MIL-A-8865 Revision B:1987
|
AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
MIL-DTL-18375H: 2005
|
WIRE ROPE, FLEXIBLE, CORROSION-RESISTING, NONMAGNETIC, FOR AIRCRAFT CONTROL |
MIL-PRF-7958 Revision D:2013
|
PUSH-PULL CONTROLS, FLEXIBLE AND RIGID |
SAE AMS A 21180 : 2011
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
SAE AMS 5676 : 2011
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WELDING WIRE, 80NI - 20CR |
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) |
SAE AS 8976 : 2012
|
BEARINGS, PLAIN, SELF-ALIGNING, ALL METAL, GENERAL SPECIFICATION FOR |
SAE AS 15002 : 2010
|
FITTING, LUBRICATION, HYDRAULIC, SURFACE CHECK, STRAIGHT THREADS, STEEL, TYPE 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 |
SAE AS 81820 : 2014
|
BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION |
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-DTL-781 Revision J:2014
|
TERMINAL, WIRE ROPE SWAGING, GENERAL SPECIFICATION FOR |
NASM33588:2010
|
NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
SAE AMS 2175 : 2010
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
SAE AS 7949 : 2004
|
BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD |
MIL-M-7997 Revision C:1981
|
MOTOR, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT GENERAL SPECIFICATION FOR |
MIL-DTL-83420 Revision P:2017
|
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, 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-A-87229 Base Document:1985
|
AUXILIARY POWER SYSTEMS, AIRBORNE |
DOT/FAA/AR-MMPDS-01 : 20030131
|
METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) |
MIL-DTL-6193 Revision E:2017
|
JOINTS, UNIVERSAL, PLAIN, LIGHT AND HEAVY DUTY, GENERAL SPECIFICATION FOR |
MIL-A-8870 Revision C:1993
|
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
SAE AMS A 22771 : 2012
|
ALUMINUM ALLOY FORGINGS, HEAT TREATED |
MIL T 5677 : B
|
THIMBLE, WIRE CABLE, AIRCRAFT |
MIL-M-38510 Revision J:1991
|
MICROCIRCUITS, SPECIFICATION FOR |
SAE AS 5440 : 2011
|
HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
NASM 25049 : REV 1
|
KNOBS, CONTROL, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
SAE AS 6038 : 2011
|
BEARINGS, BALL, BELLCRANK, ANTIFRICTION, AIRFRAME |
MIL E 5400 : T
|
ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
MIL-STD-7080 Base Document:1994
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
SAE AMS 4965 : 2014
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
SAE AS 56761 : 1999
|
SPLICING; CABLE TERMINAL, PROCESS FOR, AIRCRAFT |
NASM33540:2003
|
SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR |
MIL-STD-464 Revision C:2010
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
NEMA WC 27500 : 2015
|
STANDARD FOR AEROSPACE AND INDUSTRIAL ELECTRICAL CABLE |
MIL-DTL-6117 Revision L:2008
|
WIRE ROPE ASSEMBLIES, AVIATION, SWAGED TYPE |
MIL-PRF-5503 Revision G:2013
|
ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
SAE AS 8879 : 2004
|
SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
MS33572 Revision C:1968
|
INSTRUMENT, PILOT, FLIGHT, BASIC, STANDARD ARRANGEMENT FOR HELICOPTERS |
SAE AS 6039 : 2009
|
BEARINGS, BALL, ROD END, DOUBLE ROW, SELF-ALIGNING |
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 |
NASM33602:2011
|
BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR |
SAE ARP 1961 : 2016
|
GEARBOX - AIRFRAME MOUNTED ACCESSORY |
MIL-DTL-8878 Revision L:2014
|
TURNBUCKLES, POSITIVE SAFETYING, GENERAL SPECIFICATION FOR |
MIL-A-8867 Revision C:1987
|
AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
MIL-DTL-7034 Revision F:2005
|
PULLEYS, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-A-8861 Revision B:1986
|
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
FAA AC 120-29 : 0
|
CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH |
SAE AS 8775 : 1998
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
MIL-A-8866 Revision C:1987
|
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
SAE AS 35411 : 2010
|
FITTINGS, LUBRICATION |
SAE ARP 988 : 2016
|
ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
MIL-M-7969 Revision C:1965
|
Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
MIL-STD-1472 Revision G:2012
|
HUMAN ENGINEERING |
NASM24665:2016
|
PIN, COTTER (SPLIT) |
SAE AMS F 7190 : 2016
|
FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL-HDBK-838 Base Document:1997
|
LUBRICATION OF MILITARY EQUIPMENT |
NASM15981:2010
|
FASTENERS, EXTERNALLY THREADED, SELF-LOCKING DESIGN AND USAGE LIMITATIONS FOR |
SAE ARP 490 : 2008
|
ELECTROHYDRAULIC SERVOVALVES |
MIL-P-8564 Revision D:1970
|
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
NAS 516:2015
|
FITTING, LUBRICATION, .1250 INCH DRIVE, FLUSH TYPE |
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
MIL-HDBK-17-1 Revision F:2002
|
COMPOSITE MATERIALS HANDBOOK - VOLUME 1: POLYMER MATRIX COMPOSITES GUIDELINES FOR CHARACTERIZATION OF STRUCTURAL MATERIALS |
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 |