This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Guidelines for Engine Component Tests
- Aerospace Standard
- ARP5757
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
This document provides information and recommendations regarding the design and integration of aircraft electronic engine control systems. It provides previously unavailable guidance on how to substantiate compliance with civil certification regulations and associated advisory material for aircraft engine components.
Recommended Content
| Aerospace Standard | Guidelines for Engine Component Tests |
| Aerospace Standard | Environmental Control Systems for Rotorcraft |
| Aerospace Standard | Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | CHECK LIST FOR DEMONSTRATING AIRWORTHINESS OF ENGINE COMPONENTS | |
| TABLE 2 | SUMMARY OF HISTORICAL CHANGES TO CHECK LIST |
Issuing Committee
E-36 Electronic Engine Controls Committee
Areas of interest will include, but not be limited to, the design, installation, operation and maintenance of engine control system components including metering components and actuators and the interface and communication methods for (A) Cockpit Displays, (B) Flight Control, ¿ Diagnostic and Health Monitoring Systems. Coordination with other SAE committees will occur to minimize redundant activities within the organization and maximize the benefit of additional recommendations and standards.
For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright and Membership" link in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.Reference
| Number | Title |
|---|
* Redlines comparisons are available for those standards
listed in the Revision History that contain a radio button. A
redline comparison of the current version against a revision is
accomplished by selecting the radio button next to the standard and
then selecting 'compare'. At this time, Redline versions only exist
for some AMS standards. SAE will continue to add redline versioning
with ongoing updates to SAE MOBILUS.