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
|
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
| SAE ARP 994 : 2016 | DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
| SAE AIR 5661A : 2017 | COMPARTMENT DECOMPRESSION ANALYSIS |
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| FAA AC 25-30 : 2014 | FUEL TANK STRENGTH IN EMERGENCY LANDING CONDITIONS |
| SAE AIR1537A | REPORT ON AIRCRAFT ENGINE CONTAINMENT |
| FAA AC 25-8 : 0 | AUXILIARY FUEL SYSTEM INSTALLATIONS |
| FAA AC 23-10 : 0 | AUXILIARY FUEL SYSTEMS FOR RECIPROCATING AND TURBINE POWERED PART 23 AIRPLANES |
| FAA AC 25-20 : 0 | PRESSURIZATION, VENTILATION AND OXYGEN SYSTEMS ASSESSMENT FOR SUBSONIC FLIGHT INCLUDING HIGH ALTITUDE OPERATION |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
| SAE AIR 4003 : 1991 | REPORT ON AIRCRAFT ENGINE CONTAINMENT |
| FAA AC 20-135 : 0 | POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA |
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