MIL T 25920 : C
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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
07-23-2013
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Withdrawn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 (No S/S Document) |
| MIL-T-5522 Revision D:1975 | Test Requirementsand Methodsfor Aircraft Hydraulicand Emergency Pneumatic Systems (S/S By MIL-STD-5522) |
| 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, Electric System, Piloted Aircraft and Guided Missile, General Requirements for (No S/S Document) |
| 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 |
| 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 Strength and Rigidity Flight and Ground Operations Tests (for Future Procure. (see MIL-A-87221) |
| 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 (S/S by MIL-E-87145) |
| MIL-I-83294 Base Document:1971 | Installation Requirement, Aircraft Propulsion Systems, General Specification for (No S/S Document) |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
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