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FAA AC 33.87-1 : 2015

Current

Current

The latest, up-to-date edition.

ENGINE OVERTORQUE TEST, CALIBRATION TEST, ENDURANCE TEST, AND TEARDOWN INSPECTION FOR TURBINE ENGINE CERTIFICATION (SECTIONS 33.84, 33.85, 33.87, 33.93)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2015

€53.84
Excluding VAT

Chapter 1 - General
Chapter 2 - Calibration Tests
Chapter 3 - Endurance Test
Chapter 4 - Teardown Inspection
Appendix 1 - Graphic Profiles of Endurance Test Schedules
Appendix 2 - Endurance Test Plan Requirements
Appendix 3 - Endurance Test Cycle for Multiple Engine Tests
Appendix 4 - Engine Configuration Modifications in Endurance
              Test
Appendix 5 - Endurance Test Conformity Inspections and Type
              Inspection Authorization
Appendix 6 - Test Reports Requirements
Appendix 7 - Endurance Testing for a Two-Minute Transient
              Overtemperature Limit Approval
Appendix 8 - Endurance Test for Engine Certification and
              Showing of Compliance for Engineering Changes
Appendix 9 - Rotorcraft Operation with OEI Ratings and
              Endurance Test
Appendix 10 - Accumulated Endurance Testing Times for
              Section 33.87(e)
Appendix 11 - Teardown Inspection Requirements - Dirty
              Inspection and Clean Inspection
Appendix 12 - Historical Background for the Calibration
              Tests, Endurance Tests, and Teardown Inspection
              Requirements

Gives a method of compliance for the test requirements of Title 14, of the Code of Federal Regulations (14 CFR) 33.84 (engine overtorque test) when the applicant chooses to run that test as part of the endurance test of section 33.87.

DocumentType
Standard
Pages
86
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 33.87-2 : 2009 COMPARATIVE ENDURANCE TEST METHOD TO SHOW DURABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS

FAA AC 33.87-2 : 2009 COMPARATIVE ENDURANCE TEST METHOD TO SHOW DURABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS
FAA 8110.4 : 2011 TYPE CERTIFICATION
FAA AC 33.7-1 : 2010 RATINGS AND OPERATING LIMITATIONS FOR TURBINE ENGINES (SECTIONS 33.7 AND 33.8)

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