|
SAE AIR 4004 : 2015
|
GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
|
16/30337938 DC : 0
|
BS EN 80005-1 - UTILITY CONNECTIONS IN PORT - HIGH VOLTAGE SHORE CONNECTION (HVSC) SYSTEMS - PART 1: GENERAL REQUIREMENTS |
|
SAE AS 6129 : 2012
|
INTERFACE STANDARD, AIRBORNE EO/IR SYSTEMS, ELECTRICAL |
|
MIL-PRF-32316 Base Document:2008
|
RIFLE, 7.62 MM: SEMI-AUTOMATIC SNIPER SYSTEM (SASS) - M110 |
|
MIL-PRF-71185 Revision A:2013
|
Dynamic Reference Unit-Hybrid-Replacement (DRU-H-R) |
|
MIL-STD-1901 Revision A:2002
|
MUNITION ROCKET AND MISSILE MOTOR IGNITION SYSTEM DESIGN, SAFETY CRITERIA FOR |
|
13/30286075 DC : 0
|
BS EN 61000-4-36 ED 1.0 - ELECTROMAGNETIC COMPATIBILITY (EMC) - PART 4-36: TESTING AND MEASUREMENT TECHNIQUES - IEMI IMMUNITY TEST METHODS FOR EQUIPMENT AND SYSTEMS |
|
MIL-DTL-32151 Revision A:2006
|
IMPULSE CARTRIDGE, CCU-71/A |
|
MIL-STD-1791 Revision C:2017
|
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
|
MIL-PRF-83419 Revision F:2016
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
STANREC 4567 : 2014
|
NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE3) |
|
SAE ARP 5120 : 2016
|
AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE |
|
NFPA 780 : 2017
|
INSTALLATION OF LIGHTNING PROTECTION SYSTEMS |
|
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL-STD-2088 Revision B:2007
|
BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
|
DEFSTAN 00-970(PT0)/17(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
AIAA G-082:2022
|
Guide: Space Systems — Composite Overwrapped Pressure Vessels with a Plastic Liner |
|
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 |
|
MIL-PRF-32565 Revision A:2017
|
BATTERY, RECHARGEABLE, SEALED, 6T LITHIUM-ION |
|
MIL-DTL-32106 Base Document:2003
|
INITIATORS, ELECTRICAL, FOR ROCKET MOTOR IGNITERS |
|
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)/15(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL-PRF-7115 Revision G:2012
|
CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL-DTL-27723 Revision F:2013
|
Probe, Total Temperature, Deiceable |
|
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
ANEP-80 : 2009
|
NATO SONOBUOY INTEROPERABILITY SPECIFICATION - COMMON SPECIFICATIONS |
|
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL-HDBK-240 Revision A:2011
|
HAZARDS OF ELECTROMAGNETIC RADIATION TO ORDNANCE TEST GUIDE |
|
DI-MGMT-81826 Revision C:2014
|
F/A-18 - EA-18 AIRCRAFT/SYSTEM PROGRAM PROTECTION IMPLEMENTATION PLAN |
|
MIL-DTL-15370 Revision K:2015
|
COUPLERS, DIRECTIONAL, GENERAL SPECIFICATION FOR |
|
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
AFGS-87219 Revision B:2012
|
ELECTRICAL POWER SYSTEMS, AIRCRAFT |
|
MIL-PRF-53024 Revision C:2012
|
COMPACTOR, HIGH SPEED, SELF-PROPELLED, COMMERCIAL CONSTRUCTION EQUIPMENT (CCE) |
|
MIL-HDBK-510 Revision A:2014
|
AEROSPACE FUELS CERTIFICATION |
|
NASA MSFC STD 1800 : 2008
|
ELECTROSTATIC DISCHARGE (ESD) CONTROL FOR PROPELLANT AND EXPLOSIVE DEVICES |
|
A-A-52316 Revision C:2010
|
TESTER, CONSTRUCTION MATERIALS, MOISTURE & DENSITY (TCMMD) |
|
NASA STD 7002 : 0
|
PAYLOAD TEST REQUIREMENTS |
|
MIL-DTL-32572 Base Document:2017
|
Anchor Windlass, Electro-Mechanical, Vertical, Two-Speedand Variable-Speed |
|
MIL-STD-461 Revision G:2015
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
|
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
SAE AS 6169A : 2013
|
INTERFACE STANDARD, AIRBORNE EO/IR SYSTEMS, MECHANICAL |
|
SAE ARP 4945 : 2013
|
AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
|
IEC 61000-4-36:2014
|
Electromagnetic compatibility (EMC) - Part 4-36: Testing and measurement techniques - IEMI immunity test methods for equipment and systems |
|
MIL-DTL-32015 Base Document:1999
|
MICROPHONES, LINEAR, GENERAL SPECIFICATION FOR |
|
MIL-HDBK-516 Revision C:2014
|
AIRWORTHINESS CERTIFICATION CRITERIA |
|
AEP-62 VOL 7 : 2013
|
PROCEDURES FOR TESTING AND EVALUATION PERFORMANCE LEVELS OF DAS (DEFENSIVE AIDS SUITES) FOR ARMOURED VEHICLES - VOLUME 7: PROCEDURE FOR THE ASSESSMENT OF INTEGRATION |
|
MIL-STD-1310 Revision H:2009
|
SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY |
|
MIL-HDBK-510-1 Revision A:2010
|
AEROSPACE FUELS CERTIFICATION |
|
SAE ARP 5311 : 2016
|
AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS |
|
MIL-DTL-32188 Base Document:2005
|
INITIATOR, MECHANICAL ACTUATED JAU-25/A |
|
MIL-HDBK-1760 Revision A:2004
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
|
MIL-STD-331 Revision D:2017
|
FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
|
MIL-PRF-32381 Revision B:2016
|
Acoustic Hailing Device (Light) |
|
MIL-STD-1605 Revision A:2009
|
Procedures for Conducting a Shipboard Electromagnetic Interference (EMI) Survey (Surface Ship) |
|
SAE AIR 5128 : 2012
|
ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS |
|
NASA KSC STD E 0022 : 2013
|
BONDING, GROUNDING, SHIELDING, ELECTROMAGNETIC INTERFERENCE, LIGHTNING AND TRANSIENT PROTECTION, DESIGN REQUIREMENTS FOR GROUND SYSTEMS |
|
MIL-HDBK-1763 Base Document:1998
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
|
MIL-PRF-53051 Revision C:2017
|
PUMPING ASSEMBLIES, WHEEL-MOUNTED, DIESEL ENGINE DRIVEN, BULK TRANSFER, FUEL AND POTABLE WATER PUMPING SERVICE |
|
JSSG-2001 Revision B:2004
|
Air Vehicle |
|
MIL-DTL-32193 Base Document:2005
|
INITIATOR, EXPLOSIVE ACTUATED, JAU-29/A |
|
MIL-HDBK-274 Revision A:2011
|
ELECTRICAL GROUNDING FOR AIRCRAFT SAFETY |
|
MIL-PRF-32516 Base Document:2015
|
ELECTRONIC TEST EQUIPMENT, INTERMITTENT FAULT DETECTION AND ISOLATION FOR CHASSIS AND BACKPLANE CONDUCTIVE PATHS |
|
SAE AS 19692 : 2016
|
Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
|
MIL PRF 0032381 : A
|
ACOUSTIC HAILING DEVICE (LIGHT) |
|
SAE ARP 4404 : 2013 : R2019
|
AIRCRAFT ELECTRICAL INSTALLATIONS |
|
SAE AS 1650 : 2017
|
COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING, PROCUREMENT SPECIFICATION |
|
IEEE 1709-2010
|
IEEE Recommended Practice for 1 kV to 35 kV Medium-Voltage DC Power Systems on Ships |
|
NASA KSC E 165 : 2009
|
ELECTRICAL GROUND SUPPORT EQUIPMENT FABRICATION, SPECIFICATION FOR |
|
NASA MSFC SPEC 3635 : 2012
|
PYROTECHNIC SYSTEM SPECIFICATION |
|
MIL-DTL-53078 Revision A:2011
|
MOUNTING KIT: M1 TANK CLEARED LANE MARKING SYSTEM (CLAMS) |
|
NASA KSC DE 512-SM : 2012
|
FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
|
NASA KSC STD E 0001 : 2008
|
DESIGN OF ELECTRICAL CONTROL AND MONITORING SYSTEMS, EQUIPMENT (GSE), AND PANELS, STANDARD FOR |
|
NASA STD 8719.24 : 2011
|
NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
|
NASA MSFC HDBK 3697 : 2014
|
ELECTRICAL BONDING DESIGN GUIDE HANDBOOK |
|
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
|
MIL-DTL-83361 Revision B:2007
|
INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
|
MIL-PRF-57267 Base Document:2017
|
COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
|
IPC HDBK 630 : 0
|
GUIDELINES FOR DESIGN, MANUFACTURE, INSPECTION AND TESTING OF ELECTRONIC ENCLOSURES ASSEMBLY |
|
SAE ARP 5770 : 2012
|
MECHANICAL CONTROL DESIGN GUIDE |
|
BS ISO/IEC/IEEE 80005-1:2012
|
Utility connections in port High Voltage Shore Connection (HVSC) Systems. General requirements |
|
MIL-DTL-9490 Revision E:2008
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL-DTL-85097-13 Revision C:2000
|
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET MOTOR, CANOPY JETTISON, MARK 109 MODS 0 AND 1 (LOADED ASSEMBLIES) |
|
NASA MSFC SPEC 521 : 2013
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR EQUIPMENT AND SUBSYSTEMS |
|
MIL-DTL-82960 Revision B:2010
|
INITIATOR, PROPELLANT ACTUATED, JAU-27/A (MF72) |
|
NASA STD 4003 : 2013
|
ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT |
|
SAE ARP 5672 : 2016
|
AIRCRAFT PRECIPITATION STATIC CERTIFICATION |
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
|
MIL-STD-7179 Revision A:2009
|
Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
|
AEP-41 VOL 1 : 2004
|
UNIFIED ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) PROTECTION, PHILOSOPHY AND METHODOLOGY |
|
MIL-PRF-83323 Revision D:2016
|
TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
|
ADS-63-SP : 2001
|
AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS |
|
MIL-PRF-52955 Revision D:2009
|
IMPROVED POSITION AND AZIMUTH DETERMINING SYSTEM (IPADS) |
|
MIL-STD-1316 Revision F:2017
|
Fuze Design, Safety Criteria for |
|
MIL-DTL-32194 Revision B:2009
|
IMPULSE CARTRIDGE, CCU-72/A |
|
MIL-STD-1289 Revision D:2003
|
AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
|
JSSG-2010-12 Base Document:1998
|
Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
|
MIL-PRF-32293 Base Document:2008
|
Cap, Blasting, Electric - M6 |
|
SAE ARP 4404 : 2013
|
AIRCRAFT ELECTRICAL INSTALLATIONS |
|
SAE AS 6479 : 2014
|
SPLICER, FUSION, FIBER OPTIC, AEROSPACE |
|
AEP-24 : 2006
|
AIRCRAFT ELECTRICAL HAZARDS ON THE FLIGHT LINE |
|
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
|
SAE AS 5652 : 2018
|
10 MEGABIT/SEC NETWORK CONFIGURATION DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
|
AECTP-250 : 2014
|
ELECTRICAL AND ELECTROMAGNETIC ENVIRONMENTAL CONDITIONS |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
BS IEC 61000-4-36:2014
|
Electromagnetic compatibility (EMC) Testing and measurement techniques. IEMI immunity test methods for equipment and systems |
|
MIL-HDBK-235-1 Revision C:2010
|
MILITARY OPERATIONAL ELECTROMAGNETIC ENVIRONMENT PROFILES - PART 1: GENERAL GUIDANCE |
|
AEP-41 VOL 6 : 2014
|
NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) |
|
MIL-PRF-32294 Base Document:2008
|
Cap, Blasting, Non-Electric - M7 Cap, Blasting, Practice, Inert, Non-Electric - XM30 |
|
ADS-65-HDBK : 2004
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
|
AECTP-500 : 2016
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS TESTS AND VERIFICATION |
|
MIL-DTL-28875 Revision C:2012
|
Amplifiers, Radio-Frequency and Microwave, Solid-State, General Specification for |
|
MIL-DTL-23659 Revision F:2010
|
Initiators, Electric, General Design Specification for |
|
IEEE C62.55-2017
|
IEEE Guide for Surge Protection of DC Power Feeds to Remote Radio Heads |
|
MIL-DTL-62421 Revision A:2009
|
CONTROL, UNIT, ELECTRONIC, DIGITAL |
|
SAE AIR 5774 : 2012
|
COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
|
SAE ARP 5794 : 2014
|
CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
|
MIL-HDBK-237 Revision D:2005
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS AND SPECTRUM SUPPORTABILITY GUIDANCE FOR THE ACQUISITION PROCESS |
|
SAE ARP 60493 : 2017
|
GUIDE TO CIVIL AIRCRAFT ELECTROMAGNETIC COMPATIBILITY (EMC) |
|
AEP-41 VOL 7 : 2014
|
NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) - VOLUME 7: SUSTAINMENT TEST AND EVALUATION |
|
AEP-41 VOL 2 : 2004
|
ELECTROMAGNETIC (EM), ENVIRONMENTS (EMES), EM ENVIRONMENTAL EFFECTS (E[3]) AND OPERATIONAL CATEGORIES (OCS) |
|
SAE AS 4941 : 2015
|
AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
|
ANEP-45 : 0
|
|
|
SAE AS 5356 : 2017
|
COUPLING, FUEL LINE, FLEXIBLE, 125 PSI GENERAL SPECIFICATION FOR |
|
SAE ARP 5415 : 2008
|
USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING |
|
IEEE/ANSI C63.14-2014 REDLINE
|
American National Standard Dictionary of Electromagnetic Compatibility (EMC) including Electromagnetic Environmental Effects (E3) |
|
IEEE/ANSI C63.26-2015
|
IEEE/ANSI Standard for Compliance Testing of Transmitters Used in Licensed Radio Services |
|
SAE AIR 825/12 : 2013
|
OXYGEN SYSTEM INTEGRATION AND PERFORMANCE PRECAUTIONS |
|
AAS3P-10 : 2011
|
SAFETY AND SUITABILITY FOR SERVICE ASSESSMENT TESTING FOR SHOULDER LAUNCHED MUNITIONS |
|
IEC/ISO/IEEE 80005-1:2012
|
Utility connections in port - Part 1: High Voltage Shore Connection (HVSC) Systems - General requirements |