FAA AC 25-30 : 2014
Current
The latest, up-to-date edition.
FUEL TANK STRENGTH IN EMERGENCY LANDING CONDITIONS
Hardcopy , PDF
English
01-01-2014
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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 |
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