MIL F 9490 : D

Superseded

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FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR

Available format(s)

PDF

Superseded date

04-22-2008

Publisher

US Military Specs/Standards/Handbooks

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
DevelopmentNote	D NOTICE 1 - Notice of Validation. D NOTICE 2 - Notice of Administrative Change. (09/2007)
DocumentType	Standard
Pages	99
PublisherName	US Military Specs/Standards/Handbooks
Status	Superseded
SupersededBy	MIL-DTL-9490 Revision E:2008

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DEFSTAN 00-970(PT0)/7(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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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
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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
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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
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MIL-STD-1472 Revision G:2012	HUMAN ENGINEERING
MIL S 9419 : E	SWITCH, TOGGLE, MOMENTARY, FOUR-POSITION ON, CENTER OFF, GENERAL SPECIFICATION FOR
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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
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MIL-A-8860 Revision B:1987	AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
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