FAA AC 33.87-2 : 2009
Current
COMPARATIVE ENDURANCE TEST METHOD TO SHOW DURABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS
Hardcopy , PDF
English
01-01-2009
1. PURPOSE
2. APPLICABILITY
3. RELATED REFERENCES
4. BACKGROUND
5. BLADE DURABILITY
6. COMPARATIVE ENDURANCE TEST METHOD
7. COMPARATIVE ENDURANCE TEST METHOD FOR OTHER GAS
PATH PARTS
Appendix - Endurance Test Cycle
Specifies a comparative endurance test method to be used for certain turbine engine or auxiliary power unit (APU) parts when manufactured under Parts Manufacturer Approval (PMA).
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 33.87-1 : 2015 | ENGINE OVERTORQUE TEST, CALIBRATION TEST, ENDURANCE TEST, AND TEARDOWN INSPECTION FOR TURBINE ENGINE CERTIFICATION (SECTIONS 33.84, 33.85, 33.87, 33.93) |
| FAA AC 33.87-1 : 2015 | ENGINE OVERTORQUE TEST, CALIBRATION TEST, ENDURANCE TEST, AND TEARDOWN INSPECTION FOR TURBINE ENGINE CERTIFICATION (SECTIONS 33.84, 33.85, 33.87, 33.93) |
| FAA 8110.42 : 2014 | PARTS MANUFACTURER APPROVAL PROCEDURES |
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : All end users must be registered with an Account prior to user licenses being assigned.
Users cannot be edited or removed once added to your Multi user PDF.