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 |