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newSchoolWorks.com › VoTechWorks › Transportation › Aviation Maintenance › Federal Aviation Regulations for Aviation Maintenance › Lesson 10
TRN-AVIA22-05 · Lesson 10 · 40 clock hours · theory

14 CFR Part 21 — Certification Procedures for Products and Articles

Objective. 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.

⚠ 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.

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Why Part 21 Matters to a Mechanic

14 CFR Part 21 establishes the certification procedures for all civil aeronautical products and articles sold or installed in the United States. As a mechanic, you are personally responsible for knowing whether a part is legally approved before you install it. Installing an unapproved part on a certificated aircraft can ground the aircraft, expose you to certificate action, and — most critically — create an unsafe condition that may not reveal itself until flight. Part 21 is the regulatory foundation that answers the question: Is this part legal to install?

The Type Certificate (TC)

A Type Certificate is issued by the FAA to the designer of an aircraft, aircraft engine, or propeller. It confirms that the design meets all applicable airworthiness standards. The TC data sheet lists the approved configuration: approved engine models, operating limitations, required equipment, and more. When you install a replacement part, that part must conform to the type design documented in the TC. The TC holder is typically the original equipment manufacturer (OEM). Parts manufactured under the TC holder's quality system are called OEM parts and carry the TC holder's part number.

Production Approvals: PC and PMA

A Production Certificate (PC) authorizes a TC holder to manufacture duplicate products that conform to the approved type design. It demonstrates that the manufacturer has a quality system capable of producing consistent, airworthy products.

A Parts Manufacturer Approval (PMA) is a combined design and production approval issued by the FAA to a company other than the TC holder. A PMA part has been independently approved and may legally replace the corresponding OEM part. PMA parts must be marked with the manufacturer's name, part number, and the letters "FAA-PMA." When you receive a PMA part, verify that marking is present and that the part number matches the aircraft's parts catalog or maintenance manual. Missing or altered markings are a red flag.

Technical Standard Orders (TSO)

A TSO authorization allows a manufacturer to produce articles — typically appliances and components such as altimeters, life vests, or transponders — that meet a specific FAA-accepted minimum performance standard. A TSO article is marked with the TSO number (for example, TSO-C119 for TCAS equipment). TSO authorization alone does not automatically approve an article for installation on a specific aircraft; you must also confirm that the aircraft's TC or an STC permits that article in that position. Think of the TSO as a quality floor — it proves the article meets a standard, but the mechanic still must verify it is the correct article for the aircraft.

Supplemental Type Certificates (STC)

An STC approves a modification or alteration to an existing type-certificated product. If an operator wants to install a new avionics system or a different engine model, the STC documents the approved design change. As a mechanic performing STC work, you must have the STC data sheet and the associated maintenance or installation instructions in hand before starting work. Parts called out in the STC are approved only in conjunction with that STC.

Field Approvals

A field approval is granted by an FAA Aviation Safety Inspector and allows a specific major repair or alteration on a specific aircraft when no existing DER-approved data covers the work. The approval is recorded on an FAA Form 337. Field approvals are aircraft-specific; the data does not transfer to another aircraft without a new approval.

Unapproved Parts — A Safety and Legal Hazard

An unapproved part is any part that has not been produced under an FAA production approval (TC/PC, PMA, or TSO) or that cannot be shown to conform to an approved design through acceptable documentation. Unapproved parts enter the supply chain through counterfeit manufacturing, improper salvage operations, or paperwork fraud. Advisory Circular AC 21-29 provides detailed guidance on detecting and reporting suspected unapproved parts (SUPs).

Key warning signs include:

If you suspect a part is unapproved, do not install it. Quarantine the part, document your findings, and report to your supervisor and, if appropriate, to the FAA's Suspected Unapproved Parts Program. Attempting to install a known unapproved part is a violation of 14 CFR Part 21 and may also violate Part 43 and Part 65, risking your A&P certificate.

What to Verify Before Installation

Before installing any replacement part, confirm all of the following:

1. The part has a valid production approval — OEM (TC/PC), PMA, or TSO as appropriate.

2. Part markings are present, legible, and match the paperwork.

3. An airworthiness release document (FAA Form 8130-3 or equivalent) accompanies the part.

4. The part number matches what is called out in the aircraft maintenance manual, illustrated parts catalog, or applicable STC/field approval data.

5. The part has not been altered or shows no signs of damage or improper repair.

This verification process is not optional. It is a direct regulatory duty under Part 43 and Part 65, and it begins with understanding the Part 21 approvals described in this lesson.

Key terms8

Type Certificate (TC)FAA approval issued to the designer of an aircraft, engine, or propeller confirming the design meets applicable airworthiness standards; the TC data sheet defines the approved configuration.
Production Certificate (PC)FAA authorization allowing a TC holder to manufacture products that duplicate the approved type design, demonstrating the manufacturer maintains an acceptable quality system.
Parts Manufacturer Approval (PMA)A combined FAA design and production approval granted to a manufacturer other than the TC holder, authorizing production of replacement or modification parts for certificated products; PMA parts must be marked 'FAA-PMA.'
Technical Standard Order (TSO)A minimum performance standard issued by the FAA for specific aeronautical articles; a TSO authorization allows a manufacturer to produce and mark articles to that standard, but installation approval on a specific aircraft must still be established.
Supplemental Type Certificate (STC)FAA approval documenting an alteration or modification to an existing type-certificated product; the STC holder's data sheet and instructions govern parts and procedures for that modification.
Unapproved Part (SUP — Suspected Unapproved Part)Any part that lacks valid FAA production approval documentation or cannot be shown to conform to an approved design; installing such a part on a certificated aircraft is a regulatory violation.
FAA Form 8130-3Airworthiness Approval Tag used to release new parts from production approval holders or to document return-to-service of parts from certificated repair stations; it accompanies parts as evidence of airworthiness.
Field ApprovalAircraft-specific approval granted by an FAA Aviation Safety Inspector for a major repair or alteration when no previously approved data exists; documented on FAA Form 337 and not transferable to other aircraft.
In class: 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.
Materials: 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
Check: Parts classification exercise scored against answer key with 90% accuracy required (safety-critical skill); 20-question quiz at 70% or higher.

Practice check8

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

Regulations
1. A mechanic receives a replacement alternator for a certificated light aircraft. The part tag shows a part number, the manufacturer's name, and the marking 'FAA-PMA.' Under 14 CFR Part 21, this marking indicates the part:
Regulations
2. Before installing a replacement transponder on a certificated aircraft, a mechanic notes the unit carries a TSO marking. What additional verification is required?
Regulations
3. Which document would a mechanic expect to accompany a new aircraft part shipped from a Parts Manufacturer Approval holder as evidence of airworthiness?
Safety
4. A mechanic discovers a bag of fasteners in the stockroom. The fasteners have no markings, no accompanying paperwork, and no record of their origin. Under Part 21 and AC 21-29, the correct action is to:
Regulations
5. An operator wants to install a satellite weather display system that is not listed in the aircraft's original TC data sheet. The modification has been designed and approved by a third party. What Part 21 approval would cover this installation?
Regulations
6. A field approval for a major alteration on a specific Cessna 172 is documented on an FAA Form 337. A mechanic wants to perform the identical alteration on a different Cessna 172 with the same serial configuration. Which statement is correct?
Safety
7. Which of the following is the strongest warning sign that a part may be unapproved, according to AC 21-29 guidance?
Regulations
8. Under 14 CFR Part 21, what is the primary purpose of the Type Certificate?
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