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Advisory Circulars (ACs)

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Advisory Circulars (ACs) search results
Number Title Status Office Date
33-1B 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.

 Cancelled ANE-100 1970-04-22
33-2A Aircraft Engine Type Certificaiton 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.

 Cancelled ANE-110 1972-06-05
33-2B 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.

 Cancelled ANE-110 1993-06-30
33-7 CERTIFICATION OF 30-SECOND AND 2-MINUTE ONE-ENGINE-INOPERATIVE (OEI) RATINGS FOR ROTORCRAFT TURBINE ENGINES

This advisory circular (AC) provides information and guidance on acceptable methods, but not the only methods, for compliance with the requirements for 30-second OEI and 2-minute OEI rotorcraft turbine engine ratings in part 33 of Title 14 of the Code of Federal Regulations (14 CFR Part 33).

 Cancelled ANE-111 2006-09-06
33-10 Statistical Analysis Considerations for Comparative Test and Analysis Based Compliance Findings for Turbine Engine and Auxiliary Power Unit Replacement, Redesign and Repaired Parts

a. This advisory circular (AC) describes acceptable statistical methods, but not the only methods, to help develop substantiating data for comparative test and analysis compliance findings.

Cancelled ANE-111 2014-08-28
33-2 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.

 Cancelled ANE-110 1966-03-30
33-3 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.

 Cancelled ANE-100 1968-09-09
33-4 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.

 Cancelled ANE-110 1983-07-28