MIL F 9490 : D
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
Available format(s)
PDF
Superseded date
22-04-2008
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Specifies flight control systems which include all components to transmit flight control commands, from the pilot or other sources to appropriate force and moment producers.
| Committee |
FSC 15GP
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| DevelopmentNote |
D NOTICE 1 - Notice of Validation. D NOTICE 2 - Notice of Administrative Change. (09/2007)
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| DocumentType |
Standard
|
| Pages |
99
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC3/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| 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)/7(2011) : 2011 | 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)/11(2013) : 2013 | 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)/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 |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| DEFSTAN 00-970(PT1)SEC3/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 3 - STRUCTURE |
| MIL A 87221 : 0 | AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| DEFSTAN 00-970(PT1)SEC3/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3 - STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| DEFSTAN 00-970(PT1)SEC3/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 3: STRUCTURE |
| DEFSTAN 00-970(PT1)SEC3/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3 - STRUCTURE |
| SAE AIR4982A | Aerospace Fly-by-Light Actuation Systems |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| MIL-T-5522 Revision D:1975 | TEST REQUIREMENTS AND METHODS FOR AIRCRAFT HYDRAULIC AND EMERGENCY PNEUMATIC SYSTEMS |
| MIL-A-8865 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR |
| MIL-I-8500 Revision D:1980 | INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| MIL A 8892 : 0 | AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
| MIL G 25561 : B | GRIP ASSEMBLY, CONTROLLER, AIRCRAFT, TYPE MC AND 2 |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| MS33736 Revision D:2002 | TURNBUCKLE ASSEMBLIES, CLIP LOCKING OF |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| MIL A 8893 : 0 | AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL G 6641 : B NOTICE 1 | GEARBOX, AIRCRAFT ACCESSORY DRIVE, GENERAL SPECIFICATION FOR [ASG] |
| MIL-STD-480 Revision B:1988 | CONFIGURATION CONTROL - ENGINEERING CHANGES, DEVIATIONS AND WAIVERS |
| MIL-A-22771 Revision D:1984 | ALUMINUM ALLOY FORGINGS, HEAT TREATED |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| MIL-A-8870 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
| MIL T 5677 : B | THIMBLE, WIRE CABLE, AIRCRAFT |
| MIL T 6117 : D | TERMINAL, CABLE ASSEMBLIES, SWAGED TYPE |
| MIL-M-38510 Revision J:1991 | MICROCIRCUITS, SPECIFICATION FOR |
| MIL P 7034 : D | PULLEY, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL-B-7949 Revision E:1981 | BEARING, BALL, AIRFRAME, ANTIFRICTION |
| MIL-F-7190 Revision B:1985 | FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL C 27500 : G | CABLE, POWER, ELECTRICAL & CABLE SPECIAL PURPOSE, ELECTRICAL SHIELDED & UNSHIELDED |
| MIL C 18375 : A | CABLE, STEEL (CORROSION RESISTING, NON MAGNETIC) FLEXIBLE, PREFORMED (FOR AERONAUTICAL USE) (ASG) |
| MS33588 Revision E:1984 | NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
| MIL W 83420 : E | WIRE, ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL |
| MIL-B-81820 Revision F:1994 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION, GENERAL SPECIFICATION FOR |
| MS24665 Revision F:1986 | PIN, COTTER (SPLIT) |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MIL-U-3963 Revision A:1958 | UNIVERSAL JOINT, ANTIFRICTION BEARINGS |
| MIL I 7064 : LATEST | INDICATOR, POSITION, ELEVATOR TRIM TAB |
| MS33572 Revision C:1968 | Instrument, Pilot, Flight, Basic, Standard Arrangement for Helicopters |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-B-8976 Base Document:1969 | BEARINGS, PLAIN, SELF-ALIGNING, ALL METAL |
| MIL-S-8879 Revision C:1991 | SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-S-5676 Revision A:1950 | SPLICING, CABLE TERMINAL, PROCESS FOR AIRCRAFT |
| MIL-A-21180 Revision D:1984 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| MIL-B-6039 Revision E:1994 | BEARING, DOUBLE ROW, BALL, SEALED ROD END, ANTI FRICTION, SELF ALIGNING |
| MIL-STD-250 Revision D:1974 | AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT |
| MIL-A-8866 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
| SAE ARP 988 : 2016 | ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL S 9419 : E | SWITCH, TOGGLE, MOMENTARY, FOUR-POSITION ON, CENTER OFF, GENERAL SPECIFICATION FOR |
| MIL T 8878 : D | TURNBUCKLE, POSITIVE SAFETYING |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL D 7602 : A NOTICE 1 | DRIVE, TURBINE, AIR AIRCRAFT ACCESSORY, GENERAL SPECIFICATION FOR |
| MIL T 781 : D | TERMINAL, WIRE ROPE, SWAGING |
| MIL STD 421 : LATEST | |
| MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
| MIL-B-6038 Revision A:1961 | BEARING, BALL BELLCRANK, ANTI FRICTION, AIRFRAME |
| MIL J 6193 : C | JOINT, UNIVERSAL, PLAIN, LIGHT AND HEAVY DUTY |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| NAS 516:2015 | FITTING, LUBRICATION, .1250 INCH DRIVE, FLUSH TYPE |
| 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-S-8698 Base Document:1954 | STRUCTURAL DESIGN REQUIREMENTS, HELICOPTERS [ASG] |
| MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| MS15981 Revision D:1967 | FASTENER, EXTERNALLY THREADED, SELF LOCKING DESIGN AND USAGE LIMITATIONS FOR |
| MIL-F-3541 Revision C:1989 | FITTING, LUBRICATION, GENERAL SPECIFICATION FOR |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-F-83142 Revision A:1969 | FORGING, TITANIUM ALLOYS, PREMIUM QUALITY |
| MIL A 83444 : 0 | AIRPLANE DAMAGE TOLERANCE REQUIREMENTS |
| MS33602 Base Document:1967 | BOLT, SELF RETAINING AIRCRAFT RELIABILITY AND MAINTAINABILITY DESIGN AND USAGE REQUIREMENTS FOR |
| MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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