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MIL T 25920 : C

MIL T 25920 : C

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION

Withdrawn date

07-23-2013

Publisher

US Military Specs/Standards/Handbooks

Sets forth ground and flight testing requirements for turbojet, turbofan, turboprop, and shaft turbine propulsion system installations in military aircraft and includes test requirements for the propulsion subsystem condition indication system and propulsion installation aerospace ground equipment.

DocumentType
Standard
PublisherName
US Military Specs/Standards/Handbooks
Status
Withdrawn

MIL-I-83294 Base Document:1971 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR

MIL-T-5522 Revision D:1975 TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS
MIL A 8892 : 0 AIRPLANE STRENGTH AND RIGIDITY, VIBRATION
MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES
MIL-F-25381 Revision A:1972 FLIGHT TESTING, ELECTRICAL SYSTEM, PILOTED AIRCRAFT AND GUIDED MISSILE, GENERAL REQUIREMENTS FOR
MIL-P-26366 Revision A:1962 PROPELLER SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL A 8893 : 0 AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE
MIL-E-22285 Base Document:1959 EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF
MIL-P-8686 Base Document:1955 POWER UNITS, AIRCRAFT AUXILIARY, GAS-TURBINE TYPE GENERAL SPECIFICATION FOR [ASG]
MIL-STD-831 Base Document:1963 TEST REPORTS, PREPARATION OF
MIL-E-5007 Revision D:1973 ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
MIL-A-8871 Revision A:1971 AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS
MIL-S-8512 Revision D:1974 SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
MIL F 38363 : B (3) FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-E-38453 Revision A:1971 ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-I-83294 Base Document:1971 INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)

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