FUEL TANK STRENGTH IN EMERGENCY LANDING CONDITIONS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2014

Publisher

Federal Aviation Administration

1 Purpose
2 Applicability
3 Related Documents
4 Background
5 General
6 Other Considerations

Specifies an acceptable means for showing compliance with the fuel tank structural integrity requirements of sections 25.561, 25.721, and 25.963 of Title 14, Code of Federal Regulations (14 CFR). Section 25.963(d) addresses fuel tank safety in emergency landing conditions. Section 25.963(d) references sections 25.561 and 25.721, which also address emergency landing conditions.

DocumentType	Standard
Pages	13
PublisherName	Federal Aviation Administration
Status	Current

FAA AC 25.994-1 : 0	DESIGN CONSIDERATIONS TO PROTECT FUEL SYSTEMS DURING A WHEELS-UP LANDING
FAA AC 25-8 : 0	AUXILIARY FUEL SYSTEM INSTALLATIONS
FAA AC 20-128 : 0	DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE