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SAE AS 8054 : 1996

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

AIRBORNE ENGINE VIBRATION MONITORING (EVM) SYSTEM, GUIDELINES FOR PERFORMANCE STANDARD FOR

Withdrawn date

31-05-2012

Published date

01-01-1996

1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 UNIT QUALIFICATION AND ACCEPTANCE
5 NOTES

Provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system per FAR 25.1305 (D)(3) or transport category airplanes.

Committee
E-32
DocumentType
Standard
PublisherName
SAE International
Status
Withdrawn

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SAE AIR 1839 : 2017 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS

FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
SAE AIR 1839 : 2017 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS
ISA RP37.2 : 1982 GUIDE FOR SPECIFICATIONS AND TESTS FOR PIEZOELECTRIC ACCELERATION TRANSDUCERS FOR AEROSPACE TESTING
MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
ANSI S2.11 : 69(R2001) AMERICAN NATIONAL STANDARD FOR THE SELECTION OF CALIBRATIONS AND TESTS FOR ELECTRICAL TRANSDUCERS USED FOR MEASURING SHOCK AND VIBRATION
FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
ARINC 404A : 1974 AIR TRANSPORT EQUIPMENT CASES AND RACKING
FAA AC 25-13 : 0 REDUCED AND DERATED TAKEOFF THRUST (POWER) PROCEDURES

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