	Students will swing a magnetic compass on an aircraft, record deviation at eight headings, construct a compass correction card, and describe the architecture and data inputs of a basic glass-cockpit primary flight display (PFD) and multifunction display (MFD).	Position a training aircraft on a calibrated compass rose (or use an indoor compass swing table), take deviation readings every 45 degrees of heading, compute and record deviation values, and produce a hand-written compass correction card meeting manufacturer format requirements. Using a bench-mounted glass-cockpit trainer (or software simulator), identify the data sources feeding the PFD (ADAHRS, magnetometer, GPS) and trace the signal path from sensor to display by following the system wiring diagram and the avionics manufacturer's installation manual. Research and present a five-minute verbal summary comparing the maintenance tasks and regulatory requirements for a traditional six-pack instrument panel versus an integrated glass-cockpit system, referencing at least two sections of AC 43.13-1B or relevant ACs.	Training aircraft or compass swing table, calibrated compass rose or directional reference, magnetic compass, compass correction card blanks, non-magnetic screwdriver, glass-cockpit trainer or avionics simulator software, manufacturer installation manual, AC 43.13-1B, safety glasses	Compass correction card has deviation values at all eight headings; instructor verifies the card is legible and correctly formatted; PFD signal-path tracing exercise accepted by instructor with all data sources correctly identified — both required for pass.
8	VHF Communication Systems: Installation and Checkout	45	lab	Students will remove and reinstall a VHF communication transceiver in a training aircraft tray, verify antenna coax continuity and VSWR within acceptable limits, and conduct a functional communication check confirming transmit and receive operation.	Following the manufacturer's installation manual, remove the VHF comm unit from its tray, inspect the tray connector pins and coax for corrosion and damage, document findings on a standardized inspection form, and reinstall the unit torquing all fasteners to specification. Use a coaxial cable tester and an antenna analyzer (or VSWR meter) to measure antenna feedline continuity and standing wave ratio, recording results and comparing to the manufacturer's maximum acceptable VSWR limit. Perform a functional communication check by transmitting on a designated ground test frequency (or using a handheld radio as a local receiver), confirming clear audio transmit and receive, and entering the results in a sample maintenance record.	Training aircraft with VHF comm transceiver and tray, manufacturer installation/maintenance manual, coaxial cable tester, VSWR/antenna analyzer or field strength meter, torque driver, handheld VHF radio (for receive check), maintenance logbook sample forms, coax connectors, safety glasses, ESD wrist strap	VSWR reading within manufacturer limit; functional check demonstrates clear two-way audio; maintenance record entry reviewed and accepted by instructor as complete and accurate — all three required for pass.
9	Navigation Systems: VOR, ILS, GPS, and ADS-B	51	theory	Students will describe the operating principles of VOR, ILS (localizer and glideslope), GPS, and ADS-B Out systems, identify the regulatory requirements for ADS-B Out equipage, and interpret a navigation avionics wiring diagram to locate antenna, receiver, and indicator connections.	Complete a structured reading of FAA-H-8083-31 navigation systems chapters and the relevant sections of 14 CFR Part 91 for ADS-B Out requirements, then complete a 25-question fill-in and multiple-choice quiz on system principles, signal characteristics, and regulatory applicability. Trace a composite navigation avionics wiring diagram (VOR/ILS receiver, CDI indicator, GPS/WAAS unit, ADS-B transponder, and associated antennas) identifying each component, wire run, shield-ground point, and circuit-breaker protection, annotating the diagram in red pen. In pairs, use an avionics ramp tester or PC-based avionics simulator to perform a VOR receiver sensitivity check and an ILS CDI deflection test, recording all readings on a data sheet and comparing to manufacturer specifications.	FAA-H-8083-31, 14 CFR Part 91 ADS-B excerpt, composite navigation avionics wiring diagram set, avionics ramp tester or avionics PC simulator, multimeter, red pen, annotation worksheets, safety glasses	25-question quiz scored at 80% or higher; wiring diagram annotation checked by instructor confirming all components and ground points correctly identified — both required for pass.
10	Transponders, Audio Panels, and Intercom Systems	43	lab	Students will functionally test a Mode C or Mode S transponder using a ramp test set, verify reply efficiency and altitude encoder output, and trace and repair a simulated fault in an aircraft audio panel intercom circuit.	Connect a calibrated transponder ramp test set to a training aircraft transponder, interrogate in Mode C and Mode S, record reply efficiency percentage and altitude encoder output, and compare results to the minimum standards referenced in the maintenance manual and 14 CFR §91.413. With the aircraft electrical power isolated via lockout/tagout, trace the audio panel schematic to locate a simulated open-circuit fault (wire disconnected by instructor) using a multimeter in continuity and voltage-drop mode, documenting each step in the fault log. Repair the intercom fault, restore power, and perform a functional audio check (pilot, copilot, and passenger intercom paths), recording the repair action and post-check results in a maintenance logbook entry.	Training aircraft with Mode C or Mode S transponder and altitude encoder, calibrated transponder ramp test set, audio panel with intercom, multimeter, headsets, aircraft wiring diagram, 14 CFR §91.413 excerpt, maintenance logbook forms, lockout/tagout kit, safety glasses, ESD wrist strap	Transponder reply efficiency meets minimum standard per ramp tester readout; fault correctly located and repaired; functional audio check passed on all intercom paths; logbook entry accepted by instructor — all four required for pass.
11	Aircraft Lighting, Warning Systems, and Autopilot Interface	51	practice	Students will inspect, test, and document the airworthiness of an aircraft's exterior lighting system and at least two crew-alerting or warning circuits, and describe the electrical interface between an autopilot servo and the aircraft flight-control system.	Perform a complete exterior lighting inspection (navigation lights, anti-collision strobes, landing and taxi lights) on a training aircraft using an inspection checklist aligned with 14 CFR Part 23 and manufacturer data, replacing any discrepant lamp or bulb and recording the corrective action. Simulate a stall warning system activation using a test switch and verify the horn or stick-shaker activates within the specified speed range; then trace the stall warning circuit on the wiring diagram to identify the sensor, control module, and alerting device. Using a manufacturer's autopilot maintenance manual and wiring diagram, identify the servo motor circuit, engage relay, disconnect switch, and torque-limiter interface; complete a written explanation of how a hardover servo fault is electrically isolated by the pilot.	Training aircraft with full exterior lighting, stall warning system, and autopilot installation (or representative mock-up panel), lamp/bulb assortment, multimeter, test switch, wiring diagrams, 14 CFR Part 23 reference, manufacturer autopilot maintenance manual, inspection checklists, maintenance logbook forms, safety glasses, lockout/tagout kit	Lighting inspection checklist completed with all discrepancies correctly identified and corrective actions recorded; stall warning circuit traced correctly on diagram; autopilot written explanation accepted by instructor as technically accurate — all three required for pass.
12	Avionics System Integration, Documentation, and Return to Service	58	field	Students will plan, execute, document, and present a complete avionics maintenance task on a training aircraft — from work-order receipt through final return-to-service sign-off — demonstrating integration of electrical theory, regulatory compliance, and professional record-keeping.	Receive a written discrepancy write-up from the instructor simulating an aircraft-on-ground (AOG) situation; develop a written maintenance plan identifying the applicable maintenance manual sections, required tools and test equipment, estimated time, and safety precautions before touching the aircraft. Execute the maintenance task (instructor assigns one of: avionics unit swap, wiring repair, or instrument calibration) following the approved plan, with the instructor observing and scoring task performance against a rubric for technical accuracy, tool use, ESD discipline, and safety compliance. Complete all required documentation — maintenance logbook entry, parts record, and FAA Form 337 where applicable — and conduct a five-minute verbal defense with the instructor explaining the regulatory basis for each action taken and any limitations or airworthiness directives (ADs) reviewed.	Training aircraft, assigned avionics maintenance manuals, applicable ADs and service bulletins, full tool set (multimeter, crimper, torque driver, VSWR meter, pitot-static or transponder ramp tester as assigned), lockout/tagout kit, ESD mat and wrist strap, maintenance logbook forms, FAA Form 337 blanks, PPE (safety glasses, insulating gloves), AC 43.13-1B	Maintenance plan approved by instructor before work begins; task performance rubric scored at 80% or higher; documentation reviewed and accepted by instructor as complete, accurate, and regulatory compliant; verbal defense demonstrates understanding of at least two regulatory references — all four required for pass.

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Avionics Knowledge Exam	Written exam	25%	75% correct (30 of 40 questions)	A 40-question written exam covering electrical theory, aircraft electrical systems, instruments (pitot-static, gyroscopic, magnetic), communication and navigation system principles, transponder regulations, and maintenance documentation requirements. Questions are drawn from FAA Airframe General and Airframe Systems knowledge areas to mirror the format and content emphasis of the FAA written tests. Standard met · Safety · Time · Quality/finish · Documentation
Avionics Skills Demonstration	Skills demonstration	45%	Score of 80% or higher on the performance rubric with zero unsatisfactory marks on any safety or ESD item	Students perform two assigned tasks drawn from the lab curriculum — one instrument operational check (pitot-static or gyroscopic) and one avionics unit remove-and-reinstall with functional test — evaluated by the instructor in real time on a standardized rubric assessing technical accuracy, correct use of maintenance manuals, tool discipline, ESD precautions, lockout/tagout compliance, and completeness of logbook entry. Standard met · Safety · Time · Quality/finish · Documentation
Laboratory Log and Maintenance Documentation Portfolio	Log	15%	All 12 lesson lab sheets submitted; instructor scores each entry Satisfactory; at least 10 of 12 entries rated Satisfactory on first submission	Students maintain a cumulative lab log containing data sheets, inspection checklists, wiring diagram annotations, compass correction cards, and maintenance logbook entries from every hands-on lesson. The portfolio is reviewed at midterm (after Lesson 6) and at course end; entries must be legible, technically accurate, and include all required measurements, pass/fail determinations, and corrective-action statements as if each entry were a legal maintenance record. Standard met · Safety · Time · Quality/finish · Documentation
Safety and Compliance Check	Safety audit	15%	100% on all mandatory safety behaviors; any single failure requires immediate remediation and re-check before the student may continue laboratory work	The instructor conducts three unannounced safety walk-throughs during the course to evaluate each student on correct PPE selection and donning, proper lockout/tagout execution, ESD strap and mat use when handling avionics components, and correct storage and handling of tools and test equipment. The check uses a binary Satisfactory/Unsatisfactory rubric with no partial credit on safety items. Standard met · Safety · Time · Quality/finish · Documentation

TRN-AVIA22-05 Trade course

Federal Aviation Regulations for Aviation Maintenance

548 hr · ~~$14,205~~ COMPLIMENTARY

This course develops the regulatory knowledge and documentation skills required of certificated aviation mechanics working under Title 14 of the Code of Federal Regulations (14 CFR). Students study the parts of the FAR most directly governing airworthiness, maintenance, certification, and record-keeping, and apply that knowledge through case analysis, mock inspections, and maintenance record exercises. Lesson content is mapped to the FAA Airframe and Powerplant (A&P) knowledge test areas and the practical-test standards so that regulatory competence supports credential attainment and daily shop practice.

Outcomes

Locate, interpret, and apply the applicable sections of 14 CFR Parts 1, 21, 39, 43, 45, 65, 91, 119, 121, 135, and 145 to maintenance decisions and documentation.
Determine the airworthiness status of an aircraft using the aircraft's logbooks, airworthiness directives, type certificate data sheets, and supplemental type certificates.
Complete FAA maintenance records and forms accurately, including return-to-service entries, conformity inspection records, and maintenance release statements, meeting the requirements of 14 CFR Part 43.
Explain the privileges, limitations, and responsibilities of the Aviation Mechanic Certificate with Airframe and/or Powerplant ratings as defined in 14 CFR Part 65.
Apply safety and hazard-communication requirements (OSHA HazCom, proper PPE selection, lockout/tagout procedures) as required in a maintenance regulatory environment.
Demonstrate correct use of FAA-approved data sources—including the FAA website, Regulatory and Guidance Library, and manufacturer Airworthiness Limitations sections—to determine maintenance requirements.

Course text

How the course runs. 12 blocks: Structure of the Federal Aviation Regulations and FAA Authority; 14 CFR Part 1 — Definitions and Abbreviations; 14 CFR Part 43 — Maintenance, Preventive Maintenance, Rebuilding, and Alteration; 14 CFR Part 65 — Aviation Mechanic Certification: Privileges, Limitations, and Responsibilities; 14 CFR Part 39 — Airworthiness Directives: Compliance and Documentation; Type Certificate Data Sheets, Supplemental Type Certificates, and FAA-Approved Data; 14 CFR Part 91 — General Operating and Flight Rules Affecting Maintenance; 14 CFR Parts 121 and 135 — Air Carrier Maintenance Programs; 14 CFR Part 145 — Repair Station Certification and Operations; 14 CFR Part 21 — Certification Procedures for Products and Articles; Maintenance Documentation, Record-Keeping Systems, and Practical Record Lab; Regulatory Compliance Integration, Safety Culture, and FAR Exam Review.

What competent looks like. Locate, interpret, and apply the applicable sections of 14 CFR Parts 1, 21, 39, 43, 45, 65, 91, 119, 121, 135, and 145 to maintenance decisions and documentation. Determine the airworthiness status of an aircraft using the aircraft's logbooks, airworthiness directives, type certificate data sheets, and supplemental type certificates. Complete FAA maintenance records and forms accurately, including return-to-service entries, conformity inspection records, and maintenance release statements, meeting the requirements of 14 CFR Part 43. Explain the privileges, limitations, and responsibilities of the Aviation Mechanic Certificate with Airframe and/or Powerplant ratings as defined in 14 CFR Part 65. Apply safety and hazard-communication requirements (OSHA HazCom, proper PPE selection, lockout/tagout procedures) as required in a maintenance regulatory environment. Demonstrate correct use of FAA-approved data sources—including the FAA website, Regulatory and Guidance Library, and manufacturer Airworthiness Limitations sections—to determine maintenance requirements.

Lessons · 12 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Structure of the Federal Aviation Regulations and FAA Authority	36	theory	Students will correctly identify the structure of Title 14 CFR, locate any cited regulatory section within the FAA Regulatory and Guidance Library, and explain how FAA Orders and Advisory Circulars relate to regulatory requirements.	Guided navigation exercise: given a list of 20 regulatory citations, students locate each section in print and online versions of 14 CFR and annotate the purpose of each part. Small-group discussion comparing the binding authority of a CFR rule versus an Advisory Circular versus a manufacturer's maintenance manual, with each group presenting one scenario where the distinction matters. Written reflection: students trace the rulemaking process for a sample Airworthiness Directive from NPRM through final rule, citing which office issued it and under what statutory authority.	14 CFR Title 14 (current edition), FAA Regulatory and Guidance Library (rgl.faa.gov), FAA Order 8900.1, Advisory Circular AC 00-2 (Advisory Circular Checklist), computers with internet access, highlighters, printed CFR excerpts	Quiz of 25 multiple-choice questions covering CFR structure, FAA offices, and the hierarchy of regulatory documents; passing score 70% or higher.
2	14 CFR Part 1 — Definitions and Abbreviations	30	theory	Students will define at least 40 regulatory terms from 14 CFR Part 1 and correctly apply those definitions to classify aircraft, maintenance actions, and personnel roles presented in case scenarios.	Flashcard drill in pairs covering all definitions in Part 1 with an emphasis on terms that appear most frequently on the A&P knowledge test: airworthy, major repair, major alteration, preventive maintenance, and certificated mechanic. Classification exercise: students receive a list of 30 maintenance tasks and must label each as maintenance, preventive maintenance, major repair, or major alteration using only Part 1 and Part 43 Appendix A definitions. Case-study analysis: students read three FAA enforcement summaries in which a regulatory violation turned on the precise meaning of a defined term, then identify which definition was at issue and how it was misapplied.	14 CFR Part 1 (current edition), 14 CFR Part 43 Appendix A, printed case summaries from FAA Legal Interpretations database, definition worksheet	Matching quiz of 40 terms to definitions plus five classification scenarios; passing score 70% or higher.
3	14 CFR Part 43 — Maintenance, Preventive Maintenance, Rebuilding, and Alteration	60	theory	Students will explain every section of Part 43, including who may perform and approve maintenance, what records must be made, and what data must be FAA-approved, and will draft a compliant maintenance record entry for a sample task.	Section-by-section lecture and annotation: students read each section of Part 43 aloud in rotation, the instructor pauses to clarify and connect to real shop scenarios, and students annotate a personal copy with notes. Record-writing workshop: students are given a completed aircraft inspection checklist and must write a legally compliant return-to-service logbook entry meeting the content requirements of 14 CFR 43.9 and 43.11, then exchange entries for peer critique against a provided rubric. Mock enforcement scenario: students receive a fictitious FAA Letter of Investigation alleging a Part 43 violation, identify exactly which paragraph was allegedly violated, and prepare a written explanation of what the correct action should have been.	14 CFR Part 43 (current edition) including Appendices A–D, FAA-H-8083-30 (Aviation Maintenance Technician Handbook – General), sample aircraft logbook pages, record-entry rubric, pens	Students produce a written return-to-service entry graded against the rubric with all required data elements present; and a 20-question Part 43 quiz at 70% or higher.
4	14 CFR Part 65 — Aviation Mechanic Certification: Privileges, Limitations, and Responsibilities	44	theory	Students will state the eligibility requirements, privileges, and limitations of the Aviation Mechanic Certificate with Airframe and Powerplant ratings, and distinguish actions they may perform independently from those requiring supervision or additional authority.	Structured Q&A review of 14 CFR Part 65 Subpart D, with students taking turns citing the specific paragraph that answers each privilege or limitation question posed by the instructor. Privilege-matrix exercise: students build a two-axis table comparing what an A&P mechanic, an IA (Inspection Authorization holder), a repairman, and a pilot-owner may each perform under 14 CFR, then defend their table in small-group discussion. Role-play scenario: one student acts as an FAA inspector and one as a mechanic; the inspector asks a series of questions about the mechanic's authority to sign off a specific task, and the mechanic must cite the correct paragraph; roles then switch.	14 CFR Part 65 (current edition), Part 43, Part 91.409, privilege-matrix template, scenario cards	Oral recitation of at least five specific privileges and three specific limitations, each cited to the correct paragraph; and a 15-question written quiz at 70% or higher.
5	14 CFR Part 39 — Airworthiness Directives: Compliance and Documentation	50	demo	Students will locate an Airworthiness Directive applicable to a specified aircraft, determine the compliance method and due time, verify current compliance status using logbooks, and document compliance correctly.	Instructor demonstration: using the FAA AD search tool (rgl.faa.gov), the instructor retrieves ADs for a training aircraft by make, model, and serial number, then walks through the compliance document section by section, explaining each field. Hands-on AD search: each student is assigned a different training aircraft (using a data card with make, model, serial, and total time), searches for all applicable ADs, and prepares a compliance status worksheet showing each AD number, effective date, compliance method, and next due date. Documentation drill: given a completed AD compliance task and a filled-in AD, students write the required logbook entry to record AD compliance, including the AD number, revision, method of compliance, date, aircraft total time, and mechanic signature.	14 CFR Part 39 (current edition), FAA AD search website, sample AD documents (printed and online), aircraft data cards for training aircraft, logbook entry forms, AD compliance worksheet template, computers	Each student's AD compliance worksheet is checked for accuracy against an instructor key; all ADs must be correctly identified and the compliance entry must contain all required elements. Both items must be complete and accurate to pass.
6	Type Certificate Data Sheets, Supplemental Type Certificates, and FAA-Approved Data	44	demo	Students will retrieve a Type Certificate Data Sheet (TCDS) for a specified aircraft, identify the approved equipment list, engine model, and operating limitations, and explain how an STC changes the TCDS baseline and what documentation must accompany an STC installation.	Instructor-led walk-through of the FAA aircraft certification database: locating a TCDS, reading the approved engine and propeller combinations, noting the operating limitations, and comparing two TCDS revisions to identify what changed. TCDS scavenger hunt: student pairs receive a training aircraft data card and must answer 15 specific questions—engine TBO source, approved fuel grades, CG range, and so on—by reading the actual TCDS, then present answers with page references. STC case study: students examine a complete STC data package (STC approval document, installation instructions, aircraft flight manual supplement) for a navigation system installation and identify each required documentation element and where it must be kept in the aircraft records.	FAA aircraft certification database (rgl.faa.gov), printed TCDS examples, STC data package samples, aircraft data cards, scavenger-hunt question sheet, computers	Scavenger-hunt answers graded against instructor key with 13 of 15 correct required to pass; STC documentation checklist completed with all required elements identified.
7	14 CFR Part 91 — General Operating and Flight Rules Affecting Maintenance	50	theory	Students will identify the sections of Part 91 that directly govern maintenance requirements—including required inspections, inoperative equipment, and owner/operator responsibilities—and correctly apply them to determine an aircraft's airworthiness status.	Annotated reading of the Part 91 sections most relevant to maintenance personnel (annual inspection, 100-hour inspection, altimeter and transponder tests, ELT inspection, and RVSM requirements), with students marking each inspection interval and noting who is authorized to perform it. Airworthiness status exercise: students receive a set of aircraft logbooks and maintenance records and must determine whether the aircraft is legally airworthy for a proposed flight, citing every Part 91 section and inspection interval they check. Group debate: the class is divided into two teams and presented with a scenario where an aircraft has an inoperative piece of equipment; teams argue for and against a legal flight using Part 91.213 and the MEL framework, then the class reconciles the correct regulatory answer.	14 CFR Part 91 (current edition), sample aircraft logbooks, maintenance record packets, MEL example document, Part 91.213 decision flowchart	Airworthiness status worksheet graded for accuracy; all cited sections must be correct and the go/no-go determination must be supported by correct regulatory citation. 25-question quiz at 70% or higher.
8	14 CFR Parts 121 and 135 — Air Carrier Maintenance Programs	44	theory	Students will compare the maintenance program requirements for Part 121 air carriers and Part 135 operators with Part 91 general aviation requirements, and explain how a contract maintenance shop interacts with an air carrier's approved maintenance program.	Side-by-side comparison lecture: instructor presents a structured comparison chart of maintenance record requirements, inspection authority, and approved data requirements under Parts 91, 121, and 135; students fill in the chart as the lecture proceeds. Air carrier maintenance manual review: students read excerpts from a sample airline General Maintenance Manual (non-proprietary training copy) and identify the sections that correspond to specific regulatory requirements in Parts 121 and 135. Guest speaker or recorded interview: an A&P who works for a Part 121 or Part 135 operator describes how their daily work differs from general aviation maintenance, what their company's approved maintenance program specifies, and how FAA surveillance works; students prepare and ask at least two questions each.	14 CFR Parts 121 and 135 (current editions), sample airline General Maintenance Manual excerpts (training copy), comparison chart template, guest speaker or recorded interview	Completed comparison chart reviewed for accuracy; and a 20-question quiz covering Parts 121 and 135 maintenance requirements at 70% or higher.
9	14 CFR Part 145 — Repair Station Certification and Operations	44	theory	Students will explain the certification requirements for an FAA-certificated repair station, describe the role of the Repair Station Manual and Quality Control Manual, and state the responsibilities of the accountable manager and the certificated mechanic working under a Part 145 certificate.	Regulation walk-through: students read and annotate Part 145 subpart by subpart, using the instructor's guiding questions to identify the key requirement in each section (facility, equipment, personnel, housing, training). Manual analysis exercise: students receive excerpts from a sample Repair Station Manual and Quality Control Manual and complete a compliance checklist verifying that the sample manual addresses each Part 145 requirement; gaps are noted and discussed. Scenario discussion: the instructor presents three scenarios—a new shop applying for a Part 145 certificate, an existing station adding a new rating, and a station undergoing an FAA renewal inspection—and students identify the regulatory steps and documentation required for each.	14 CFR Part 145 (current edition), sample Repair Station Manual and Quality Control Manual excerpts, compliance checklist template, Advisory Circular AC 145-9	Compliance checklist graded for completeness and accuracy against instructor key; 80% of checklist items correctly evaluated required to pass. Short-answer quiz on Part 145 personnel and manual requirements at 70% or higher.
10	14 CFR Part 21 — Certification Procedures for Products and Articles	40	theory	Students will explain the significance of the type certificate, production approval, and airworthiness certificate in determining whether a part or product may be legally installed on a certificated aircraft, and distinguish between PMA parts, TSO articles, and unapproved parts.	Lecture and discussion covering Part 21 approval categories (TC, PC, STC, PMA, TSO, Field Approval) with emphasis on what documentation a mechanic must verify before installing a replacement part. Parts identification lab: students receive a set of actual aircraft parts or part tags representing PMA, TSO, OEM, and unmarked parts and must classify each as approved or unapproved for installation on a certificated aircraft, citing the Part 21 basis for each decision. Unapproved parts case study: students review an FAA Special Airworthiness Information Bulletin or enforcement record involving an unapproved part installation, identify the regulatory violation, and write a one-paragraph corrective action statement.	14 CFR Part 21 (current edition), sample aircraft part tags (PMA, TSO, OEM), Advisory Circular AC 21-29 (Detecting and Reporting Suspected Unapproved Parts), SAIB or enforcement record examples	Parts classification exercise scored against answer key with 90% accuracy required (safety-critical skill); 20-question quiz at 70% or higher.
11	Maintenance Documentation, Record-Keeping Systems, and Practical Record Lab	72	lab	Students will create, audit, and correct a complete set of aircraft maintenance records—including logbook entries for inspections, AD compliance, repairs, alterations, and return-to-service—meeting every content requirement of 14 CFR Part 43 and Part 91.	Record-keeping system overview and setup: students are assigned a simulated aircraft history and must establish a logbook set (airframe, engine, propeller), entering each historical event in the correct book in the correct format using sample data provided by the instructor. Audit exercise: students exchange their completed logbook sets with another student, perform a formal records audit using a structured checklist, flag any discrepancy or missing entry, and prepare a written discrepancy report citing the specific regulatory requirement violated. Correction and sign-off drill: using the flagged discrepancies from the audit, students correct their records in a legally compliant manner (no erasures, correct error-correction method, dating and initialing corrections) and make the required return-to-service entries for three simulated maintenance events.	Blank aircraft logbook sets, sample maintenance data cards with historical events, FAA Form 8130-3 samples, return-to-service entry checklist, Part 43 record-requirement summary card, red and black pens, ruler	Final logbook set assessed against master answer set; all mandatory data elements must be present in every entry (zero tolerance for missing required fields such as date, description, signature, or certificate number), and overall accuracy must be 85% or higher.
12	Regulatory Compliance Integration, Safety Culture, and FAR Exam Review	34	practice	Students will integrate knowledge from all prior lessons by working through complex, multi-regulation compliance scenarios that mirror A&P knowledge-test questions, and will demonstrate correct safety and hazard-communication practices in a maintenance regulatory context.	Integrated scenario stations: five stations each present a multi-regulation scenario (e.g., an aircraft with an open AD, a PMA part of uncertain status, and an incorrect logbook entry); students rotate through all five and must produce a written compliance determination citing each applicable regulation. A&P knowledge-test practice block: students complete two full sets of FAA-style regulatory knowledge questions under timed conditions, self-score using the FAA Airman Knowledge Test question bank, and identify their three weakest topic areas for targeted review. Safety culture discussion and OSHA HazCom refresher: instructor-led review of lockout/tagout procedures, SDS location requirements, proper PPE selection for chemical hazards common in a maintenance regulatory environment (solvents, hydraulic fluids, battery acids), connecting OSHA 29 CFR 1910.147 and HazCom Standard to the FAA safety culture framework.	Scenario station packets, FAA Airman Knowledge Test question bank (printed and/or online), answer keys, SDS examples for common shop chemicals, PPE samples (nitrile gloves, safety glasses, chemical-resistant apron), OSHA HazCom reference card	All five scenario stations completed with written regulatory citations; A&P practice block scored with results recorded to guide exam preparation. Safety walk-through observed by instructor: student must correctly identify PPE and lockout/tagout requirements for two assigned scenarios to pass the safety component.

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Federal Aviation Regulations Knowledge Examination	Written exam	25%	70% or higher (35 of 50 questions correct)	A 50-question multiple-choice examination covering all regulatory areas addressed in the course—14 CFR Parts 1, 21, 39, 43, 45, 65, 91, 119, 121, 135, and 145—using FAA A&P knowledge-test format questions. Questions are drawn from all lessons and require students to apply definitions, identify compliance requirements, and interpret regulatory text; students may use a clean copy of 14 CFR with no annotations. Standard met · Safety · Time · Quality/finish · Documentation
Regulatory Compliance Skills Demonstration	Skills demonstration	45%	All four tasks completed accurately with correct regulatory citations; no safety violations	Students complete four timed practical tasks: (1) retrieve and interpret an Airworthiness Directive for an assigned aircraft and state the compliance method; (2) examine a set of aircraft records and give a written airworthiness determination with regulatory support; (3) classify three parts as approved or unapproved with Part 21 citations; and (4) explain the privileges and at least two limitations of their A&P certificate to the evaluating instructor. Each task is scored on a pass/fail rubric; all four must be passed. Standard met · Safety · Time · Quality/finish · Documentation
Aircraft Records Lab Log	Log	15%	85% or higher on content accuracy; zero missing mandatory data elements across all entries	The cumulative logbook set produced during Lesson 11 is evaluated as the lab log. The instructor assesses every entry for compliance with 14 CFR 43.9 and 43.11 content requirements, correct AD compliance documentation, error-correction method, and completeness; each deficiency is documented on a grading rubric and returned to the student with specific regulatory citations for any error. Standard met · Safety · Time · Quality/finish · Documentation
Regulatory Safety Compliance Check	Safety audit	15%	100% on all safety-critical items; no unapproved-part installation decisions missed	A structured safety walk-through in which the instructor presents the student with two maintenance scenarios requiring PPE selection, lockout/tagout application, and identification of whether a specific part is approved for installation; the student must verbally identify every required safety control and make the correct regulatory determination on the part before being cleared to proceed to the next course. Standard met · Safety · Time · Quality/finish · Documentation

TRN-AVIA22-06 Capstone

Capstone Project: Integrated Aircraft Maintenance and Documentation

432 hr · ~~$4,320~~ COMPLIMENTARY

Students execute a comprehensive, hands-on maintenance project on an airframe/powerplant assembly, applying skills from all prior courses under realistic shop conditions. Each student produces a complete maintenance record package and defends their technical decisions before a panel, mirroring the documentation and judgment expectations of an FAA-certificated mechanic.

Outcomes

Plan and execute a multi-system aircraft maintenance task—including inspection, repair, and return-to-service actions—in compliance with applicable FAA-approved data and 14 CFR Part 43 requirements.
Complete all required maintenance records, logbook entries, and discrepancy write-ups to the standard required for a properly certificated mechanic's signature.
Demonstrate safe shop practices throughout the project, including correct use of PPE, hazardous-materials handling, and lockout/tagout procedures for each task performed.
Troubleshoot a minimum of two assigned discrepancies across different aircraft systems using manufacturer maintenance manuals, FAA Advisory Circulars, and approved troubleshooting procedures.
Apply trade mathematics—including unit conversions, torque calculations, and rigging measurements—accurately in support of each maintenance task.
Defend all maintenance decisions, logbook entries, and regulatory compliance rationale clearly and accurately in an oral examination before a faculty panel.

Course text

How the course runs. 4 blocks: Project Planning, Regulatory Framework, and Safety Baseline; Multi-System Inspection and Discrepancy Identification; Repair, Corrective Maintenance, and Approved-Data Compliance; Maintenance Documentation, Logbook Entries, and Oral Defense Preparation.

What competent looks like. Plan and execute a multi-system aircraft maintenance task—including inspection, repair, and return-to-service actions—in compliance with applicable FAA-approved data and 14 CFR Part 43 requirements. Complete all required maintenance records, logbook entries, and discrepancy write-ups to the standard required for a properly certificated mechanic's signature. Demonstrate safe shop practices throughout the project, including correct use of PPE, hazardous-materials handling, and lockout/tagout procedures for each task performed. Troubleshoot a minimum of two assigned discrepancies across different aircraft systems using manufacturer maintenance manuals, FAA Advisory Circulars, and approved troubleshooting procedures. Apply trade mathematics—including unit conversions, torque calculations, and rigging measurements—accurately in support of each maintenance task. Defend all maintenance decisions, logbook entries, and regulatory compliance rationale clearly and accurately in an oral examination before a faculty panel.

Lessons · 4 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Project Planning, Regulatory Framework, and Safety Baseline	72	theory	Given a project aircraft and a defined scope of work, the student will produce a complete work-order package—including task cards, required FAA-approved data references, parts list, and a documented safety plan—that meets 14 CFR Part 43 and Part 65 requirements before any hands-on work begins.	Review the assigned aircraft's maintenance manual, airworthiness directives, and service bulletins; identify all applicable FAA-approved data sources and list them in a formal data-reference log. Draft a written project safety plan identifying all applicable hazards (electrical, fuel, hydraulic, pneumatic, compressed gas), the required PPE for each task, and lockout/tagout procedures for each energy-isolating step. Build a sequenced task-card set for the full project scope, annotating each card with the regulatory basis (e.g., 14 CFR Part 43 Appendix A categories), estimated labor hours, required tooling, and inspection hold points.	Assigned training aircraft or approved airframe/powerplant assembly; manufacturer's maintenance manual (current revision); applicable FAA Advisory Circulars (AC 43.13-1B and AC 43.13-2B); 14 CFR Parts 43 and 65; airworthiness directive database (FAA AD portal); OSHA lockout/tagout standard reference; task-card template forms; PPE (safety glasses, gloves, hearing protection as required by task)	Instructor reviews the completed work-order package against a 20-point rubric covering accuracy of regulatory citations, completeness of parts list, correctness of LOTO procedures, and logical task sequencing; student must score 80% or higher to proceed to lab work.
2	Multi-System Inspection and Discrepancy Identification	120	lab	Using only FAA-approved data, the student will perform a structured inspection of assigned airframe, powerplant, and avionics systems, identify all discrepancies against serviceable limits, and record each finding on a standardized discrepancy log with sufficient detail to support a maintenance decision.	Conduct a systematic visual and operational inspection of airframe structural components, flight control rigging, and landing gear in accordance with the aircraft maintenance manual inspection checklist, recording actual measurements against published serviceable limits. Perform engine and engine-mount inspection tasks including compression check, oil-system inspection, and ignition-system continuity check, documenting all findings with measured values and comparing to limits specified in the type certificate data sheet and engine overhaul manual. Inspect avionics wiring, antenna installations, and instrument connections for security, chafing, and corrosion, using a calibrated multimeter to verify continuity and insulation resistance, and log all out-of-tolerance findings with wire identification and location.	Project aircraft or assembly; differential compression tester; calibrated torque wrenches (inch-pound and foot-pound ranges); multimeter (calibrated); bore scope; flashlight/inspection light; mechanic's mirror; aircraft maintenance manual; engine overhaul manual; type certificate data sheet; discrepancy log forms; safety wire; required PPE	Instructor compares student's discrepancy log against a master list of seeded discrepancies; student must correctly identify 90% of seeded faults and provide an accurate measurement or observation for each; any safety-critical discrepancy missed requires immediate remediation and re-inspection before the project continues.
3	Repair, Corrective Maintenance, and Approved-Data Compliance	168	practice	The student will correct all logged discrepancies using FAA-approved repair data and standard practices, applying trade math (torque values, drill sizing, rigging measurements, weight-and-balance adjustments) accurately, and will demonstrate correct use of tools and materials throughout each repair to achieve a return-to-service standard.	Perform sheet-metal or composite structural repair (as applicable to the assigned aircraft) following AC 43.13-1B repair data or manufacturer-approved data, selecting correct rivet type and size using trade math, drilling and countersinking to specified tolerances, and applying corrosion-inhibiting compound per the approved process. Troubleshoot and correct the two assigned powerplant or avionics system discrepancies using the manufacturer's troubleshooting guide and fault-isolation procedures; replace or adjust components as directed by the approved data, torquing all fasteners to specification using calibrated torque wrenches and documenting each step on the task card. Perform a return-to-service functional test for each corrected system—including a flight-control rigging check with measurements recorded against published tolerances and an engine run-up following the checklist—and confirm that all discrepancies are resolved and all measurements are within limits before signing off the task card.	Sheet-metal or composite repair materials (aluminum sheet, rivets, epoxy/fabric as applicable); calibrated drill press and hand drills; rivet gun and bucking bars; calibrated torque wrenches; safety wire and pliers; turnbuckles and rigging tools; engine run-up checklist; multimeter; required replacement parts (per approved parts manual); AC 43.13-1B; manufacturer repair manual; task cards; required PPE including fire extinguisher at run-up area	Instructor inspects each completed repair using the same measurement tools against published limits; torque values are spot-checked with a calibrated torque wrench; a pass requires all repairs within tolerances specified in approved data, all task cards signed with accurate entries, and no unsafe conditions present—any out-of-tolerance repair is rejected and must be redone before portfolio assembly.
4	Maintenance Documentation, Logbook Entries, and Oral Defense Preparation	72	demo	The student will compile a complete, regulation-compliant maintenance record package for all project work performed, draft the required 14 CFR Part 43 logbook entries, and present a 20-minute technical defense of their maintenance decisions and regulatory compliance to a faculty panel.	Write final logbook entries for each maintenance action performed, including the date, aircraft registration and serial number, description of work performed, reference to FAA-approved data used, airworthiness directive compliance statements where applicable, and the required mechanic certificate statement of 14 CFR Part 43.9; entries are peer-reviewed for completeness before submission. Assemble the full project portfolio in a structured binder: work order, task cards, parts traceability documentation (8130-3 or equivalent tags), calibration records for all measuring tools used, discrepancy log with disposition for every item, and final logbook entry copies—organized to allow an FAA inspector to verify compliance without additional explanation. Conduct two structured mock oral examinations with a partner using the FAA Oral and Practical Test Standards as a guide; each student questions the other on the regulatory basis for each maintenance action, the approved-data reference used, and any safety-critical decision made, then receives structured feedback from the instructor before the final defense.	Completed task cards and discrepancy logs from Lessons 2 and 3; 14 CFR Part 43 text; FAA Form 8130-3 examples; logbook entry forms (or aircraft logbooks); portfolio binder; FAA Airframe and Powerplant Oral and Practical Test Standards (current edition); instructor rubric for oral defense; projector or whiteboard for defense presentation	Logbook entries are evaluated against a checklist of all required 14 CFR Part 43.9 elements; each entry must include all required elements to pass. The oral defense is scored by two faculty members on a standardized rubric covering technical accuracy, regulatory knowledge, and communication clarity; a minimum score of 80% on the rubric and no critical safety errors in responses is required to pass the course.

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Integrated Maintenance Project	Project	60%	All repairs within published serviceable limits, 90% of seeded discrepancies correctly identified, all task cards completed with accurate entries, and no unsafe conditions found during final instructor inspection.	The hands-on project is evaluated as a whole: the instructor performs a final inspection of every repair, verifies that all discrepancies are resolved to approved-data standards, and confirms that the completed work would meet the return-to-service standard a certificated A&P mechanic would apply. Any safety-critical deficiency—an out-of-tolerance repair, a missing safety wire, or an unapproved repair method—results in a failing mark for that task, which must be remediated before the portfolio can be submitted. Meets specification · Within estimate · Workmanship · Safety · Documentation
Maintenance Documentation Portfolio	Portfolio	20%	100% of required 14 CFR Part 43.9 logbook entry elements present for every task; all discrepancies dispositioned; parts traceability documents included; portfolio organized so a reviewer can trace each task from discrepancy to repair to return-to-service without additional explanation. An overall portfolio rubric score of 80% or higher is required.	The portfolio is evaluated by the instructor using a structured rubric that checks regulatory completeness of every logbook entry, accuracy of discrepancy dispositions, correct use of FAA-approved data references, and professional organization of the document package. The portfolio directly reflects the documentation responsibility that falls on an A&P certificated mechanic under 14 CFR Part 43, and its standards mirror what an FAA Aviation Safety Inspector would review. Completeness · Organization · Evidence quality
Technical Oral Defense	Oral / panel	20%	Minimum score of 80% on the faculty rubric across all evaluation categories, with zero critical safety errors; a critical safety error (e.g., stating an unsafe or non-approved maintenance practice as correct) results in an automatic failure of the defense and requires remediation before a re-defense.	Each student presents their project to a two-person faculty panel for approximately 20 minutes, then answers unprompted questions on their maintenance decisions, the FAA-approved data they referenced, regulatory compliance rationale, and any safety-critical actions taken. The defense simulates the knowledge demonstration required of a mechanic before an FAA Designated Mechanic Examiner and directly prepares students for the oral portion of the FAA A&P practical test. Explains decisions · Answers technical questions · Professional communication

TRN-AVIA22-07 Externship / clinical

Externship / Worksite Placement in Aviation Maintenance

648 hr · ~~$2,590~~ COMPLIMENTARY

Students complete 648 supervised hours at an FAA-certificated repair station, airline maintenance base, or general aviation shop, applying airframe, powerplant, avionics, and regulatory knowledge under the direct oversight of certificated Aviation Maintenance Technicians (AMTs) and Inspection Authorized (IA) mechanics. Work is documented in a structured logbook that records task categories, supervising mechanic signatures, and reflective entries aligned to FAA A&P knowledge and skill areas. An employer evaluation at the midpoint and program end measures professional readiness, technical accuracy, and workplace conduct.

Outcomes

Perform assigned airframe and powerplant maintenance tasks under certificated AMT supervision, meeting the quality and documentation standards of the host facility's approved maintenance manual or maintenance release procedures.
Correctly complete FAA-acceptable maintenance records, work orders, and parts documentation as required by the host facility's quality-control system.
Demonstrate consistent application of personal protective equipment, lockout/tagout, hazardous-materials handling, and FOD-prevention protocols in a live shop environment.
Receive a satisfactory or above rating from the supervising employer on professional behavior, technical skill progression, and communication at both the midpoint and final employer evaluations.
Compile and submit a complete externship logbook that records each week's tasks by FAA A&P subject area, hours, and supervising mechanic signature, with reflective journal entries linking field experience to credential exam topics.
Identify at least three career development steps—such as seeking additional type ratings, pursuing IA authorization, or joining a professional aviation maintenance organization—based on site mentor guidance and self-assessment.

Course text

How the course runs. 4 blocks: Externship Orientation and Worksite Integration; Supervised Airframe and Powerplant Task Rotation; Avionics, Systems, and Regulatory Compliance Exposure; Final Evaluation, Logbook Completion, and Career Reflection.

What competent looks like. Perform assigned airframe and powerplant maintenance tasks under certificated AMT supervision, meeting the quality and documentation standards of the host facility's approved maintenance manual or maintenance release procedures. Correctly complete FAA-acceptable maintenance records, work orders, and parts documentation as required by the host facility's quality-control system. Demonstrate consistent application of personal protective equipment, lockout/tagout, hazardous-materials handling, and FOD-prevention protocols in a live shop environment. Receive a satisfactory or above rating from the supervising employer on professional behavior, technical skill progression, and communication at both the midpoint and final employer evaluations. Compile and submit a complete externship logbook that records each week's tasks by FAA A&P subject area, hours, and supervising mechanic signature, with reflective journal entries linking field experience to credential exam topics. Identify at least three career development steps—such as seeking additional type ratings, pursuing IA authorization, or joining a professional aviation maintenance organization—based on site mentor guidance and self-assessment.

Lessons · 4 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Externship Orientation and Worksite Integration	48	field	The student will successfully complete host-facility onboarding, safety induction, and quality-system orientation, and begin logging supervised maintenance tasks in the externship logbook with no missing entries.	Attend and document the host facility's new-employee or contractor safety orientation, including emergency procedures, FOD walk protocols, and facility-specific PPE requirements; record completion in the externship logbook with supervisor signature. Meet with the assigned supervising AMT to review the externship task plan, select initial work assignments matched to the student's current skill level, and clarify how maintenance records and discrepancy logs are written at the site. Complete the first weekly logbook entry: list each task attempted, the applicable FAA A&P subject area (e.g., Airframe Structures, Powerplant Fuel Systems), hours spent, outcome (observed, assisted, or performed), and supervising mechanic signature.	Host facility safety and operations manual, facility-issued PPE (hearing protection, safety glasses, gloves as required), externship logbook (school-issued form with AMT signature blocks), FAA Advisory Circular AC 65-2 (Airframe and Powerplant Mechanics Certification Guide) for subject-area mapping reference.	Supervisor confirms student completed facility onboarding and can locate emergency exits, first-aid stations, and MSDS/SDS binders; externship logbook Week 1 entry is complete with no blank fields and carries supervising mechanic signature. Pass = zero missing required fields and supervisor sign-off on orientation checklist.
2	Supervised Airframe and Powerplant Task Rotation	300	lab	The student will perform a rotating series of supervised airframe and powerplant maintenance tasks—spanning inspection, component removal and installation, rigging, and run-up support—with quality and documentation meeting shop standards on at least 80% of assigned tasks.	Rotate through at least four distinct work areas (e.g., sheet-metal and structural repair, flight-control rigging, engine change or cylinder overhaul support, fuel and oil system servicing) under direct AMT supervision, recording each task in the logbook with task category, applicable maintenance manual section, hours, and result. Practice completing maintenance release entries or work-order sign-offs under supervising AMT oversight, cross-checking that part numbers, serial numbers, and airworthiness directive compliance notes match the aircraft log or work card before the AMT countersigns. After each two-week rotation block, conduct a 15-minute debrief with the supervising AMT to identify one skill area for improvement, one area of strength, and one FAA A&P exam topic the field experience reinforced; record debrief notes in the reflective journal section of the logbook.	Aircraft maintenance manuals (AMM) and component maintenance manuals (CMM) for aircraft types operated by the host facility, calibrated torque wrenches, safety-wire pliers, inspection mirrors, borescope (if available), PPE as specified by task, externship logbook, host facility work-order forms.	Midpoint employer evaluation form completed by supervising AMT at approximately 180 hours; student scores Satisfactory or above on technical accuracy, safe work habits, and documentation quality. Logbook entries for the period are complete, signed, and correctly categorized by A&P subject area. Pass = Satisfactory or above on all three midpoint evaluation dimensions and 100% logbook entry completion rate.
3	Avionics, Systems, and Regulatory Compliance Exposure	200	field	The student will assist certificated technicians with avionics-related tasks, aircraft system inspections, and regulatory paperwork—including airworthiness directive research and 100-hour or annual inspection support—documenting each activity with the correct FAA subject-area tag in the externship logbook.	Shadow avionics technicians performing navigation, communication, or instrument system checks; assist with wire-bundle inspection, connector cleaning, or placard replacement as authorized, and record observations using correct avionics subject-area tags (e.g., Aircraft Instruments, Communications and Navigation Systems). Under AMT supervision, use the FAA Airworthiness Directives database (FAA.gov) to look up applicable ADs for an aircraft in the shop, verify compliance status against the aircraft records, and note any discrepancy or upcoming compliance due date on a shop form reviewed and signed by the supervising AMT. Participate in a 100-hour or annual inspection walk-through: follow the approved inspection checklist, record discrepancies on the squawk sheet, and observe how the AMT or IA documents findings in the aircraft maintenance record; write a reflective journal entry linking the inspection sequence to FAA 14 CFR Part 43 requirements discussed in Course 5.	FAA Airworthiness Directives database access (computer or tablet), host facility approved inspection checklists, aircraft logbooks and maintenance records, multimeter or avionics test set as authorized by supervisor, externship logbook, 14 CFR Part 43 reference copy.	Student correctly identifies and documents at least one AD compliance check under AMT oversight, with no errors in the aircraft record entry (AMT countersigns); reflective journal entry for the inspection experience references at least two regulatory requirements by name. Pass = zero documentation errors on countersigned entries and a reflective entry of at least 200 words that correctly names relevant regulatory requirements.
4	Final Evaluation, Logbook Completion, and Career Reflection	100	field	The student will finalize all logbook entries, receive and discuss the employer's final evaluation, and produce a written career action plan that uses site-mentor feedback and A&P exam subject-area gap analysis to set three specific post-graduation professional development goals.	Audit the complete externship logbook with the supervising AMT: verify that every week's entries are present, correctly categorized by FAA A&P subject area, signed, and that total hours meet the 648-hour requirement; correct any missing entries before the final employer evaluation meeting. Participate in the formal final employer evaluation meeting with the supervising AMT or facility manager, who completes the school's Final Employer Evaluation Form covering technical skill level, reliability and professionalism, safety practices, and readiness for entry-level employment; discuss ratings openly and ask for specific improvement feedback. Using feedback from the employer evaluation and a self-scored gap analysis of FAA A&P subject areas (matched against the logbook's task distribution), write a two-page career action plan identifying three professional development goals with specific actions, target timelines, and resources (e.g., seeking IA authorization after two years of experience, joining the Aviation Technician Education Council network, completing a specific avionics type-rating course).	Complete externship logbook, school Final Employer Evaluation Form, FAA A&P subject-area checklist (mapped from AC 65-2), word processor or notebook for career action plan, any professional organization membership information provided by site mentor.	Final employer evaluation score of Satisfactory or above on all dimensions; logbook audit confirms 648 hours logged, all entries signed, and tasks distributed across at least five distinct FAA A&P subject areas; career action plan submitted and reviewed by school program coordinator. Pass = Satisfactory or above on final evaluation, 100% logbook completion, and a career action plan accepted by the program coordinator as specific and actionable.

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Employer Skills Demonstration Evaluation	Skills demonstration	70%	Satisfactory or above on all rated dimensions of both the midpoint and final Employer Evaluation Forms, with no dimension rated Unsatisfactory on the final evaluation.	The supervising AMT or facility manager completes the school's standardized Employer Evaluation Form at the midpoint (approximately 324 hours) and at program end (648 hours), rating the student on technical task performance, safe work habits, documentation accuracy, and professional conduct. Ratings are discussed face-to-face with the student, and the signed forms are submitted to the program coordinator as the primary skills demonstration record. Competency · Safety · Attendance · Conduct · Initiative
Externship Logbook and Reflective Journal	Log	30%	100% of weekly entries present and AMT-signed, tasks distributed across at least five FAA A&P subject areas, reflective journal entries averaging at least 150 words per two-week block, and career action plan accepted by the program coordinator.	The student's externship logbook serves as the official record of all 648 field hours, capturing task descriptions, subject-area classifications, supervising mechanic signatures, and weekly hour totals, alongside a reflective journal section that links field activities to FAA A&P knowledge areas and regulatory requirements covered in earlier courses. The program coordinator audits the complete logbook at submission, checking for completeness, legibility, correct subject-area tagging, and the quality of reflective entries and the final career action plan. Complete · Verified

TRN-AVIA22-08 Exam prep

FAA A&P Certification Exam Preparation

180 hr · ~~$1,800~~ COMPLIMENTARY

This 180-hour course systematically reviews every subject area tested on the FAA Aviation Mechanic written, oral, and practical tests for both the Airframe and Powerplant ratings, using timed mock written exams, oral questioning drills, and hands-on practical project stations. Learners diagnose their individual weak areas through data-driven score analysis and target remediation before sitting the actual FAA tests. The course closes with full-length simulated exams and an examiner-style oral and practical session to build the confidence and procedural fluency required to pass all three test components.

Outcomes

Achieve a score of 80% or higher on timed full-length FAA-format written practice tests for both the Airframe and Powerplant subject areas.
Correctly respond to oral questioning on the FAA Airframe and Powerplant Oral and Practical Standards (ACS) subject areas with examiner-acceptable depth and accuracy.
Demonstrate safe, correct completion of practical project tasks drawn from the FAA Airframe and Powerplant ACS task lists, meeting all quality and documentation standards.
Identify personal knowledge gaps through score analysis and complete targeted remediation using FAA-approved references including 14 CFR Part 65, FAA-H-8083 series handbooks, and applicable Advisory Circulars.
Locate, interpret, and apply manufacturer maintenance manuals, airworthiness directives, and FAA-approved data during simulated oral and practical test scenarios.
Complete all required pre-test documentation accurately, including FAA Form 8610-2, and explain the eligibility requirements under 14 CFR Part 65 for the Aviation Mechanic certificate.

Course text

How the course runs. 4 blocks: Diagnostic Assessment and Written Test Fundamentals; Oral Test Preparation — ACS Knowledge and Judgment Areas; Practical Project Stations — ACS Task Performance; Full Mock FAA Written, Oral, and Practical Examinations.

What competent looks like. Achieve a score of 80% or higher on timed full-length FAA-format written practice tests for both the Airframe and Powerplant subject areas. Correctly respond to oral questioning on the FAA Airframe and Powerplant Oral and Practical Standards (ACS) subject areas with examiner-acceptable depth and accuracy. Demonstrate safe, correct completion of practical project tasks drawn from the FAA Airframe and Powerplant ACS task lists, meeting all quality and documentation standards. Identify personal knowledge gaps through score analysis and complete targeted remediation using FAA-approved references including 14 CFR Part 65, FAA-H-8083 series handbooks, and applicable Advisory Circulars. Locate, interpret, and apply manufacturer maintenance manuals, airworthiness directives, and FAA-approved data during simulated oral and practical test scenarios. Complete all required pre-test documentation accurately, including FAA Form 8610-2, and explain the eligibility requirements under 14 CFR Part 65 for the Aviation Mechanic certificate.

Lessons · 4 blocks

#	Lesson	Hr	Type	Objective	Activities	Materials	Check
1	Diagnostic Assessment and Written Test Fundamentals	40	practice	Learners will complete a baseline diagnostic written test for each rating, analyze their scores by subject area, and build a personal remediation plan targeting any area below 80%.	Complete a full-length timed diagnostic practice written test (150 questions, Airframe) and a full-length diagnostic practice written test (150 questions, Powerplant) under simulated FAA computer testing conditions, with answers drawn from the current FAA Airmen Knowledge Test question bank. Use a score-analysis worksheet to sort missed questions by ACS subject category (e.g., mathematics, weight and balance, aircraft systems, powerplant theory, regulations), calculate a percentage score per category, and flag any category below 80% for a written remediation plan with specific FAA handbook page references. Conduct three additional timed practice written sessions per rating across the lesson block, reviewing every incorrect answer against the source FAA-H-8083 handbook chapter or 14 CFR section immediately after each session and recording corrections in a personal error log.	FAA Airmen Knowledge Testing Supplement (CT-8080 series for Airframe and Powerplant), current FAA Airmen Knowledge Test question bank (printed or approved test-prep software), FAA-H-8083-2 (Weight and Balance), FAA-H-8083-30 (General Handbook), FAA-H-8083-31 (Airframe Handbook), FAA-H-8083-32 (Powerplant Handbook), 14 CFR Parts 43 and 65, personal error-log notebook, calculator.	Learner produces a written remediation plan listing every sub-category scored below 80% with specific reference citations; end-of-lesson practice test score for each rating is recorded; instructor reviews plan for completeness. Pass mark: remediation plan accepted as complete by instructor; at least one full-length practice test per rating completed and scored.
2	Oral Test Preparation — ACS Knowledge and Judgment Areas	45	demo	Learners will accurately answer examiner-style oral questions across all ACS knowledge areas for both the Airframe and Powerplant ratings, demonstrating the ability to locate supporting references when unable to answer from memory.	Participate in structured peer oral-questioning pairs using the FAA Aviation Mechanic ACS task lists as the question guide; each learner takes turns in the role of applicant and questioner for 30-minute rotations covering aircraft structures, systems, instruments, engines, fuel systems, ignition systems, and regulations, recording any question answered incorrectly or incompletely for follow-up. Attend instructor-led panel oral drills in groups of four, with the instructor playing the role of a Designated Mechanic Examiner (DME); instructor asks open-ended ACS oral questions, interrupts to probe depth of understanding, and models the technique of answering 'I do not know from memory, but I would refer to [specific manual or regulation]' when appropriate, so learners practice acceptable reference-use responses. Complete a written self-assessment after each oral drill session, rating personal confidence on each ACS subject area on a 1–4 scale and identifying three specific topics to re-study in the FAA-H-8083 series handbooks or applicable ADs before the next session.	FAA Aviation Mechanic — Airframe and Powerplant Airman Certification Standards (ACS) document, FAA-H-8083-31 (Airframe Handbook), FAA-H-8083-32 (Powerplant Handbook), FAA-H-8083-30 (General Handbook), 14 CFR Part 43 and Part 65, applicable manufacturer maintenance manuals available in the classroom, oral question card decks organized by ACS area, self-assessment rating forms.	Instructor evaluates each learner during at least two panel oral drills using an ACS-aligned rubric scoring accuracy, depth, and appropriate reference use; learners must demonstrate acceptable responses (accurate or correctly redirected to source) on at least 80% of questions posed across all ACS subject areas. Pass mark: 80% acceptable response rate on instructor-scored oral drill rubric.
3	Practical Project Stations — ACS Task Performance	65	lab	Learners will safely and correctly perform hands-on maintenance tasks drawn from the FAA Airframe and Powerplant ACS practical task lists, completing all required maintenance record entries to airworthy standards.	Rotate through a series of practical project stations set up to replicate FAA practical test tasks, including: sheet metal repair and inspection, control cable rigging and tension measurement, aircraft fabric inspection, reciprocating engine cylinder compression test, magneto timing check, carburetor removal and installation, spark plug inspection and gapping, fuel system component inspection, hydraulic system servicing, and landing gear operational check — each station specifies the applicable ACS task reference, and learners complete the task independently while an instructor or qualified peer evaluates performance against the ACS pass/fail criteria. For each completed station task, learners write a simulated maintenance record entry on a blank FAA Form 337 or a general maintenance logbook entry form as appropriate, including the work performed, the data used (manual title, revision, and page), the part numbers and materials used, the return-to-service statement, and the mechanic's signature block — entries are reviewed by the instructor for regulatory accuracy per 14 CFR Part 43. Complete a minimum of two full-cycle practical scenario exercises in which the instructor presents a simulated aircraft squawk (discrepancy), the learner performs the troubleshooting sequence using the manufacturer maintenance manual, carries out the corrective action at a station, and presents the completed work and documentation to the instructor acting as the DME for a final accept/reject decision.	Training airframe (or representative airframe section), training reciprocating engine or engine trainer, sheet metal tools (rivet gun, bucking bars, drills, dimple dies), fabric inspection tools, compression tester, timing light, spark plug gap gauge and cleaner, cable tension meter (tensiometer), torque wrenches (inch-pound and foot-pound), safety wire pliers, hydraulic service equipment, multimeter, applicable manufacturer maintenance manuals, FAA Form 337 blank copies, maintenance logbook entry forms, PPE (safety glasses, hearing protection, chemical-resistant gloves as task requires), LOTO equipment, FAA-H-8083-31 and -32.	Instructor scores each station task on an ACS-aligned practical evaluation form with go/no-go criteria matching those a DME would apply; maintenance record entries are graded for regulatory completeness; learners must earn a 'go' rating on at least 80% of all stations attempted, with any safety-of-flight critical error resulting in immediate station failure and mandatory repeat. Pass mark: 80% or higher go-rating across all stations; zero uncorrected safety-critical errors.
4	Full Mock FAA Written, Oral, and Practical Examinations	30	practice	Learners will complete a full simulated FAA Aviation Mechanic examination sequence — written, oral, and practical — for both the Airframe and Powerplant ratings under realistic test conditions and use final score feedback to confirm readiness or complete last-cycle remediation.	Sit a full-length, strictly timed mock written test for the Airframe rating (150 questions, 3-hour limit) and the Powerplant rating (150 questions, 3-hour limit) administered under FAA testing conditions (no reference materials, no interruptions, single sitting per rating), scored immediately after submission with missed items mapped back to ACS subject areas for final gap analysis. Undergo a 45-minute full mock oral examination per rating conducted by the instructor or an invited industry professional acting as DME, using the ACS oral task list to select questions unpredictably across subject areas, with the session recorded (audio or written notes) so the learner can review any marginal answers and confirm final readiness. Complete a mock practical examination per rating in which the examiner selects three to five ACS practical tasks at random from a task card set, the learner performs each task at the appropriate station with no coaching, writes all required maintenance documentation, and receives a pass/fail decision with a written debrief listing any discrepancies; learners who do not pass any element complete one additional targeted remediation session and a focused re-check before the course closes.	FAA Airmen Knowledge Testing Supplement (CT-8080 series), current FAA question bank (test-prep software in exam mode), ACS task card set, all practical station equipment from Lesson 3, blank maintenance record forms, FAA Form 8610-2 (completed by learner as part of session orientation), stopwatch/timer, DME evaluation score sheets, audio recorder (optional), 14 CFR Part 65 for eligibility review.	Written mock tests scored automatically and reported by ACS subject area; oral examination scored on DME evaluation sheet with pass defined as no unsatisfactory ACS area; practical examination scored go/no-go per task. Overall pass standard for this lesson: 70% or higher on each mock written test (FAA minimum is 70%; the program targets higher, but this final mock uses the actual FAA passing score to confirm baseline readiness), no unsatisfactory oral area, and go on all mock practical tasks. Instructor documents final readiness recommendation for each learner.

Assessments

Assessment	Type	Weight	Pass standard	Method & rubric
Full FAA A&P Mock Certification Examination (Airframe and Powerplant)	Mock certification exam	100%	Written component: minimum 70% on each rating test (matching the FAA passing standard), with program target of 80% or higher documented; Oral component: no unsatisfactory rating in any ACS subject area across either rating; Practical component: go on all selected ACS tasks for both ratings with zero uncorrected safety-critical errors and all maintenance documentation accepted as regulatory-compliant.	This cumulative mock examination replicates the full FAA Aviation Mechanic certification test sequence for both the Airframe and Powerplant ratings: a timed written test, a DME-style oral examination, and a multi-task practical examination, all scored against FAA ACS standards. Learners who do not meet the passing standard on any component complete a structured remediation cycle and a focused re-examination of that component before the course ends, ensuring every graduate is documented as examination-ready prior to scheduling their official FAA tests. Score · Time management

Program completion

External credential: FAA A&P

Students sit the FAA Airframe and Powerplant (A&P) mechanic certification examinations, which consist of written knowledge tests, oral tests, and practical skill tests administered by FAA-designated Aviation Maintenance Technician Examiners (DAMTEs). Pass standard: Credential issued by the body.

Back to Aviation Maintenance · How the school gets authority to award these credentials