U .S. Department of Transportation Federal Aviation Administration Advisory Circular Subject: Performance Rules: Provisions Contained in an Operator Manual Under § 43.13(c) Date: 9/10/26 AC No: 120-77B Initiated by: AFS-300 Change:
1 PURPOSE OF THIS ADVISORY CIRCULAR (AC). This AC provides one means, but not the only means, of ensuring that the contemplated maintenance, alteration, or continue-in-service condition is in compliance with applicable regulations and existing policy. The AC recommends acceptable methods by which:
1. Title 14 of the Code of Federal Regulations (14 CFR) § 43.13(c) allows commercial operators, operating under 14 CFR part 121 and §§ 129.14(b)(3) and 135.411(a)(2),1 to meet the requirements of 14 CFR § 43.13(a) and (b) by applying the maintenance methods, techniques, and practices of their maintenance manual or the maintenance portions of the manual. This AC describes that means of compliance.
1 For the purposes of this AC, 14 CFR part 121 operators, 14 CFR part 135 operators operating under 14 CFR § 135.411(a)(2), and 14 CFR § 129.14 operators holding operations specifications (OpSpecs) which require a continuing airworthiness maintenance and inspection program are referred to collectively as “operators.”
2. T hese operators may continue to use articles in-service or perform maintenance and alterations in a different manner than incorporating the manufacturer’s maintenance information. Other methods, techniques, and practices may be incorporated into the operator’s manual so long as the methods, techniques, and practices are an acceptable standard to the Administrator, as required by 14 CFR § 43.13(c). An operator may not produce or incorporate in their manual a method, technique, or practice that is not based on accepted standards (refer to 14 CFR § 43.13).
Note 1: This is a guidance document. Its content is not legally binding in its own right and will not be relied upon by the Department as a separate basis for affirmative enforcement action or other administrative penalty.
Conformity with the guidance document is voluntary only. Nonconformity will not affect rights and obligations under existing statutes and regulations.
Note 2: The special provisions of 14 CFR § 43.13(c) do not exempt these operators from the approved data requirement of 14 CFR §§ 121.379(b) and 135.437(b) for major repairs and alterations.
Note 3: As stated in 14 CFR § 43.13(c), the special provisions are applicable only to 14 CFR § 129.14 operators of aircraft that are subject to a continuous airworthiness maintenance and inspection program. Therefore, not all 14 CFR part 129 operators are eligible to apply the provisions of 14 CFR § 43.13(c) and this AC. With respect to 14 CFR § 129.14(b)(3) for leased aircraft maintained and
2 operated under a U.S. operator’s continuous airworthiness maintenance and inspection programs, eligibility under 14 CFR § 43.13(c) is determined by the existence of and traceability to the U.S. operator’s OpSpec D072, Aircraft Maintenance—Continuous Airworthiness Maintenance Program (CAMP) Authorization. Operators using leased aircraft maintained and operated under a U.S. operator’s Continuous Airworthiness Maintenance Program (CAMP) under 14 CFR § 129.14(b)(3) can use the special provisions in 14 CFR § 43.13(c). Any other maintenance programs under 14 CFR § 129.14 cannot use 14 CFR § 43.13(c).
2 AUDIENCE. This AC applies to 14 CFR part 121 and §§ 129.14(b)(3) and 135.411(a)(2) operators using the provisions of 14 CFR § 43.13(c).
3 WHERE YOU CAN FIND THIS AC. You can find this AC on the Federal Aviation Administration’s (FAA) website at https://www.faa.gov/regulations_policies/advisory_cir culars and the Dynamic Regulatory System (DRS) at https://drs.faa.gov.
4 WHAT THIS AC CANCELS. AC 120-77A, Maintenance and Alteration Data, dated October 24, 2023, is canceled.
5 SCOPE. This AC is intended for air operators conducting operations under 14 CFR part 121 and §§ 129.14(b)(3) and 135.411(a)(2). It offers guidance on methods, techniques, and practices outlined in the maintenance manual or maintenance sections of the manual utilized by these operators. The group of affected aircraft may include:
• Aircraft type certificated in accordance with 14 CFR part 25 and Civil Air Regulations (CARs) 4b, and
• Aircraft that have been type certificated in accordance with 14 CFR parts 23, 27, and 29.
6 REGULATIONS AND GUIDANCE MATERIAL.
6.1 Regulations. These acceptable means of compliance with operating regulations refer to the applicable sections of the following 14 CFR parts:
1. Part 1, Definitions and Abbreviations.
2. Part 21, Certification Procedures for Products and Articles.
3. Part 23, Airworthiness Standards: Normal Category Airplanes.
4. Part 25, Airworthiness Standards: Transport Category Airplanes.
5. Part 27, Airworthiness Standards: Normal Category Rotorcraft.
6. Part 29, Airworthiness Standards: Transport Category Rotorcraft.
7. Part 33, Airworthiness Standards: Aircraft Engines.
8. Part 35, Airworthiness Standards: Propellers.
9. Part 36, N oise Standards: Aircraft Type and Airworthiness Certification.
10. Part 38, Airplane Fuel Efficiency Certification.
11. Part 39, Airworthiness Directives.
12. Part 43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration.
13. Part 65, Certification: Airmen Other Than Flight Crewmembers.
14. Part 91, General Operating and Flight Rules.
15. Part 119, Certification: Air Carriers and Commercial Operators.
16. Part 121, Operating Requirements: Domestic, Flag, and Supplemental Operations.
17. Part 129, Operations: Foreign Air Carriers and Foreign Operators of U.S.-Registered Aircraft Engaged in Common Carriage.
18. Part 135, Operating Requirements: Commuter and On Demand Operations and Rules Governing Persons On Board Such Aircraft.
19. Part 183, Representatives of the Administrator.
6.2 Related Guidance Materials (current editions):
6.2.1 Orders. The following orders may be used to derive information to incorporate into an operator’s manual for the purpose of alternate methods of inspection, repair, alteration, or maintenance. This list may not be all inclusive. These orders may be accessed online at https://www.faa.gov/regulations_policies/orders_notices/.
1. FAA Order 8100.15, Organization Designation Authorization Procedures.
2. FAA Order 8110.4, Type Certification.
3. FAA Order 8110.37, Designated Engineering Representative (DER) Handbook.
4. FAA Order 8110.51, Acceptability of Previously Approved Compliance Data From Foreign Sources.
5. FAA Order 8110.53, Reciprocal Acceptance of Repair Design Data Approvals Between FAA and TCCA.
6. FAA Order 8110.54, Instructions for Continued Airworthiness Responsibilities, Requirements, and Contents.
7. FAA Order 8110.113, Approval of Flammability Test Data in Support of Major Repairs or Major Alterations.
8. FAA Order 8130.2, Airworthiness Certification of Aircraft.
9. FAA Order 8300.16, Major Repair and Alteration Data Approval.
10. FAA Order 8620.2, Applicability and Enforcement of Manufacturer’s Data.
11. FAA Order 8900.1, Flight Standards Information Management System.
12. FAA Order 8900.1, Volume 3, Chapter 36, Section 1, Evaluating an Engineering Change Authorization/Order.
6.2.2 ACs. The following ACs may be used to derive information to incorporate into an operator’s manual for the purpose of alternate methods of inspection, repair, alteration, or maintenance. This list may not be all inclusive. You may obtain copies of these documents from the FAA’s website at https://www.faa.gov/regulations_policies/advisory _circulars/.
1. AC 20-77, Use of Manufacturers’ Maintenance Manuals.
2. AC 20-107, Composite Aircraft Structure.
3. AC 21.101-1, Establishing the Certification Basis of Changed Aeronautical Products.
4. AC 23.1309-1, System Safety Analysis and Assessment for Part 23 Airplanes.
5. AC 25.571-1, Damage Tolerance and Fatigue Evaluation of Structure.
6. AC 25.1309-1, System Design and Analysis.
7. AC 25.1529-1, Instructions for Continued Airworthiness of Structural Repairs on Transport Airplanes.
8. AC 27-1, Certification of Normal Category Rotorcraft.
9. AC 29-2, Certification of Transport Category Rotorcraft.
10. AC 33-2, General Type Certification Guidelines for Turbine Engines.
11. AC 33.4-1, Instructions for Continued Airworthiness.
12. AC 43-9, Maintenance Records and FAA Form 8130-3 Return to Service.
13. AC 43.13-1, Acceptable Methods, Techniques, and Practices—Aircraft Inspection and Repair.
14. AC 43.13-2, Acceptable Methods, Techniques, and Practices—Aircraft Alterations.
15. AC 43-210, Standardized Procedures for Obtaining Approval of Data Used in the Performance of Major Repairs and Major Alterations.
16. AC 91-56, Continuing Structural Integrity Program for Airplanes.
7 BACKGROUND. Operators have requested additional guidance on existing policies and procedures for developing, substantiating, and documenting maintenance or alteration data for civil aviation products. They have specifically requested guidance for when an operator performs a maintenance or alteration task (or allows an existing condition to remain in-service) that differs from that called out in a manufacturer’s service document, such as a Structural Repair Manual (SRM), Service Bulletin (SB), or maintenance manual. In response, the FAA Aircraft Certification Service and Flight Standards Service have jointly developed this AC.
8 PERFORMANCE-BASED REGULATIONS. The performance-based maintenance regulations place the scope of responsibility for the airworthiness and reliability of aircraft on the operators. Operators do not share this responsibility with manufacturers and design approval holders (DAH). Performance-based regulations require operators to produce a manual that is comprehensive in scope and detail (refer to 14 CFR §§ 121.133,
121.135, 135.21, and 135.23). Whi le they may derive maintenance (including inspections), preventive maintenance, and alteration information from product and article manufacturers, operators’ methods, techniques, and practices are specific to their operations. Where these methods, techniques, and practices would result in major repairs or alterations to an aircraft, they must be supported by technical data approved by the Administrator. The operator using a CAMP is responsible to ensure the CAMP’s effectiveness, and quickly identify and address any deficiencies in their program or information they reference.
9 DEFINI TIONS. For the purposes of this AC, the following definitions apply:
9.1 Airworthiness Limitations Section (ALS). The FAA-approved section of the instructions for continued airworthiness (ICA) that set forth mandatory maintenance requirements for structure and systems, such as those specified in accordance with 14 CFR part 23 appendix A, § A23.4 and 14 CFR part 25 appendix H, § H25.4. These maintenance requirements are approved by the FAA and may only be changed with approval from the FAA.
9.2 Airworthy. This means the aircraft conforms to its type design and is in a condition for safe operation (refer to 14 CFR § 3.5).
1. The product must conform to its type design (refer to 14 CFR § 21.31). A product conforms to its type design when its configuration and the equipment installed are as described in drawings, specifications, Type Certificate Data Sheet (TCDS), and other applicable data, including any Supplemental Type Certificate (STC) and field-approved alterations incorporated into the aircraft.
2. The aircraft must be in a condition for safe operation. The condition of the aircraft relative to wear and deterioration (e.g., skin corrosion, window delamination or crazing, fluid leaks, tire wear, etc.) must be within limits prescribed in the operator’s maintenance manual or ICA. Unless sooner surrendered, suspended, or revoked, or a termination date is otherwise established by the FAA, an airworthiness certificate is effective as long as maintenance, preventive maintenance, and alterations are performed per the applicable Federal aviation regulations and the aircraft is registered in the United States (refer to 14 CFR § 21.181).
9.3 Approved Data. Data approved by the FAA. The term “approved” is based on 14 CFR § 1.1, which states, “Approved, unless used with reference to another person, means approved by the FAA or any person to whom the FAA has delegated its authority in the matter concerned, or approved under the provisions of a bilateral agreement between the United States and a foreign country or jurisdiction.”
9.4 Article. This means a material, part, component, process, or appliance (refer to 14 CFR § 21.1).
9.5 Certification Maintenance Requirements (CMR). Required periodic tasks established during the design certification of the airplane as an operating limitation of the type
6 certificate (TC). A detailed explanation of CMRs can be found in A C 25-19, Certification Maintenance Requirements.
9.6 Change.
A variation from the method, technique, or practice, or the continue-in-service condition specified in the manufacturer’s service document and incorporated into the operator’s manual for the aircraft or article being maintained, altered, or otherwise evaluated. Such changes include, but are not limited to, developing new repair designs, revising existing work instructions or inspection intervals, using a substituted part other than the one “called out” in a maintenance manual, or revising a damage limit or wear tolerance. Changes must be executed according to the documented policies in the operator’s manual, and result in methods, techniques, and practices acceptable to the Administrator (refer to 14 CFR § 43.13(c)).
9.7 Continue-in-Service Condition. A limit, tolerance, or other parameter specified in a manufacturer’s service document or operator’s manual that authorizes operation with wear or damage within the specified parameter.
9.8 FAA Designees. As specified in 14 CFR part 183.
9.9 Instructions for Continued Airworthiness (ICA). The methods, techniques, and practices for performing maintenance, preventive maintenance, and alterations, which are provided by the DAH or its component manufacturers, are considered acceptable to the Administrator under 14 CFR § 43.13(c). For example, under 14 CFR part 25 appendix H, the ICA includes an airplane maintenance manual or section, maintenance instructions, and an ALS (refer to 14 CFR §§ 21.50(b), 25.1529, and 43.13(c), and 14 CFR part 25 appendix H).
9.10 Major Alteration. An alteration not listed in the aircraft, aircraft engine, or propeller specifications.
1. An alteration that might appreciably affect weight, balance, structural strength, performance, powerplant operation, flight characteristics, or other qualities affecting airworthiness; or
2. An alteration that is not done according to accepted practices or cannot be done by elementary operations (refer to 14 CFR § 1.1).
Note: Various segments of industry use the term “modification” to define a design change. The term “modification” is used throughout 14 CFR part 21 and is synonymous with the term “alteration.”
9.11 Major Change. Certification regulation 14 CFR § 21.93 explains major changes to type design. These changes are an FAA Aircraft Certification Service office function. Major changes to type design and major alterations can sometimes be confused. A major change to type design will result in a major alteration to the aircraft. On the other hand, not all major alterations to an aircraft will necessarily be a major change to type design. Major changes to type design can be done with STCs, changes to the original TC, or issuance of
7 a new TC only by a responsible Aircraft Certification Service office (refer to 14 CFR § 21.113).
9.12 Major Repair.
1. A repair that, if improperly done, might appreciably affect weight, balance, structural strength, performance, powerplant operation, flight characteristics, or other qualities affecting airworthiness; or
2. A repair that is not done according to accepted practices or cannot be done by elementary operations (refer to 14 CFR § 1.1).
Note: Title 14 CFR part 43 appendix A contains a listing of major alterations and repairs. The appendix listing may not include every major alteration or major repair. Operators and anyone else working on an aircraft will have to make a determination of whether the work performed is a major or minor repair or alteration in accordance with 14 CFR part 1.
9.13 Manufacturer’s Service Documents. Publications by a DAH that provide acceptable methods, techniques, and practices for performing maintenance, preventive maintenance, and alterations. They include, but are not limited to, maintenance manuals, restoration or overhaul manuals, ICAs, Component Maintenance Manuals (CMM), SRMs, SBs, Service Letters (SL), or other similar information. These documents may be incorporated into the operator’s manual and are subject to the operator’s control in consideration of 14 CFR § 43.13(c).
9.14 Methods, Techniques, and Practices. The methods, techniques, and practices referenced in 14 CFR § 43.13 are the step-by-step instructions for performing maintenance (including inspections), preventive maintenance, and alterations. These “how-to” instructions are normally contained in manufacturers’ maintenance manuals and other service documents, and are usually based on approved technical data developed by the DAH in accordance with 14 CFR §§ 21.31 and 21.50(b). In accordance with 14 CFR § 43.13(c), operators incorporate instructions into their manual for performance of maintenance. These instructions are the responsibility of the operator and can be changed as described in this AC.
9.15 Minor Alteration. An alteration other than a major alteration (refer to 14 CFR § 1.1).
9.16 Minor Repair. A repair other than a major repair (refer to 14 CFR § 1.1).
9.17 Structural Repair Manuals (SRM). These typically provide repair instructions, material substitutions, and allowable damage limits for the aircraft’s structure.
9.18 Substantiating Data. Data used to show that an aircraft, article, or a product complies with the applicable airworthiness standards (e.g., 14 CFR §§ 23.2260, 25.603, 27.603,
29.603, 33.15, and 35.17). Types of substantiating data include tests, analysis, experience, or computations appropriate to the maintenance, alteration, or continue-in-service condition of the article or product being evaluated. Substantiating
8 data establishes that the article or product meets the regulatory requirements and would be returned to its original or properly altered condition, as required by 14 CFR § 43.13(b). This data may not only be manufacturer data. It may be any other acceptable data (refer to 14 CFR §§ 21.31, 25.603, and 43.13(c)).
9.19 Supplemental Type Certificate (STC). A certificate issued by the Administrator approving a change in the type design of the product (refer to 14 CFR § 21.117).
Title 14 CFR § 21.117 references 14 CFR § 21.113, which states an STC is a major change to type design not requiring a new TC.
9.20 Technical Data. Drawings and specifications, and a listing of those drawings and specifications, needed to define the configuration and design features of a particular article, product, repair, or alteration. Typically, this includes information on materials, dimensions, and processes necessary to define structural strength, any required airworthiness limitations (AL), and any data necessary to determine the airworthiness, noise characteristics, fuel efficiency, fuel venting, and exhaust emissions (as applicable).
Technical data also includes test data, engineering analyses, or other engineering information, such as engineering handbooks or approved military or industry specifications. It may also include operational and service experience, maintenance and alteration experience, reliability data, and other documented factual information that can be shown to be directly applicable to the airworthiness of the aircraft or article (refer to 14 CFR § 21.31).
9.21 Type Certificate (TC). Includes the type design, the operating limitations, the TCDS, the applicable regulations with which the Administrator records compliance, and any other conditions or limitations prescribed for the product in the pertinent airworthiness regulations (refer to 14 CFR § 21.41).
9.22 Type Design. Title 14 CFR § 21.31 specifies type design; in pertinent part, this includes:
1. The drawings and specifications, and a listing of those drawings and specifications, necessary to define the configuration and the design features of the product shown to comply with the requirements applicable to the product;
2. Information on dimensions, materials, and processes necessary to define the structural strength of the product; and
3. The ALS of the ICA as required by 14 CFR parts 23, 25, 27, 29, 33, and 35, or as otherwise required by the Administrator.
10 APPROVED DOCUMENTS.
10.1 Prior FAA Approval. In several situations, prior approval must be obtained from the Administrator before an operator may implement changes to methods, techniques, and practices under 14 CFR § 43.13(c) included in approved documents that are required by the regulations. For example, changes to Airworthiness Directives (AD) may not be made without the prior approval of the Administrator. This is because 14 CFR § 39.7 requires the operator of any product to which an AD applies to comply with the provisions of an applicable AD. The alternative method of compliance (AMOC) procedure is incorporated
9 i nto an AD; therefore, complying with an AMOC constitutes compliance with the AD.
An AMOC can be obtained in accordance with 14 CFR §
39.19 . The aircraft manufacturer may have made arrangements with an FAA designee to approve repairs as an AMOC to an AD. Each AD identifies the FAA office responsible for approving AMOCs (refer to 14 CFR § 39.21) .
10.2 ALs, CMRs, and the TCDS. ALs and CMRs incorporated by reference into the appropriate TCDS also require prior approval of the Administrator or appropriately delegated or authorized designee (refer to 14 CFR § 21.1 and 14 CFR part 21 subpart B).
For example, the TCDS for the Boeing 777-200/300 series airplanes states that the CMRs are listed in either the FAA-approved Section 9 of the Boeing Maintenance Planning Document (ALs and CMRs) or the applicable engine TCDS. The TCDS for the aircraft specifically states that “the more restrictive requirement from these two documents shall be in force.”
11 MANUFACTURERS’ SERVICE DOCUMENTS.
11.1 General. These documents are usually the baseline incorporated into an operator’s manual system to perform maintenance and inspections. In most cases, these documents can be changed by an operator under 14 CFR § 43.13(c). Manufacturers’ service documents include maintenance manuals, restoration or overhaul manuals, ICAs, CMMs, SRMs, SBs, SLs, and other similar information. Under 14 CFR § 21.50(b), DAHs are required to prepare and make ICAs available to operators required to comply with ICAs.
While the FAA does not approve all service documents, it approves the ALS of the ICA (refer to 14 CFR § 23.1529; part 23 appendix A; § 25.1529; and part 25 appendix H).
Other documents could include FAA-approved sections of the SRM, SBs approved as described in AC 20-77, and Maintenance Review Board Report (MRBR)-approved data, as described in AC 121-22, Maintenance Review Boards, Maintenance Type Boards, and Original Equipment Manufacturer/Type Certificate Holder Recommended Maintenance Procedures.
11.2 FAA Approval of Technical Data. Approval of data when required must be obtained in accordance with the procedures contained in the CAMP regardless of who does the maintenance (refer to 14 CFR § 43.13(c)). Sometimes manufacturers elect to obtain the FAA’s approval of technical data supporting a maintenance or alteration action before issuing a service document. This is often the most efficient and cost-effective way to approve technical data because it eliminates the need for affected operators and maintenance providers to secure independent approval before doing the work. However, it remains the operator’s responsibility to ensure that the Administrator’s approval of technical data is obtained, if required, before approving for return to service an aircraft or an article after incorporation of a repair or alteration based on the advice or recommendation of a manufacturer. A no technical objection (NTO) letter or a statement that a particular maintenance or alteration action is “DER approvable” does not constitute FAA approval. However, such a statement may be considered, when supported along with other technical information, when evaluating particular maintenance or alteration action or continue-in-service condition.
11.3 FAA-Approved Technical Data. When a manufacturer has obtained the FAA’s approval of technical data, a service document is often marked “FAA-Approved,” “FAA/DER-Approved,” or “DER-Approved.” Although the entire document is reviewed by the FAA, only the technical data (see paragraph 9.20) associated with it is approved.
In many cases, the technical data is not included in the body of the service document. All of the drawings, engineering data, and other technical information approved by the FAA is proprietary information aircraft manufacturers will normally not give out. As a result, the service documents typically contain only the instructions (methods, techniques, and practices) for performing a particular repair or alteration and not the engineering information that established compliance with the applicable airworthiness standards.
Note: Technical data alone, however, may not fulfill the requirements of the performance standards set forth in 14 CFR part 43. Drawings, specifications, and other engineering data seldom contain the how-to instructions (methods, techniques, and practices) for performing maintenance, preventive maintenance, rebuilding, or alterations. For example, it may not contain disassembly, inspection criteria, or repair procedures. A DAH’s ICAs or maintenance information contains methods, techniques, and practices considered acceptable to the FAA based on technical data approved by the FAA.
12 THE SRM AND MAINTENANCE/RESTORATION OR OVERHAUL MANUALS, WHICH ARE ALL ICA.
12.1 ICA Purpose. ICA should provide repair instructions, material substitutions, and allowable damage limits data for continue-in-service condition of the aircraft’s structure.
ICA sets forth acceptable methods, techniques, and practices for performing structural repairs in the same manner as other service documents (e.g., maintenance, component, or restoration or overhaul manual). Manufacturers typically request FAA approval of the SRM so the operator may have ready access to approved data to perform minor or major repairs and return aircraft to service in accordance with the airworthiness standards and 14 CFR §§ 121.379(b) and 135.437(b).
12.1.1 It is the operator’s responsibility to classify repairs as major or minor. An operator may use an FAA-approved SRM or other ICA to accomplish repairs it has classified as either major or minor. However the operator accomplishes the process, it must be done in accordance with the procedures described in the operator’s manual.
12.1.2 ICA should describe allowable damage limits that an operator may use to keep an aircraft in-service without incorporating a repair. These damage limits are not necessarily the maximum limits that the aircraft is capable of withstanding while still complying with the airworthiness standards. An operator intending to operate an aircraft with damage beyond a manufacturer’s established damage limit must support the position that the aircraft continues to meet the airworthiness standards. The substantiating data must be in accordance with technical data or standards acceptable to the Administrator (refer to 14 CFR § 43.13(c)) (i.e., traceable to a certification basis standard).
12.2 Maintaining Airworthy Condition. Performing maintenance in accordance with the applicable ICA is one way to maintain certain areas, such as those the SRM is applicable to, of an aircraft in an airworthy condition. Aircraft structural designs are certificated to meet the applicable airworthiness standards (certification basis) that were in effect when the TC was issued. Any subsequent repairs must continue to comply with applicable airworthiness standards (certification basis) and be accomplished in accordance with 14 CFR part 43.
12.3 Additional ICA Uses. In addition to providing acceptable methods, techniques, and practices for performing maintenance, and when supported by appropriate substantiating data traceable to standards acceptable to the Administrator, ICAs may also be used to develop new or different repairs, or to authorize damage limits beyond those set forth in the operator’s manual. An SRM may also have specific procedures authorizing continued aircraft operation for a defined period of time before a permanent repair is required to be completed.
Note: The SRM is not part of the ALS of the ICA or the CMR. Moreover, the SRM is not part of the type design, even though it is often referenced on the TCDS under the heading of “Service Information,” as it is for the Boeing 777-200/300-series airplanes.
13 MAINTENANCE PERFORMANCE RULES.
13.1 Title 14 CFR § 43.13(a). Title 14 CFR § 43.13(a) states that maintenance, preventive maintenance, and alterations may be performed in accordance with either of the following, except as noted in 14 CFR § 43.16:
1. Methods, techniques, and practices in the current manufacturer’s maintenance manual or the ICA prepared by the manufacturer; or
2. Other methods, techniques, and practices acceptable to the Administrator.
13.2 Title 14 CFR § 43.13(b). Under 14 CFR § 43.13(b), each person must perform work in such a manner and use materials of such a quality that the aircraft or article worked on will be returned to at least its original or properly altered condition. This does not mean that an aircraft or article must be maintained in factory-new condition. Rather, it requires that the maintenance, preventive maintenance, and alterations result in an airworthy aircraft (i.e., one that complies with 14 CFR part 25, any other applicable airworthiness standards (such as 14 CFR part 33), and the pertinent operating rules). Generally, this is accomplished by following the maintenance manuals prepared by the manufacturers, or using other information acceptable to the Administrator, such as ACs.
13.3 Title 14 CFR § 43.13(c). Title 14 CFR § 43.13(c) states that (unless otherwise notified by the Administrator) the methods, techniques, and practices in the operator’s maintenance manual constitute an acceptable means of compliance with 14 CFR § 43.13.
Therefore, an operator that follows its maintenance manual procedures not only complies with 14 CFR §§ 121.367, 121.369, 135.425, and 135.427 (see paragraph 15), but also
12 complies with 14 CFR § 43.13(a) and (b). This applies to operators using a continuous airworthiness maintenance and inspection program under 14 CFR § 129.14.
Note: The special conditions of 14 CFR § 43.13(c) notwithstanding, each operator is responsible for determining that major repairs and major alterations have been accomplished in accordance with technical data approved by the Administrator (refer to 14 CFR §§ 121.379(b) and 135.437(b)).
14 METHODS, TECHNIQUES, AND PRACTICES VERSUS TECHNICAL DATA.
14.1 General. The terms “methods, techniques, and practices” and “technical data” have often been confused. While the concepts are related, each has a distinct meaning in 14 CFR.
14.1.1 The methods, techniques, and practices referenced in 14 CFR § 43.13 are the step-by-step instructions for performing maintenance (including inspections), preventive maintenance, and alterations. These “how-to” instructions are normally contained in manufacturers’ maintenance manuals and other service documents, and are usually based on approved technical data developed by the DAH. In accordance with 14 CFR § 43.13(c), operators generally incorporate these DAH instructions into their manual. These methods, techniques, and practices are the responsibility of the operator and can be changed as described in this AC.
14.2 Technical Data. Technical data is defined in paragraph 9.20. It can be included in maintenance manuals or restoration or overhaul manuals. For example, if the manual specifies the required materials, dimensions, or other design information, this represents technical data. The operator must substantiate any changes to technical data in order for the methods, techniques, or practices to be acceptable to the Administrator.
14.3 Damage Limits. An allowable damage limit in an SRM represents an acceptable method for accomplishing a repair or authorizing a continue-in-service condition. The allowable damage “limit” established by the TC holder (TCH) is based on approved substantiating data (i.e., an engineering analysis showing that even with such damage the aircraft would still meet the appropriate airworthiness standards). In many cases, a higher damage limit can also be shown to comply with those airworthiness standards (see paragraph 16).
15 MAINTENANCE AND RESTORATION OR OVERHAUL MANUALS.
15.1 Title 14 CFR Parts 121 and 135.
15.1.1 Under 14 CFR §§ 119.49, 121.133, 121.135, 135.21, 135.23, and 135.427, operators must prepare and keep current a manual containing these items, among others:
• Instructions and procedures for performing maintenance, preventive maintenance, and servicing.
• Time limitations, or standards for determining time limitations, for overhaul, inspections, and checks of aircraft and related components.