Advisory Circulars
Airworthiness Standards: Aircraft Engines
[1]
| Number | Office | Title | Date |
|---|---|---|---|
| 33-1B | ANE-100 |
Turbine Engine Foreign Object Ingestion and Rotor Blade Containment Type Certification Procedures
Provides guidance and acceptable means, not the sole means, by which compliance may be shown with the design and construction requirements of Part 33 of the Federal Aviation Regulations.
|
04-22-1970 |
| 33-2B | ANE-110 |
Aircraft Engine Type Certification Handbook
Contains guidance relating to type certification of aircraft engines which will constitute acceptable means, although not the sole means, of compliance with the Federal Aviation Regulations.
|
06-30-1993 |
| 33-3 | ANE-100 |
Turbine and Compressor Rotors Type Certification Substantiation Procedures
Sets forth guidance and acceptable means, not the sole means, by which compliance may be shown with the turbine and compressor rotor substantiation requirements in FAR Part 33.
|
09-09-1968 |
| 33-4 | ANE-110 |
Design Considerations Concerning the Use of Titanium in Aircraft Turbine Engines
Provides guidance and acceptable means, not the sole means, by which compliance may be shown with the design requirements of Part 33 to minimize the probability of the occurrence of an internal fire when titanium is used in aircraft turbine engines.
|
07-28-1983 |
| 33-5 | ANE-110 |
Turbine Engine Rotor Blade Containment/Durability
Provides guidance and acceptable methods, but not the only methods, that may be used by an applicant in showing compliance with the turbine engine rotor blade containment requirements of Part 33 of the Federal Aviation Regulations (FAR).
|
06-18-1990 |
| 33-6 | ANE-110 |
Weld Repair of Aluminum Crankcases and Cylinders of Piston Engines
Provides information and guidance concerning acceptable means, but not the only means, for the development of process specifications for weld repairs on crankcases and cylinders of piston engines.
|
12-20-1994 |
| 33-7A | ANE-111 |
Guidance for 30-Second and 2-Minute One-Engine-Inoperative (OEI) Ratings for Rotorcraft Turbine Engines
This advisory circular (AC) provides guidance and acceptable means, but not the only means, for demonstrating compliance with the specific requirements applicable to 30-second and 2-minute One-Engine-Inoperative (OEI) rotorcraft turbine
engine ratings in part 33 of Title 14 of the Code of Federal Regulations (14 CFR part 33).
|
06-11-2009 |
| 33-8 | ANE-111 |
Guidance for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts under Test and Computation
This advisory circular (AC) provides guidance for developing substantiation data to support the design approval of critical and complex turbine engine and auxiliary power unit (APU) parts produced under parts manufacturer approval (PMA). This guidance is for the comparative test and analysis method used to show compliance to the airworthiness requirements under test and computation, per § 21.303 of Title 14 of the Code of Federal Regulations(14 CFR). This method supports showing the engine or APU still complies with 14 CFR part 33 and Technical Standard Order (TSO) C77. b. Additionally, this AC provides information on developing a continued operational safety (COS) plan and part numbering for turbine engine parts. |
08-19-2009 |
| 33-9 | ANE-111 |
Developing Data for Major Repairs of Turbine Engine Parts
a. This advisory circular (AC) provides information and guidance on developing the technical data needed for major repairs of critical and complex turbine engine parts. This guidance will help persons developing major repair data meet the requirements of Title 14 of the Code of Federal Regulations (14 CFR) part 43 to restore the engine to at least equal to its original or properly altered condition. This does not mean that a repaired part must be returned to a factory-new condition. However, the engine on which the repaired part is installed must remain airworthy and in compliance with the applicable regulations. For repairs of turbine engines and parts, the applicable requirements are Airworthiness Standards: Aircraft Engines (14 CFR part 33) and Fuel Venting and Exhaust Emissions Requirements for Turbine Engine Powered Airplanes (14 CFR part 34).
b. Additionally, this AC provides guidance to assist persons developing major repairs with developing a continued operational safety plan. It also helps them evaluate engine parts recovered from accidents and incidents prior to making a repair.
|
04-30-2010 |
| 33-75A | ANE-100 |
Guidance Material for 14 CFR § 33.75, Safety Analysis
Describes guidance and acceptable methods, but not the only methods, for demonstrating compliance with the safety analysis requirements of Title 14 of the Code of Federal Regulations (14 CFR) § 33.75.
|
09-26-2007 |
| 33-83A | ANE-111 | Turbine Engine Vibration Test | 09-29-2006 |
| 33.14-1 | ANE-110 |
Damage Tolerance for High Energy Turbine Engine Rotors
This advisory circular describes an acceptable means for showing compliance with the requirements of section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). Section 33.14 contains requirements applicable to the design and life management of high energy rotating parts of aircraft gas turbine engines.
|
01-08-2001 |
| 33.15-1 | ANE-110 |
Manufacturing Process of Premium Quality Titanium Alloy Rotating Engine Components
Provides guidance for compliance with the provisions under Title 14 under the Code of Federal Regulations, Part 33 (14 CFR 33) pertaining to the materials suitability and durability requirements, 33.15, as applicable to the manufacture of titanium alloy high energy rotating parts of aircraft engines.
|
09-22-1998 |
| 33.17-1A | ANE-111 |
Engine Fire Protection
This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine fire protection requirements of Title 14 Code of Federal Regulations (14 CFR 33.17). The guidance provided in this AC supersedes information contained in AC 33-2B titled "Aircraft Engine Type Certification Handbook" (Chapter 3, Section 22, titled "Section 33.17, Fire Prevention"). |
08-03-2009 |
| 33.19-1 | ANE-110 |
Guidance Material for 14 CFR §33.19, Durability, for Reciprocating Engine Redesigned Parts
This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate the redesigned parts for reciprocating engines comply with the requirements of §33.19 of Title 14 of the Code of Federal Regulations (14 CFR). This AC addresses major types design changes, parts manufacturing approvals (PMA), and supplemental type certificates (STC) for drive system or structural parts in reciprocating engines. Like all AC material, this AC is not, in itself, mandatory and does not constitute a regulation. While these guidelines are not mandatory, they are derived from extensive Federal Aviation Administration (FAA) and industry experience in determining compliance with the pertinent regulations.
|
09-27-2004 |
| 33.28-1 | ANE-110 |
Compliance Criteria for 14 CFR §33.28, Aircraft Engines, Electrical and Electronic Engine Control Systems
This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with 14 CFR 33.28, Electrical and Electronic Engine Control Systems. Like all AC material, this AC is not, in itself, mandatory and does not constitute a regulation. While these guidelines are not mandatory, they are derived from extensive Federal Aviation Administration (FAA) and industry experience in determining compliance with the pertinent regulations.
|
06-29-2001 |
| 33.28-2 | ANE-110 |
Guidance Material for 14 CFR 33.28, Reciprocating Engine, Electrical and Electronic Engine Control Systems
Provides guidance and acceptable methods, but not the only methods, that may be used by designers of reciprocating engine electronic control systems to demonstrate compliance with §33.28 of Title 14 of the Code of Federal Regulations (14 CFR 33.28), Electrical and electronic engine control systems.
|
08-13-2003 |
| 33.4-1 | ANE-110 |
Instructions for Continued Airworthiness
Provides guidance on acceptable methods, but not the only methods, of compliance with section 33.4 of the Federal Aviation Regulations, Title 14, Code of Federal Regulations.
|
08-27-1999 |
| 33.4-2 | ANE-110 |
Instructions for Continued Airworthiness: In-Service Inspection of Safety Critical Turbine Engine Parts at Piece-Part Opportunity
Instructions for Continued Airworthiness: In-Service Inspection of Safety Critical Turbine Engine Parts at Piece-Part Opportunity
|
03-08-2001 |
| 33.4-3 | ANE-111 | Instructions for Continued Airworthiness, Aircraft Engine High Intensity Radiated Fields (HIRF) and Lightning Protection Features | 09-16-2005 |
| 33.47-1 | ANE-110 |
Detonation Testing in Reciprocating Aircraft Engines
Provides guidance material for acceptable means of demonstrating compliance with the requirements of FAR Part 33, relating to detonation testing for reciprocating aircraft engines.
|
06-27-1988 |
| 33.63-1 | ANE-110 |
Turbine Engine Vibration
This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the vibration requirements of § 33.63 of Title 14 of the Code of Federal Regulations (14 CFR part 33).
|
07-25-2007 |
| 33.65-1 | ANE-110 |
Surge and Stall Characteristics of Aircraft Turbine Engines
Provides guidance material for acceptable means of demonstrating compliance with the requirements of Part 33 of the Federal Aviation Regulations (FAR) relative to surge and stall characteristics and thrust response of turbine engines. These guidelines do not constitute a regulation and are therefore not mandatory.
|
12-06-1985 |
| 33.7-3A | ANE-111 | FAA Certification Policy for Turbine Engine Lubricating Oils Qualified to AS5780 | 04-20-2007 |
| 33.70-1 | ANE-111 | Guidance Material for Aircraft Engine Life-Limited Parts Requirements | 07-31-2009 |