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FAA AC 33.87-2 : 2009

Current

Current

The latest, up-to-date edition.

COMPARATIVE ENDURANCE TEST METHOD TO SHOW DURABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

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

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