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MIL-D-8708 Revision C:1991
Current
The latest, up-to-date edition.
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DEMONSTRATION REQUIREMENTS FOR AIRPLANES
English
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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