FAA AC 20-128 : 0
Current
The latest, up-to-date edition.
DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE
Hardcopy , PDF
English
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1 PURPOSE
2 CANCELLATION
3 APPLICABILITY
4 RELATED DOCUMENTS
5 BACKGROUND
6 DEFINITIONS
7 DESIGN CONSIDERATIONS
8 ACCEPTED DESIGN PRECAUTIONS
9 ENGINE AND APU FAILURE MODEL
10 SAFETY ANALYSIS
APPENDIX 1 AC-20-128A USER'S MANUAL - RISK ANALYSIS
METHODOLOGY for UNCONTAINED ENGINE/APU FAILURE
Provides a method of compliance with the requirements of section 23.901(f), 23.903(b)(1), 25.901(d) and 25.903(d)(1) of the Federal Aviation Regulations (FAR) pertaining to design precautions taken to minimize the hazards to an airplane in the event of uncontained engine or auxiliary power unit (APU) rotor failures.
| DocumentType |
Standard
|
| Pages |
48
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
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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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