MIL-F-8785 Revision C:1980
Current
Current
The latest, up-to-date edition.
FLYING QUALITIES OF PILOTED AIRPLANES
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Important note : Users cannot be edited or removed once added to your Multi user PDF.Covers requirements for the flying and handling qualities, in flight and on the ground, of US Military, manned, piloted airplanes.
| Committee |
FSC 15GP
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| DevelopmentNote |
INACTIVE FOR NEW DESIGN 28/8/96
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| DocumentType |
Standard
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| Pages |
96
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| MIL-HDBK-2089 Base Document:1997 | AIRCRAFT SURVIVABILITY TERMS |
| MIL-D-23143 Revision A:1982 | DATA, TECHNICAL AIRCRAFT, FOR DESIGN OF AVIATION TRAINING DEVICES |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
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| DEFSTAN 00-970(PT1)SEC2/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 2: FLIGHT |
| DEFSTAN 00-970(PT1)SEC2/9(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 2: FLIGHT |
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| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
| MIL-STD-2072 Base Document:1977 | SURVIVABILITY, AIRCRAFT, ESTABLISHMENT AND CONDUCT OF PROGRAMS FOR |
| SAE AIR4094A | Aircraft Flight Control Systems Descriptions |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL-STD-1793 Base Document:1985 | FLIGHT PERFORMANCE, AIR VEHICLE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON RFB OH 45433-6503 |
| DEFSTAN 00-970(PT1)SEC2/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 2: FLIGHT |
| MIL-C-18244 Revision A:1962 | CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-18244 Revision A:1962 | CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-756 Revision B:1981 | RELIABILITY MODELING AND PREDICTION |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| MIL S 83691 : A | STALL, POST-STALL, SPIN FLIGHT TEST DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL F 18372 : 0 | FLIGHT CONTROL SYSTEMS, DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR) |
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