Number | Title | Status | Office | Date |
---|---|---|---|---|
33-8 |
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). |
Active | ANE-111 | 2009-08-19 |
33-6 |
Weld Repair of Aluminum Crankcases and Cylinders of Piston Engines - Including Change 1
This advisory circular also includes information on critical areas of welding, qualifications of welder's, inspection techniques, the thermal processes, and technical data required. This advisory circular references industry and military specifications which are acceptable for use by repair stations as approved data. |
Active | ANE-110 | 1994-12-20 |
33-7A |
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). |
Active | ANE-111 | 2009-06-11 |
33-11 |
Oxidation, Hot Corrosion, Thermal Fatigue, and Erosion Characteristics Testing to Support 14 CFR, Part 33, § 33.15, Compliancefor Turbine Engines
These equivalencies relate to oxidation, hot corrosion, and thermal fatigue and erosion characteristics in the engine environment. |
Active | ANE-111 | 2014-09-23 |
33-2C |
General Type Certification Guidelines for Turbine Engines
This AC applies to certain sections of Title 14 of the Code of Federal Regulations (14 CFR) parts 21, 33, and 45, and describes or references methods of compliance that may be acceptable for engine type certification work. |
Active | ANE-111 | 2013-06-25 |
33-9 |
Developing Data for Major Repairs of Turbine Engine Parts
This advisory circular (AC) provides information and guidance on developing the technical data needed for major repairs of critical and complex turbine engine parts. |
Active | AIR-600 | 2010-04-30 |
33-5 |
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). |
Active | ANE-110 | 1990-06-18 |