SAE ARP5757A
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Guidelines for Engine Component Tests
Hardcopy , PDF
English
16-10-2016
03-11-2025
1. SCOPE
2. REFERENCES
3. APPLICABILITY
4. HISTORICAL PERSPECTIVE
5. APPROACH
6. SUMMARY
7. NOTES
This SAE Aerospace Recommended Practice (ARP) provides guidance for substantiating the airworthiness of aircraft engine components.
| DocumentType |
Standard
|
| Pages |
27
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
This SAE Aerospace Recommended Practice (ARP) provides guidance for substantiating the airworthiness of aircraft engine components. Generally these components are associated with the engine control system, the system or systems that allow the engine to provide thrust or power as demanded by the pilot of the aircraft while also ensuring the engine operates within acceptable operating limits. But these components may also include hardware and systems associated with engine lubrication, engine or aircraft hydraulic or electrical systems, aircraft environmental control systems, thrust reverser control, or similar aircraft or engine propulsion system functions.This paper develops the concept of using a 26 item matrix of environmental conditions for evaluating aircraft engine component airworthiness. This approach is compatible with current practices used in the industry and has been accepted by engine certification authorities as part of engine certification programs.
| FAA AC 33.91-1 : 2010 | ENGINE SYSTEM AND COMPONENT TESTS |
| FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
| SAE ARP5107B | Guidelines for Time-Limited-Dispatch (TLD) Analysis for Electronic Engine Control Systems |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| SAE AS4273A | Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations |
| FAA AC 33.17-1 : 2009 | ENGINE FIRE PROTECTION SECTION 33.17 |
| SAE AIR1639A | Safety Criteria for Pneumatic Starting Systems |
| FAA AC 33.63-1 : 2007 | TURBINE ENGINE VIBRATION |
| FAA AC 20-104 : 1978 | REVISED POWER PLANT ENGINEERING REPORT NO. 3A, STANDARD FIRE TEST APPARATUS AND PROCEDURE (FOR FLEXIBLE HOSE ASSEMBLIES) |
| FAA AC 33.91-1 : 2010 | ENGINE SYSTEM AND COMPONENT TESTS |
| FAA AC 33.28-3 : 2014 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS |
| MIL-E-8593 Revision A:1975 | Engines, Aircraft, Turboshaft and Turboprop, General Specification for |
| MIL-E-5007 Revision D:1973 | Engine, Aircraft, Turbojet and Turbofan, General Specification for |
| SAE ARP1401B | Aircraft Fuel System and Component Icing Test |
| ISO 2669:1995 | Environmental tests for aircraft equipment — Steady-state acceleration |
| FAA AC 20-147 : 2014 | TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION |
| FAA AC 20-135 : 0 | POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA |
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