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Number Office Title Date
25.981-1A AIR-110E Guidelines for Substantiating Compliance with the Fuel Tank Temperature Requirements (Cancelled) Date Cancelled: 04-18-2001
Cancelled By: 25.981-1B
01-20-1971
25.981-1B ANM-112 Fuel Tank Ignition Source Prevention Guidelines (Cancelled) Date Cancelled: 09-19-2008
Cancelled By: 25.981-1C
04-18-2001
25.981-2 ANM-112 Fuel Tank Flammability Minimization (Cancelled) Date Cancelled: 09-19-2008
Cancelled By: 25.981-2A
04-18-2001
27-1A ASW-110 Certification of Normal Category Rotorcraft (Cancelled) Provides guidance regarding an acceptable means but not the only means of compliance with Part 27 of the Federal Aviation Regulations (FAR) applicable to certification of normal category rotorcraft. This revision renumbers paragraphs to correspond with FAR numbering. Also, it is divided by Subparts and the page numbers reflect the relevant FAR Subpart. SN 050-007-01279-9 Date Cancelled: 04-25-2006 07-30-1997
29-1 ASW-110 Approval Basis for Automatic Stabilization Equipment (ASE) Installation in Rotorcraft (Cancelled)

Gives means for compliance with flight requirements in various CAR’s. Change 2, Transmits revised information about the time delay of automatic stabilization equipment.

Date Cancelled: 08-23-2013
12-26-1963
29-2B ASW-110 Certification of Transport Category Rotorcraft (Cancelled) Provides guidance regarding an acceptable means but not the only means of compliance with Part 29 of the Federal Aviation Regulations (FAR) applicable to certification of transport category rotorcraft. This revision renumbers paragraphs to correspond with FAR numbering. Also, it is divided by Subparts and the page numbers reflect the relevant FAR Subpart. Date Cancelled: 02-12-2003 07-30-1997
33-1B ANE-100 Turbine Engine Foreign Object Ingestion and Rotor Blade Containment Type Certification Procedures (Cancelled)

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.

Date Cancelled: 06-30-2015
04-22-1970
33-2 ANE-110 Aircraft Engine Type Certification Handbook (Cancelled) 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. Date Cancelled: 06-05-1972
Cancelled By: 33-2A
03-30-1966
33-2A ANE-110 Aircraft Engine Type Certificaiton Handbook (Cancelled) 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. Date Cancelled: 06-30-1993
Cancelled By: 33-2B
06-05-1972
33-2B ANE-110 Aircraft Engine Type Certification Handbook (Cancelled)

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.

Date Cancelled: 06-25-2013
06-30-1993
33-3 ANE-100 Turbine and Compressor Rotors Type Certification Substantiation Procedures (Cancelled)

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.

Date Cancelled: 06-30-2015
09-09-1968
33-4 ANE-110 Design Considerations Concerning the Use of Titanium in Aircraft Turbine Engines (Cancelled)

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.

Date Cancelled: 12-14-2015
07-28-1983
33-7 ANE-111 CERTIFICATION OF 30-SECOND AND 2-MINUTE ONE-ENGINE-INOPERATIVE (OEI) RATINGS FOR ROTORCRAFT TURBINE ENGINES (Cancelled) 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). Date Cancelled: 06-11-2009
Cancelled By: 33-7A
09-06-2006
33-10 ANE-111 Statistical Analysis Considerations for Comparative Test and Analysis Based Compliance Findings for Turbine Engine and Auxiliary Power Unit Replacement, Redesign and Repaired Parts (Cancelled)

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. The findings support the Federal Aviation Administration (FAA) approval of turbine engine and auxiliary power unit (APU) replacement, redesign and repaired parts produced under:

(1)  Parts manufacturer approval (PMA),

(2)  Type Certificate (TC),

(3)  Supplemental Type Certificate (STC), or

(4)  Repair or alteration.

b.   The AC describes statistical principles that can be used to help determine adequate sample sizes for a comparative showing of equivalency of parts from different design or manufacturing processes. The guidance in this AC is acceptable for determining sample sizes and/or populations of specimens. The resulting data may be used to support a showing of compliance to the airworthiness requirements of Title 14 of the Code of Federal Regulations (14 CFR) 21.303, 14 CFR part 33, 14 CFR part 43 and Technical Standard Order (TSO) C77.

Date Cancelled: 12-24-2015
08-28-2014
33-83 ANE-110 Turbine Engine Vibration Survey (Cancelled) Provides information and guidance concerning acceptable means, but not the only means, of compliance with part 33 of the Federal Aviation Regulation (FAR) applicable to vibration tests. Date Cancelled: 09-29-2006
Cancelled By: 33-83A
02-14-1997
33.17-1 ANE-110 Fire Prevention (Cancelled)

Provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the fire prevention requirements under Title 14 CFR, part 33. (06/28/02) (ANE-110

Date Cancelled: 08-03-2009
06-28-2002
33.27-1 ANE-110 Turbine Rotor Strength Requirements of 14 CFR 33.27 (Cancelled)

This advisory circular (AC) provides guidance and acceptable methods, but not the only methods, for demonstrating compliance with the rotor strength (overspeed) requirements of 14 CFR §33.27.

Date Cancelled: 07-18-2011
09-27-2004
33.74-92 ANE-110 Turbine Engine Continued Rotation and Rotor Locking (Cancelled) Date Cancelled: 07-23-2003
Cancelled By: 33.74/92-1A
02-14-1997
33.74/92-1A ANE-110 Turbine Engine Continued Rotation and Rotor Locking (Cancelled) (Cancelled)

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).

Date Cancelled: 06-23-2016
07-23-2003
33.75-1 ANE-110 Guidance Material for 14 CFR § 33.75, Safety Analysis (Cancelled) Date Cancelled: 09-26-2007
Cancelled By: 33.75-1A
03-04-2005
33.87-1 ANE-111 Calibration Test Endurance Test and Teardown Inspection for Turbine Engine Certification (§§ 33.85, 33.87, 33.93) (Cancelled)

Provides information and guidance on acceptable methods, but not only methods, of compliance with the test requirements of § 33.85 (Calibration test) § 33.87 (endurance test), and §33.93 (teardown inspection) of Title 14 of the Code of Federal Regulations (14 CFR Part 33).

Date Cancelled: 03-09-2015
04-13-2006
33.90-1 ANE-110 Initial Maintenance Inspection (IMI), 14 CFR §33.90, Test for Turbine Engines (Cancelled) (Cancelled)

Initial Maintenance Inspection (IMI), 14 CFR §33.90, Test for Turbine Engines

Date Cancelled: 04-13-2016
03-05-2004
35.37-1 ANE-110 Composite Propeller Blade Fatigue Substantiation (Cancelled) Date Cancelled: 09-17-2001
Cancelled By: 35.37-1A
09-07-1993
35.37-1 ANE-110 Composite Propeller Blade Fatigue Substantiation (Cancelled) Date Cancelled: 09-17-2001
Cancelled By: 35.37-1A
05-11-1993
35.37-1A ANE-110 Guidance Material for Fatigue Limit Tests and Composite Blade Fatigue Substantiation (Cancelled)

Provides guidance and describes methods, but not the only methods, for demonstrating compliance with 35.37. The AC also provides methods for the fatigue evaluation of propellers and the fatigue substantiation of composite propeller blades.

Date Cancelled: 03-24-2011
09-17-2001

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