POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA

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Hardcopy , PDF

Language(s)

English

Publisher

Federal Aviation Administration

1 PURPOSE
2 RELATED FAR SECTIONS
3 BACKGROUND
4 DEFINITIONS
5 FIRE PROTECTION PRINCIPLES AND OBJECTIVES
6 FIRE TEST EQUIPMENT STANDARDS AND TEST CRITERIA
7 FIRE PROTECTION INSTALLATION AND DESIGN FEATURES
8 ENGINE CASE BURN-THROUGH CRITERIA [SECTION 23.903 (b)
(1) and 25.903 (d) (1)]
APPENDIX 1 RELATED FAR SECTIONS
APPENDIX 2 RELATED READING MATERIAL

Gives guidance for use in demonstrating compliance with the powerplant fire protection requirements of the Federal Aviation Regulations (FAR).

DocumentType	Standard
Pages	18
PublisherName	Federal Aviation Administration
Status	Current

SAE AS 5127/2 : 2014	TEST METHOD FOR AEROSPACE FIREWALL SEALANT FLAME PENETRATION
FAA AC 23-15 : 2003	SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM
FAA AC 23-24 : 2005	AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS
SAE ARP 292 : 2014	ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS
SAE ARP 5757 : 2016	GUIDELINES FOR ENGINE COMPONENT TESTS
ISO 2685:1998	Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones
FAA AC 23-16 : 0	POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
FAA AC 33.17-1 : 2009	ENGINE FIRE PROTECTION SECTION 33.17
FAA 8110.4 : 2011	TYPE CERTIFICATION
SAE ARP 986 : 2015	GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES
FAA AC 20-128 : 0	DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE
BS ISO 2685:1998	Aircraft. Environmental test procedure for airborne equipment. Resistance to fire in designated fire zones
FAA AC 23-2 : 2013	FLAMMABILITY TESTS

SAE AIR 1377B : 1980	FIRE TEST EQUIPMENT FOR FLEXIBLE HOSE AND TUBE ASSEMBLIES
SAE AS 1055 : 2013	FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS

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FAA AC 20-135 : 0

POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA

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