🚧 Under construction — VoTechWorks is being built. A free tech program — complimentary, as our commitment to get America working.
voTechWorksGrade 13 · a vocational technology learning center, by urbanicity
newSchoolWorks.com › VoTechWorks › Transportation › Aviation Maintenance › Airframe Systems and Structures › Lesson 11
TRN-AVIA22-02 · Lesson 11 · 60 clock hours · field

Aircraft Inspections, Airworthiness, and Documentation

Objective. 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.

⚠ Pending professional review

This lesson, its worked examples and its practice questions 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.

Why Inspections Matter

An aircraft is only legally airworthy when it meets its type design and is in a condition for safe operation. The 100-hour inspection is one of the primary scheduled maintenance events that keeps general aviation aircraft in that condition. Under 14 CFR Part 91, aircraft operated for hire or flight instruction must receive a 100-hour inspection every 100 hours of flight time. The mechanic who performs and signs off that inspection takes on direct regulatory responsibility for the work. Understanding how to conduct the inspection systematically, classify findings correctly, and document everything completely is a core FAA A&P competency.

Safety Before You Begin

Before touching the aircraft, conduct a proper hazard assessment. Don appropriate PPE: safety glasses, nitrile gloves when handling fluids or cleaning agents, and hearing protection if engines will be run. Chock the wheels and verify the master switch and ignition are off. If any fuel or hydraulic lines will be opened, have absorbent material ready and know the location of the nearest fire extinguisher. Apply a DO NOT OPERATE placard to the cockpit and, where applicable, use lockout/tagout procedures on any circuit breakers or switches that could energize a system you are inspecting. Never assume a system is de-energized — verify it.

The Inspection Checklist and AMM

A 100-hour inspection follows the scope and detail of an annual inspection (14 CFR Part 43 Appendix D lists the minimum areas to examine). In practice, you work from the aircraft manufacturer's Aircraft Maintenance Manual (AMM), which provides model-specific procedures, tolerances, and limits. The school-issued checklist is aligned with the AMM so nothing is skipped. Work through the checklist in sequence — engine compartment, airframe exterior, flight controls, landing gear, interior, instruments, avionics, and required documents. For each line item, record one of three conditions:

Record actual measurements (wear limits, torque values, gap measurements) wherever the checklist calls for them. A note saying "OK" without data is not acceptable for items that require a measurement.

Using AC 43.13-1B

Advisory Circular 43.13-1B, Acceptable Methods, Techniques, and Practices — Aircraft Inspection and Repair, is your field reference when the AMM does not specify a repair method. It is not mandatory in itself, but methods it describes are FAA-accepted as airworthy practice. When writing corrective actions for discrepancies, cite the specific chapter and section of the AMM or the applicable AC 43.13-1B reference so anyone reading the record knows exactly what authority was used.

Building the Discrepancy List

Every item that is not airworthy at the time of inspection goes on the discrepancy list — a formal document separate from the checklist. Each entry must include:

1. Description of the discrepancy (what, where, measured value vs. limit).

2. Airworthiness classification (repairable or unairworthy).

3. Corrective action planned, with the AMM, AC, or regulatory reference.

4. Priority: unairworthy items go to the top because they prevent return to service.

Organize the list so the supervising A&P and the aircraft owner can see at a glance which items ground the aircraft and which are maintenance items to be corrected before the next flight.

Completing the 14 CFR Part 43 Appendix D Logbook Entry

Part 43 Appendix B specifies what a maintenance record entry must contain, and Appendix D describes the scope of a 100-hour/annual inspection. Your logbook entry for the 100-hour inspection must include:

If the aircraft cannot be returned to service, you still sign the logbook but record that a discrepancy list has been furnished to the owner per 14 CFR Part 43. You do not write a return-to-service approval until all unairworthy items are corrected.

Return-to-Service Approval

Once all discrepancies are resolved, the approving A&P (or IA for an annual) makes a return-to-service entry. This entry references the previous inspection entry, lists the corrective actions taken, cites the authority used, and includes the mechanic's signature and certificate number. Incomplete, vague, or missing entries are among the most common FAA compliance findings — precision in paperwork is as important as precision with a torque wrench.

Common Mistakes to Avoid

Key terms9

100-Hour InspectionA scheduled maintenance inspection required by 14 CFR Part 91 for aircraft operated for compensation or hire; scope is identical to an annual inspection but may be performed by any certificated A&P mechanic.
AirworthinessThe condition of an aircraft when it conforms to its type design and is in a condition for safe operation, as defined under 14 CFR.
Discrepancy ListA formal written record of all inspection findings that are not airworthy at the time of inspection, including a description, classification, and planned corrective action for each item.
Return-to-Service EntryA logbook entry made by an authorized mechanic or inspector that approves an aircraft for return to operation after maintenance or inspection; required by 14 CFR Part 43.
14 CFR Part 43The federal regulation governing maintenance, preventive maintenance, rebuilding, and alteration of civil aircraft; includes requirements for record entries and the scope of inspections.
AC 43.13-1BFAA Advisory Circular providing acceptable methods, techniques, and practices for aircraft inspection and repair; widely used as a reference when the AMM does not specify a particular method.
Aircraft Maintenance Manual (AMM)The manufacturer's official document specifying maintenance procedures, tolerances, limits, and inspection requirements for a specific aircraft model.
Appendix D (Part 43)The section of 14 CFR Part 43 that defines the minimum scope and detail required for a 100-hour or annual inspection, listing the areas and systems that must be examined.
Certificate NumberThe FAA-issued identification number on an A&P mechanic's certificate that must appear on every maintenance record entry the mechanic signs.

Worked examples4

1. During a brake disk inspection, the AMM lists the minimum allowable disk thickness as 0.188 inches. Your caliper measurement reads 0.174 inches. How do you classify this finding and what measurement data must appear on the discrepancy list?
  1. Record the measured value: 0.174 in.
  2. Compare to the AMM minimum limit: 0.188 in.
  3. Calculate the difference: 0.188 − 0.174 = 0.014 in. below the minimum limit.
  4. Because the disk is below the minimum allowable thickness, the condition prevents safe operation — classify as Unairworthy.
  5. Enter on the discrepancy list: 'Left main brake disk measured 0.174 in.; AMM minimum limit 0.188 in. (0.014 in. below limit). Unairworthy. Corrective action: Replace brake disk per AMM [chapter/section].'
Answer: Unairworthy — measured thickness (0.174 in.) is 0.014 in. below the AMM minimum (0.188 in.); disk must be replaced before return to service, and the discrepancy list must show both the measured value and the AMM limit.
2. A tire sidewall shows a small surface crack that does not extend into the cords. The AMM states surface cracks not exposing cord are acceptable. What classification applies and why?
  1. Inspect the crack and confirm it does not expose the cord fabric — use a flashlight and mirror if needed.
  2. Compare the finding to the AMM acceptance criterion: surface cracks not reaching cord are acceptable.
  3. Since the condition meets the AMM acceptance standard, classify the tire as Airworthy.
  4. Record on the checklist: 'Nose tire — surface crack noted, cord not exposed, within AMM limits — Airworthy.' No discrepancy list entry required.
Answer: Airworthy — the crack meets the AMM acceptance criterion; no discrepancy list entry is required, but the finding must still be noted on the inspection checklist with a description.
3. A spark plug gap measures 0.021 inches. The AMM specifies a gap range of 0.015 to 0.018 inches. By how many thousandths is the plug out of tolerance, and how should this be classified?
  1. Identify the upper limit: 0.018 in.
  2. Subtract the upper limit from the measured gap: 0.021 − 0.018 = 0.003 in. above the maximum.
  3. The plug gap is 3 thousandths of an inch over the maximum allowable.
  4. The plug can be re-gapped to within limits — classify as Repairable.
  5. Record on the discrepancy list: 'No. X cylinder spark plug gap measured 0.021 in.; AMM limit 0.015–0.018 in. Repairable. Corrective action: Re-gap to 0.016 in. per AMM.'
Answer: Repairable — the gap is 0.003 in. over the AMM maximum; the plug can be re-gapped to within the specified 0.015–0.018 in. range before return to service.
4. You have completed a 100-hour inspection. The aircraft total time is 1,247.3 hours. All discrepancies have been corrected. List the required data elements for the logbook entry.
  1. Date of completion of the inspection.
  2. Aircraft total time in service: 1,247.3 hours.
  3. A description of the work: 'Performed 100-hour inspection in accordance with 14 CFR Part 43 Appendix D and [AMM reference].'
  4. Statement that the aircraft was found to be in airworthy condition (since all discrepancies are resolved).
  5. Name of the person who performed the work.
  6. Certificate type (Airframe and Powerplant) and certificate number of the approving mechanic.
  7. Signature of the approving mechanic.
Answer: The logbook entry must include the date, aircraft total time (1,247.3 hrs), description of inspection scope and authority, airworthy-condition statement, the mechanic's name, certificate type and number, and signature — all required by 14 CFR Part 43.
In class: 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.
Materials: 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
Check: 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

Practice check8

Answer each question, then check it. Nothing is recorded; this is your own practice.

Regulations
1. Which regulation specifies the minimum scope and detail required for a 100-hour inspection?
Inspection Concepts
2. During a 100-hour inspection, you find a flight control cable whose measured diameter is below the AMM minimum allowable limit. How should this item be classified?
Regulations
3. If a 100-hour inspection is completed but one item remains unairworthy, what must the mechanic do regarding the logbook?
Maintenance Publications
4. AC 43.13-1B is best described as:
Regulations
5. Which of the following is a required element of a maintenance record entry under 14 CFR Part 43?
Powerplant Inspection
6. A spark plug is removed and its gap measures 0.013 inches. The AMM specifies a gap range of 0.015 to 0.018 inches. What is the correct classification and action?
Safety
7. Before beginning a 100-hour inspection that involves opening fuel lines, which safety action is most important?
Documentation
8. A discrepancy list entry must include which of the following to be considered complete?
Record this lesson on my transcript. Sign in with your key and enrollment email to record lessons (enroll free if you have no key). This page stays open to read and practise.