Number | Title | Status | Office | Date |
---|---|---|---|---|
33-6 |
Weld Repair of Aluminum Crankcases and Cylinders of Piston Engines - Including Change 1
This advisory circular (AC) provides guidance to demonstrate compliance with the requirements of Title 14, Code of Federal Regulations (14 CFR) part 33, Airworthiness Standards: Aircraft Engines. |
Active | ANE-110 | 1994-12-20 |
33.14-1 |
Damage Tolerance for High Energy Turbine Engine Rotors - Including Change 1
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). |
Active | ANE-110 | 2001-01-08 |
33.78-1 |
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). |
Active | ANE-110 | 2000-02-08 |
33.15-1 |
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. |
Active | ANE-110 | 1998-09-22 |
91-33A |
Use of Alternate Grades of Aviation Gasoline for Grade 80/87, and Use of Automotive Gasoline
Provides information relating to the use of alternate grades of gasoline when grade 80/87 aviation is not available and the resultant effects of the use of the alternate fuels which have higher TEL (tetraethyl lead) content. |
Active | ANE-110 | 1984-07-18 |
33.19-1 |
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). |
Active | ANE-110 | 2004-09-27 |
33.47-1 |
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. |
Active | ANE-110 | 1988-06-27 |
35.4-1 |
Propeller Instructions for Continued Airworthiness
Provides guidance and acceptable methods, but not the only methods, for demonstrating compliance with 14 CFR §35.4, Instructions for Continued Airworthiness. |
Active | ANE-110 | 2003-11-03 |
33.4-1 |
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. |
Active | ANE-110 | 1999-08-27 |
33.4-2 |
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 |
Active | ANE-110 | 2001-03-08 |
33.28-2 |
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. |
Active | ANE-110 | 2003-08-13 |
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 |
33.28-1 |
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. |
Active | ANE-110 | 2001-06-29 |
33.63-1 |
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). |
Active | ANE-110 | 2007-07-25 |
33.87-2 |
Comparative Endurance Test Method to Show Durability for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts
Comparative Endurance Test Method to Show Durability for Parts Manufacturer Approval of Turbine Engine and Auxiliary Power Unit Parts |
Active | ANE-110 | 2009-06-25 |