MIL-D-8708 Revision C:1991
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The latest, up-to-date edition.
DEMONSTRATION REQUIREMENTS FOR AIRPLANES
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Important note : All end users must be registered with an Account prior to user licenses being assigned.Covers general requirements of NAVAIR (Naval Air Systems Command Headquarters) for the contractor demonstration of airplanes. Describes reporting requirements relating to demonstrations.
| DocumentType |
Standard
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| Pages |
283
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| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED.
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| SAE AS 81366 : 2002 | BOUNDARY LAYER CONTROL SYSTEM; PRESSURE |
| MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
| MIL-A-8866 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| SAE ARP 217 D : 2016 | TESTING OF AIRPLANE INSTALLED ENVIRONMENTAL CONTROL SYSTEMS (ECS) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
| MIL-A-8865 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-A-8868 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS |
| MIL-D-23143 Revision A:1982 | DATA, TECHNICAL AIRCRAFT, FOR DESIGN OF AVIATION TRAINING DEVICES |
| MIL-I-8670 Revision B:1993 | INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL W 006729 : B (1) | WATERTIGHTNESS OF AIRCRAFT, TESTING |
| MIL-A-18717 Revision C:1993 | ARRESTING HOOK INSTALLATIONS, AIRCRAFT |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| 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 |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| SAE AS 8860 : 2012 | LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS |
| MIL-T-5522 Revision D:1975 | TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS |
| MIL-I-6115 Revision A:1951 | INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF |
| DOD-STD-2167 Revision A:1988 | DEFENSE SYSTEM SOFTWARE DEVELOPMENT |
| MIL-B-83769 Revision D:1983 | BATTERY, STORAGE, LEAD ACID, GENERAL SPECIFICATION FOR |
| MIL F 15160 : G | FUSE, INSTRUMENT, POWER, AND TELEPHONE, GENERAL SPECIFICATION FOR |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-P-26366 Revision A:1962 | PROPELLER SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| DOD-C-85050 Base Document:1982 | CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| MIL-C-7762 Revision A:1967 | COMPASS, INSTALLATION OF |
| MIL-A-8591 Revision H:1990 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR |
| MIL-T-81571 Base Document:1967 | THERMAL PROTECTIVE SYSTEM, AIRCRAFT COCKPIT, GENERAL SPECIFICATION FOR |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
| MIL-STD-1333 Revision B:1987 | AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT |
| MIL-C-18244 Revision A:1962 | CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL B 85110 : A | BAR, REPEATABLE RELEASE HOLDBACK, AIRCRAFT LAUNCHING, GENERAL DESIGN REQUIREMENTS FOR |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| MIL-A-8870 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
| NISO Z39.18 : 1995 | SCIENTIFIC AND TECHNICAL REPORTS - PREPARATION, PRESENTATION, AND PRESERVATION |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-D-6728 Revision A:1956 | DAMPER, ENGINE EXHAUST FLAME AND GLARE |
| MIL-I-8675 Base Document:1953 | INSTALLATION, AIRCRAFT ARMOR |
| MIL-C-23866 Revision A:1965 | CONTROL SET, APPROACH POWER AN/ASN-54 (V) |
| MIL-E-7016 Revision F:1976 | ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
| MIL STD 470 : B | MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL E 24021 : J NOTICE 1 | ELECTRIC POWER MONITORS, EXTERNAL, AIRCRAFT |
| MIL C 83413 : A | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
| MIL-L-18276 Revision C:1964 | LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| MIL-D-19326 Revision H:1990 | Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for |
| DOD STD 2169 : 1985 | HIGH ALTITUDE ELECTROMAGNETIC PULSE (HEMP) ENVIRONMENT (U) (CLASSIFIED) |
| MIL-E-18927 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-1388-1 Revision A:1983 | LOGISTIC SUPPORT ANALYSIS |
| MIL-H-18325 Revision B:1959 | HEATING AND VENTILATING SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-F-17874 Revision B:1965 | FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF |
| MIL-T-5842 Revision B:1985 | TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
| MIL-L-22589 Revision D:1991 | LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT |
| MIL-STD-1757 Revision A:1983 | LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL F 5372 : D | FUSE, CURRENT LIMITER TYPE, AIRCRAFT |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MS90298 Revision C:1981 | CONNECTOR, RECEPTACLE ELECTRIC GROUNDING |
| MIL-A-8868 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS |
| MIL-C-8678 Base Document:1984 | COOLING REQUIREMENTS OF POWER PLANT INSTALLATIONS |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-STD-471 Revision A:1973 | MAINTAINABILITY DEMONSTRATION |
| MIL B 8565 : J | BATTERY AND CELL, STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| MIL-F-23447 Base Document:1962 | FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
| MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL-W-6729 Revision C:1993 | WATERTIGHTNESS OF AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-18717 Revision C:1993 | ARRESTING HOOK INSTALLATIONS, AIRCRAFT |
| MIL B 81757 : C | BATTERIES & CELLS STORAGE, NICKEL CADMIUM, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-T-18606 Base Document:1955 | TEST PROCEDURES FOR AIRCRAFT ENVIRONMENT SYSTEMS |
| MIL-I-85071 Revision A:1992 | INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
| MIL-R-23761 Revision B:1975 | Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
| MIL-I-8670 Revision B:1993 | INSTALLATION OF FIXED GUNS AND ASSOCIATED EQUIPMENT IN NAVAL AIRCRAFT |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-E-81910 Revision A:1977 | ELECTRICAL POWER GENERATING AND CONTROL EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATIONS FOR |
| MIL-G-7940 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE, INSTALLATION AND CALIBRATION OF |
| MIL-C-5809 Revision G:1987 | CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
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