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Number Office Title Date
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
33.65-1 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
33.74-92-1A ANE-110 Turbine Engine Continued Rotation and Rotor Locking 07-23-2003
33.74/92-1A ANE-110 Turbine Engine Continued Rotation and Rotor Locking Provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the continued rotation and rotor locking requirements of part 33 of the Federal Aviation Regulations (FARs). 07-23-2003
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
33.78-1 ANE-110 Turbine Engine Power-Loss and Instability in Extreme Conditions of Rain and Hail Provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the requirements contained under Title 14 of the Code of Federal Regulations (14 CFR), part 33, sections 33.78(a)(2) and 33.78(c). 02-08-2000
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
33.63-1 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 ยง 33.63 of Title 14 of the Code of Federal Regulations (14 CFR part 33). 07-25-2007
33-83A ANE-111 Turbine Engine Vibration Test 09-29-2006
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
33-6 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

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