SAE AS 8054 : 1996
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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
31-05-2012
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Withdrawn
|
| SAE ARP 1839 : 2015 | A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS |
| SAE ARP 1587 : 2013 | AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM GUIDE |
| SAE AIR 4175 : 2016 | A GUIDE TO THE DEVELOPMENT OF A GROUND STATION FOR ENGINE CONDITION MONITORING |
| 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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