|
SAE AIR 4004 : 2015
|
GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
|
DEFSTAN 00-250(PT3)SEC13/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 13 - THE WORKPLACE |
|
MIL I 85889 : 0
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
|
15/30322573 DC : 0
|
BS ISO/IEC 33071 - INFORMATION TECHNOLOGY - PROCESS ASSESSMENT - AN INTEGRATED PROCESS CAPABILITY ASSESSMENT MODEL FOR ENTERPRISE PROCESSES |
|
PD IEC/TS 62239-2:2017
|
Process management for avionics. Management plan Preparation and maintenance of an electronic COTS assembly management plan |
|
AFGS-87213 Revision B:1993
|
DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
|
MIL-DTL-25959 Revision H:2012
|
TIE DOWN, TENSIONERS, CARGO, AIRCRAFT |
|
DOD S 87956 : 0
|
SHELTER, S-80A AND S-82A |
|
MIL T 5842 : B
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
|
MIL I 83294 : 0
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
|
MIL STD 2156 : 0
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL DTL 53135 : 0
|
AUXILIARY POWER UNIT, 10 KW, 120/240 VAC, 60 HZ |
|
SAE AS 5506/1 : 2015
|
SAE ARCHITECTURE ANALYSIS AND DESIGN LANGUAGE (AADL) ANNEX VOLUME 1: ANNEX A: ARINC653 ANNEX, ANNEX C: CODE GENERATION ANNEX, ANNEX E: ERROR MODEL ANNEX |
|
MIL L 24554 : 0
|
LAMPS MK III INTERFACE SIGNAL SWITCHING SET |
|
MIL PRF 32104 : 0
|
MOBILE HYDRAULIC OIL DISPENSER |
|
MIL G 21296 : B
|
GENERATOR SET, DIESEL ENGINE, 45O VOLT, 6O HZ AC, SINGLE AND TWIN ENGINE DRIVEN, NAVAL SHIPBOARD |
|
MIL STD 1629 : A
|
PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
|
MIL-PRF-32080 Revision G:2014
|
TRUCK, AIRCRAFT FUELING-DEFUELING, 6,000 GALLON, A/S32R-11 |
|
MIL L 53106 : 0
|
LAUNCHER, BRIDGE, LIGHT ASSAULT TOWED |
|
GEIA TA HB 0009 : 2013
|
RELIABILITY PROGRAM HANDBOOK |
|
MIL HDBK 2084 : 0
|
GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT |
|
JSGS 87231 : A
|
ENGINES, AIRCRAFT, TURBINE |
|
BS ISO/IEC 33071:2016
|
Information technology. Process assessment. An integrated process capability assessment model for Enterprise processes |
|
MIL M 8555 : C
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
|
MIL-PRF-85676 Revision A:2006
|
LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
|
ANSI A10.17 : 2006 : R2011
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
MIL STD 756 : B
|
RELIABILITY MODELING AND PREDICTION |
|
MIL A 85055 : 0
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
|
MIL I 27197 : C
|
INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
|
NASA SP 580 : 2011
|
NASA SYSTEM SAFETY HANDBOOK - VOLUME 1, SYSTEM SAFETY FRAMEWORK AND CONCEPTS FOR SYSTEM SAFETY FRAMEWORK AND CONCEPTS FOR IMPLEMENTATION |
|
DEFSTAN 00-250(PT3)SEC12/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 12 - OPERATIONS, MAINTENANCE & SUPPORT |
|
MIL HDBK 11991 : 0
|
DESIGN OF ELECTRICAL, ELECTRONIC, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPONS SYSTEMS |
|
GEIA HB 649 : 2005
|
CONFIGURATION MANAGEMENT STANDARD IMPLEMENTATION GUIDE |
|
ANSI A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
MIL HDBK 287 : 0
|
A TAILORING GUIDE FOR DOD-STD-2167, DEFENSE SYSTEM SOFTWARE DEVELOPMENT |
|
MIL STD 2124 : A
|
FLIGHT INCIDENT RECORDER/CRASH POSITION LOCATOR, MINIMUM PERFORMANCE STANDARDS FOR |
|
IEEE 1887:2017
|
WAYSIDE ENERGY STORAGE SYSTEMS FOR DC TRACTION APPLICATIONS |
|
MIL-PRF-83419 Revision F:2016
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
MIL STD 2080 : 0
|
MAINTENANCE ENGINEERING, PLANNING AND ANALYSIS FOR AERONAUTICAL SYSTEMS, SUBSYSTEMS, EQUIPMENT AND SUPPORT EQUIPMENT |
|
MIL-P-6457 Revision E:1974
|
POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
|
MIL S 0053085 : A
|
SURVEY INSTRUMENT AUTOMATED, INTEGRATED (AISI) |
|
SAE JA 1003 : 2012
|
SOFTWARE RELIABILITY PROGRAM IMPLEMENTATION GUIDE |
|
ANSI/ASSE A10.17 : 2006 : R2011
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
DI-MGMT-81398 Revision C:2014
|
HAZARDOUS MATERIALS MANAGEMENT PROGRAM (HMMP) PLAN |
|
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 |
|
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-STD-1365 Revision C:2010
|
GENERAL DESIGN CRITERIA FOR HANDLING EQUIPMENT ASSOCIATED WITH WEAPONS AND RELATED ITEMS |
|
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)/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 |
|
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MIL-DTL-53126 Revision A:2012
|
POWER DISTRIBUTION, ILLUMINATION SYSTEMS, ELECTRICAL, 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 |
|
SAE ARP 6385 : 2017
|
AIRCRAFT FUEL PUMP MECHANICAL AND ELECTRICAL SAFETY DESIGN |
|
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
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 C 85521 : 0
|
CONCENTRATOR, OXYGEN, GGU-7/A |
|
ASTM F 3201 : 2016
|
Standard Practice for Ensuring Dependability of Software Used in Unmanned Aircraft Systems (UAS) |
|
DEFSTAN 00-250(PT2)/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 2: PARTICULAR PEOPLE-RELATED REQUIREMENTS |
|
MIL R 85880 : 0
|
ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
|
DI MGMT 81826 : C
|
F/A-18 - EA-18 AIRCRAFT/SYSTEM PROGRAM PROTECTION IMPLEMENTATION PLAN |
|
MIL-STD-2097 Revision A:1989
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
|
MIL-PRF-53090 Revision B:2016
|
BLADE, MINE CLEARING |
|
MIL STD 721 : C
|
DEFINITIONS OF EFFECTIVENESS TERMS FOR RELIABILITY MAINTAINABILITY, HUMAN FACTORS, AND SAFETY |
|
MIL H 4607 : E
|
HEATER, ENGINE AND SHELTER, GROUND |
|
MIL E 4158 : E
|
ELECTRONIC EQUIPMENT, GROUND GENERAL REQUIREMENTS FOR |
|
MIL B 53107 : 0
|
BRIDGE, LIGHT ASSAULT 23 METER SPAN |
|
AFGS 87219 : B
|
ELECTRICAL POWER SYSTEMS, AIRCRAFT |
|
SAE ARP 5764 : 2013(R2018)
|
AEROSPACE ACTIVE INCEPTOR SYSTEMS FOR AIRCRAFT FLIGHT AND ENGINE CONTROLS |
|
MIL P 85710 : 0
|
PARACHUTES, PERSONNEL, EMERGENCY ESCAPE GENERAL DESIGN SPECIFICATION FOR |
|
BS ISO 4126-10:2010
|
Safety devices for protection against excessive pressure Sizing of safety valves for gas/liquid two-phase flow |
|
DEFSTAN 00-250(PT3)SEC1-7/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTIONS 1-7 - OVERALL CONTENTS/SCOPE |
|
SAE ARP 5796 : 2013
|
FLIGHT CRITICAL CONTROL VALVES, MILITARY AIRCRAFT |
|
DEFSTAN 00-250(PT3)SEC8/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 8 - PEOPLE IN SYSTEMS |
|
MIL HDBK 2067 : 0
|
AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR |
|
AIHA Z10 : 2012
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
|
MIL P 87220 : 0
|
PROPELLANT, AND EXPLOSIVE SYSTEMS, AIRCRAFT CREW ESCAPE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON, AFB OH 45433-6503 |
|
MIL STD 705 : D
|
MOBILE ELECTRIC POWER SYSTEMS |
|
MIL STD 100 : G
|
ENGINEERING DRAWINGS |
|
MIL P 85766 : 0
|
PROJECTILE, 20 MILLIMETER , TARGET PRACTICE-TRACER, PGU-30/B |
|
MIL-HDBK-510 Revision A:2014
|
AEROSPACE FUELS CERTIFICATION |
|
MIL E 50796 : 0
|
EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
|
ANSI A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
MIL STD 973 : 0
|
CONFIGURATION MANAGEMENT |
|
MIL-STD-1904 Revision B:2016
|
DESIGN AND TEST REQUIREMENTS FOR LEVEL A AMMUNITION PACKAGING |
|
MIL W 52875 : B
|
WATER QUALITY ANALYSIS SET: PREVENTIVE MEDICINE |
|
MIL STD 884 : C
|
ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION |
|
MIL M 87977 : 0
|
MAINTENANCE PLATFORM, AIRCRAFT |
|
MIL DTL 32408 : 0
|
INTEGRAL MOTOR PUMP (IMP) |
|
DEFSTAN 00-56(PT1)/5(2014) : 2014
|
SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
|
DEFSTAN 00-55(PT1)/3(2014) : 2014
|
REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
|
CSA ISO/TS 14798 : 2007
|
LIFTS (ELEVATORS), ESCALATORS AND MOVING WALKS - RISK ASSESSMENT AND REDUCTION METHODOLOGY |
|
MIL-DTL-32572 Base Document:2017
|
ANCHOR WINDLASS, ELECTRO-MECHANICAL, VERTICAL, TWO-SPEED AND VARIABLE-SPEED |
|
MIL DTL 0083833 : B
|
3000 GALLON AERIAL BULK FUEL DELIVERY SYSTEM BLADDER |
|
DOD B 24668 : 0
|
BEARING UNIT, MAIN THRUST, SUBMARINE PROPULSION SYSTEM |
|
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
|
MIL DTL 83833 : C
|
3000 GALLON AERIAL BULK FUEL DELIVERY SYSTEM BLADDER |
|
MIL HDBK 764 : 0
|
SYSTEM SAFETY ENGINEERING DESIGN GUIDE FOR ARMY MATERIAL |
|
MIL STD 1901 : A
|
MUNITION ROCKET AND MISSILE MOTOR IGNITION SYSTEM DESIGN, SAFETY CRITERIA FOR |
|
MIL P 83927 : B
|
POWER SUPPLIES, GUIDED MISSILE LAUNCHERS, SINGLE TYPES PP-2401B/A PP-2401C/A PP-2401D/A, PP-4285/A, PP-4286/A, AND COMPOSITE TYPE PP-4506/A AND PS-1037 |
|
MIL-HDBK-2097 Revision A:1997
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
|
DEFSTAN 00-250(PT3)SEC14/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 14 - THE ENVIRONMENT |
|
MIL A 85648 : 0
|
AMPLIFIER, TRAVELING WAVE TUBE |
|
MIL A 11210 : G
|
AIR CONDITIONERS: BASE MOUNTED, SELF-CONTAINED, MULTIPACKAGE-TYPE, AIR-COOLED, ELECTRIC-MOTOR-DRIVEN, 18,000 - BTU/HR |
|
MIL-STD-2131 Revision A:1991
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
|
DEFSTAN 00-250(PT3)SEC10/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 10 - SYSTEMS SAFETY |
|
DEFSTAN 00-250(PT3)SEC11/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 11 - TRAINING |
|
MIL S 83352 : B
|
SIGNAL KIT, PERSONNEL, DISTRESS, A/P25S-5A |
|
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
NFPA 130 : 2017
|
FIXED GUIDEWAY TRANSIT AND PASSENGER RAIL SYSTEMS |
|
ANSI/CSA NGV 5.1-2016 (R2020)
|
Residential fueling appliances |
|
CSA NGV 5.1 : 2016
|
RESIDENTIAL FUELING APPLIANCES |
|
MIL PRF 32168 : 0
|
VARIABLE SPEED DRIVE SYSTEM FOR INDUCTION AND SYNCHRONOUS MACHINES |
|
MIL HDBK 115 : C
|
U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
|
UFC 4-440-01 : 2014
|
UNIFIED FACILITIES CRITERIA - WAREHOUSES AND STORAGE FACILITIES |
|
SAE ARP594 : 2017
|
FUEL PUMP THERMAL SAFETY DESIGN |
|
ASME A17.7 : 2007 : R2012
|
PERFORMANCE-BASED SAFETY CODE FOR ELEVATORS AND ESCALATORS |
|
VDI 4007:2012-06
|
RELIABILITY GOALS - DETERMINATION, CHECK, REVIEW, CERTIFICATE |
|
ASME A17.7 : 2007
|
PERFORMANCE-BASED SAFETY CODE FOR ELEVATORS AND ESCALATORS |
|
MIL-HDBK-516 Revision C:2014
|
AIRWORTHINESS CERTIFICATION CRITERIA |
|
PD ISO/TS 18667:2018
|
Space systems. Capability-based Safety, Dependability, and Quality Assurance (SD&QA) programme management |
|
ANSI/ASSE Z590.3 : 2011
|
PREVENTION THROUGH DESIGN GUIDELINES FOR ADDRESSING OCCUPATIONAL HAZARDS AND RISKS IN DESIGN AND REDESIGN PROCESSES |
|
UFC 4-133-01N : Change 5
|
UNIFIED FACILITIES CRITERIA - NAVY AIR TRAFFIC CONTROL FACILITIES |
|
AAS3P-20 : 2017
|
SAFETY AND SUITABILITY FOR SERVICE ASSESSMENT TESTING OF LARGE CALIBER AMMUNITION GREATER THAN 40MM |
|
MIL S 8812 : D
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
|
MIL-G-18473 Revision B:1978
|
GENERATOR, MOTOR, AND AUXILIARY EQUIPMENT, DIRECT CURRENT, NAVAL SHIP PROPULSION |
|
MIL STD 1310 : H
|
SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY |
|
AAS3P-12 : 2017
|
SAFETY AND SUITABILITY FOR SERVICE ASSESSMENT TESTING FOR AIRCRAFT LAUNCHED MUNITIONS |
|
DEFSTAN 00-250(PT4)/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 4: HFI METHOD, TOOLS AND TECHNIQUES |
|
MIL STD 3029 : 0
|
HOT GUN COOK-OFF HAZARDS ASSESSMENT, TEST AND ANALYSIS |
|
MIL HDBK 510-1 : A
|
AEROSPACE FUELS CERTIFICATION |
|
DEFSTAN 00-250(PT0)/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 0: HUMAN FACTORS INTEGRATION |
|
SAE EIA 649/1 : 2014
|
CONFIGURATION MANAGEMENT REQUIREMENTS FOR DEFENSE CONTRACTS |
|
AASTP-4-1 : 1ED 2016 VERSION 4
|
EXPLOSIVES SAFETY RISK ANALYSIS - PART 1: GUIDELINES FOR RISK-BASED DECISIONS |
|
DEFSTAN 00-051(PT2)/1(2018) : 2018
|
ENVIRONMENTAL MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 2: GUIDANCE |
|
MIL S 85510 : 0
|
|
|
MIL C 85717 : 0
|
CARTRIDGE, 20 MILLIMETER, SEMI-ARMOR PIERCING HIGH EXPLOSIVE INCENDIARY, PGU-28/B |
|
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
|
MIL HDBK 1760 : A
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
|
MIL-PRF-32479A:2017
|
TRAILERS, LIFT - AIRCRAFT AND MISSILE ENGINE |
|
DEFSTAN 00-55(PT1)/4(2016) : 2016
|
REQUIREMENTS FOR SAFETY OF PROGRAMMABLE ELEMENTS (PE) IN DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
|
MIL-STD-1798 Revision C:2013
|
MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
|
MIL F 85596 : 0
|
FIN, RETARDER, AIR INFLATABLE BSU-85/B |
|
MIL P 87210 : 0
|
PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
|
ANSI A10.17 : 2006 : R2011
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
MIL P 85723 : 0
|
PROJECTILE, 20 MILLIMETER, SEMI-ARMOR PIERCING, HIGH EXPLOSIVE INCENDIARY PGU-28/B |
|
MIL STD 1388/2 : B
|
DOD REQUIREMENTS FOR A LOGISTIC SUPPORT ANALYSIS RECORD |
|
MIL R 87245 : 0
|
RADIO COMMUNICATION SYSTEM, AIRBORNE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA: ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
|
MIL S 18471 : G
|
|
|
MIL I 87216 : 0
|
INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
|
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 |
|
MIL HDBK 338 : B
|
ELECTRONIC RELIABILITY DESIGN HANDBOOK |
|
MIL HDBK 1763 : 0
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
|
MIL PRF 32090 : A
|
DELIVERY SYSTEM, AERIAL, BULK FUEL |
|
MIL-STD-40051-2 Revision C:2015
|
PREPARATION OF DIGITAL TECHNICAL INFORMATION FOR PAGE-BASED TECHNICAL MANUALS (TMS) |
|
MIL HDBK 2124 : 0
|
FLIGHT DATA RECORDER FUNCTIONAL STANDARDS FOR |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
DOD STD 2105 : LATEST
|
HAZARD ASSESSMENT TESTS FOR NAVY NON NUCLEAR ORDNANCE |
|
MIL-C-85248 Revision A:1984
|
CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
|
JSSG 2001 : B
|
AIR VEHICLE |
|
NASA GB 8719.13 : 0
|
NASA SOFTWARE SAFETY GUIDEBOOK |
|
MIL STD 3031 : A
|
ARMY BUSINESS RULES FOR S1000D: INTERNATIONAL SPECIFICATION FOR TECHNICAL PUBLICATIONS UTILIZING A COMMON SOURCE DATA BASE |
|
MIL PRF 62430 : B
|
HARNESS ASSEMBLY, THERMOCOUPLE |
|
DEFSTAN 00-56(PT2)/2(1996) : 1996
|
SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 2: GUIDANCE |
|
MIL M 38780 : A
|
MANUAL,TECHNICAL, NONDESTRUCTIVE INSPECTION |
|
NASA HDBK 8739.23 : 2016
|
NASA COMPLEX ELECTRONICS HANDBOOK FOR ASSURANCE PROFESSIONALS |
|
MIL C 63541 : 0
|
CANNON 8 INCH HOWITZER, M201/M201A1 |
|
DEFSTAN 00-051(PT1)/1(2018) : 2018
|
ENVIRONMENTAL MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 1: REQUIREMENTS |
|
GEIASTD0007B:2013
|
LOGISTICS PRODUCT DATA |
|
MIL-STD-1543 Revision B:1988
|
RELIABILITY PROGRAM REQUIREMENTS FOR SPACE AND LAUNCH VEHICLES |
|
MIL P 24568 : A
|
POWER SUPPLY, D.C., FOR OXYGEN GENERATOR |
|
MIL T 27200 : C
|
TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
|
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
MIL I 8700 : A
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-250(PT3)SEC15/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 15 - WORK EQUIPMENT |
|
ANSI/ASSE Z10 : 2012(R2017)
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
|
FAA AC 431.35-2 : 2005
|
REUSABLE LAUNCH AND REENTRY VEHICLE SYSTEM SAFETY PROCESS |
|
SAE AIR 5774 : 2012
|
COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
|
DEFSTAN 00-56(PT1)/6(2015) : 2015
|
SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 1: REQUIREMENTS AND GUIDANCE |
|
SAE ARP 5783 : 2012
|
HEALTH AND USAGE MONITORING METRICS, MONITORING THE MONITOR |
|
CSA/ANSI NGV 5.2-2017
|
Vehicle fueling appliances (VFA) |
|
IEC TS 62239-2:2017
|
Process management for avionics - Management plan - Part 2: Preparation and maintenance of an electronic COTS assembly management plan |
|
SAE AIR 6027 : 2017
|
CONSIDERATIONS FOR SAFE STORE OPERATION ON MANNED AND UNMANNED VEHICLES |
|
ANSI B11.0 : 2015
|
SAFETY OF MACHINERY - GENERAL REQUIREMENTS AND RISK ASSESSMENT |
|
ASCE 21 96 : 1997
|
AUTOMATED PEOPLE MOVER STANDARDS - PART 1 |
|
ANSI/ASSE Z590.3 : 2011
|
PREVENTION THROUGH DESIGN GUIDELINES FOR ADDRESSING OCCUPATIONAL HAZARDS AND RISKS IN DESIGN AND REDESIGN PROCESSES |
|
ANSI/ASSE A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
ISO/IEC 33071:2016
|
Information technology Process assessment An integrated process capability assessment model for Enterprise processes |
|
AOP 52 : 2016
|
GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS |
|
ANSI/ASSP Z244.1:2016
|
THE CONTROL OF HAZARDOUS ENERGY LOCKOUT, TAGOUT AND ALTERNATIVE METHODS |
|
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
ISO 4126-10:2010
|
Safety devices for protection against excessive pressure Part 10: Sizing of safety valves for gas/liquid two-phase flow |
|
CSA B44.7 : 2007 : R2012
|
PERFORMANCE-BASED SAFETY CODE FOR ELEVATORS AND ESCALATORS |
|
MIL-DTL-53078 Revision A:2011
|
MOUNTING KIT: M1 TANK CLEARED LANE MARKING SYSTEM (CLAMS) |
|
NASA STD 8719.24 : 2011
|
NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
|
ASME A17.7-2007/CSA B44.7-07 (R2017)
|
Performance-Based Safety Code for Elevators and Escalators (Bi-National standard, with ASME A17.7) |
|
CSA B44.7 : 2007
|
PERFORMANCE-BASED SAFETY CODE FOR ELEVATORS AND ESCALATORS |
|
ISO/TS 14798:2006
|
Lifts (elevators), escalators and moving walks Risk assessment and reduction methodology |
|
MIL-HDBK-272 Revision A:1993
|
NUCLEAR WEAPONS SYSTEMS, SAFETY DESIGN AND EVALUATION CRITERIA FOR |
|
RE.AERO 70110 : A1998
|
SAFETY CONSTRUCTION PRINCIPLE FOR A MISSILE OR SPACE PRODUCT |
|
IEEE 7-4.3.2-2016
|
STANDARD CRITERIA FOR DIGITAL COMPUTERS IN SAFETY SYSTEMS OF NUCLEAR POWER GENERATING STATIONS |
|
NFPA 551 : 2016
|
EVALUATION OF FIRE RISK ASSESSMENTS |
|
SSPC-CPC 1 : 2016
|
CORROSION PREVENTION AND CONTROL PLANNING |
|
MIL STD 3035 : 0
|
DESIGN CRITERIA STANDARD - USAF AIRCRAFT ARRESTING SYSTEMS |
|
MIL PRF 32390 : 0
|
ENGAGING DEVICE, AIRCRAFT ARRESTING SYSTEM - USAF PENDANT CABLE RETRACTION SYSTEMS (PCRS) |
|
IEEE DRAFT 1474.1 : D8.0 JUL 99
|
DRAFT STANDARD FOR COMMUNICATIONS-BASED TRAIN CONTROL (CBTC) PERFORMANCE AND FUNCTIONAL REQUIREMENTS |
|
MIL S 9479 : C
|
|
|
MIL-W-52874 Revision B:1983
|
WATER QUALITY ANALYSIS SET, ENGINEER |
|
MIL L 52325 : D
|
LAUNCHER, TRANSPORTER, BRIDGE M48A5 OR M60A1 TANK CHASSIS |
|
DD ISO/TS 14798:2006
|
LIFTS (ELEVATORS), ESCALATORS AND MOVING WALKS - RISK ASSESSMENT AND REDUCTION METHODOLOGY |
|
MIL M 4819 : D
|
MOTOR GENERATOR, SKID MOUNTED, TYPE MD 3 |
|
DEFSTAN 00-056(PT2)/5(2017) : 2017
|
SAFETY MANAGEMENT REQUIREMENTS FOR DEFENCE SYSTEMS - PART 2: GUIDANCE ON ESTABLISHING A MEANS OF COMPLYING WITH PART 1 |
|
DOD HDBK 791 : 0
|
MAINTAINABILITY DESIGN TECHNIQUES |
|
MIL DTL 32392 : A
|
AIRCRAFT ARRESTING SYSTEM - TEXTILE (TAAS) |
|
ADS-63-SP : 2001
|
AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS |
|
MIL-DTL-49314 Revision B:2008
|
ANTENNAS, UHF, SATCOM, PORTABLE, FOLDABLE, (LIGHT WEIGHT, MEDIUM WEIGHT, AND HEAVY DUTY), GENERAL SPECIFICATION FOR |
|
ANSI B11 TR3 : 2000
|
RISK ASSESSMENT AND RISK REDUCTION - A GUIDE TO ESTIMATE, EVALUATE AND REDUCE RISKS ASSOCIATED WITH MACHINE TOOLS |
|
17/30318744 DC : 0
|
BS ISO 20188 - SPACE SYSTEMS - PRODUCT ASSURANCE REQUIREMENTS FOR COMMERCIAL SATELLITES |
|
MIL G 83380 : 0
|
GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
|
MIL P 83126 : A
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
|
MIL-I-8671 Revision D:1994
|
INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
|
MIL-HDBK-1222 Revision F:2015
|
GUIDE TO THE GENERAL STYLE AND FORMAT OF U.S. ARMY WORK PACKAGE TECHNICAL MANUALS |
|
MIL HDBK 515 : 0
|
WEAPON SYSTEM INTEGRITY GUIDE (WSIG) |
|
MIL S 23069 : A
|
SAFETY REQUIREMENTS, MINIMUM, FOR AIR LAUNCHED GUIDED MISSILES |
|
RG.AERO 00040 : 1999
|
GENERAL RECOMMENDATION FOR THE PROGRAMME MANAGEMENT SPECIFICATION |
|
MIL STD 2067 : 0
|
AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR |
|
JSSG 2010 12 : 0
|
CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK |
|
MIL-E-38453 Revision A:1971
|
ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-250(PT3)SEC16/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 16 - LIVING SPACES |
|
MIL S 48405 : 0
|
SHIELDED AND CONFINED MILD DETONATING CORD ASSEMBLIES |
|
MIL HDBK 514 : 0
|
OPERATIONAL SAFETY, SUITABILITY, & EFFECTIVENESS FOR THE AERONAUTICAL ENTERPRISE |
|
MIL A 0083216 : C
|
AIR CONDITIONER, HORIZONTAL, 54,000 BTUH, 208/230 V |
|
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
SAE ARP 1070E : 2019
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
ANSI/ASSE A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
MIL B 52088 : F
|
BRIDGE, ARMOURED VEHICLE LAUNCHED, SCISSORING TYPE, CLASS 60, ALUMINUM, 60 FOOT SPAN |
|
MIL P 85573 : 0
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
|
CEI CLC/TR 50126-2 : 2008
|
RAILWAY APPLICATIONS - THE SPECIFICATION AND DEMONSTRATION OF RELIABILITY, AVAILABILITY, MAINTAINABILITY AND SAFETY (RAMS) - PART 2: GUIDE TO THE APPLICATION OF EN 50126-1 FOR SAFETY |
|
MIL G 70617 : B
|
GUNFIRE SIMULATOR: 12725085-1 |
|
SAE ARP 5150 : 2013
|
SAFETY ASSESSMENT OF TRANSPORT AIRPLANES IN COMMERCIAL SERVICE |
|
MIL E 18927 : E
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
MIL B 29595 : 0
|
BATTERIES AND CELLS, LITHIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE AS 6479 : 2014
|
SPLICER, FUSION, FIBER OPTIC, AEROSPACE |
|
PREN 9200 : 200P1
|
AEROSPACE SERIES - PROGRAMME MANAGEMENT - GUIDELINES FOR PROJECT MANAGEMENT SPECIFICATION |
|
SAE ARP 1070 : 2014
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
ANSI/ASSE Z10 : 2012(R2017)
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
|
ASTM F 1337 : 2010
|
Standard Practice for Human Engineering Program Requirements for Ships and Marine Systems, Equipment, and Facilities |
|
BS EN 9200:2004
|
AEROSPACE SERIES - PROGRAMME MANAGEMENT - GUIDELINES FOR PROJECT MANAGEMENT SPECIFICATION |
|
MIL-STD-1474 Revision E:2015
|
NOISE LIMITS |
|
EN 9200:2004
|
Aerospace series - Programme management - Guidelines for project management specification |
|
MIL STD 1425 : A
|
SAFETY DESIGN REQUIREMENTS FOR MILITARY LASERS AND ASSOCIATED SUPPORT EQUIPMENT |
|
DEFSTAN 00-250(PT3)SEC9/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 9 - PEOPLE CHARACTERISTICS |
|
MIL A 87211 : NOTICE 1
|
AIR DATA SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD ENES, WRIGHT PATTERSON, AFB OH 45433 6503 |
|
MIL W 81752 : A
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
|
MIL STD 1512 : 0
|
ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
|
MIL STD 1367 : A
|
PACKAGING, HANDLING, STORAGE, AND TRANSPORTABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
|
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
|
MIL M 4818 : D
|
MOTOR GENERATOR, SKID MOUNTED, TYPE MD 2 |
|
MIL S 87238 : 0
|
SURVIVAL AND FLOTATION SYSTEM, AIRBORNE |
|
MIL M 87222 : 0
|
MECHANICAL SYSTEMS FOR AIRCRAFT DOORS AND CANOPIES |
|
EIA 933 : 2015
|
REQUIREMENTS FOR A COTS ASSEMBLY MANAGEMENT PLAN |
|
MIL STD 1530 : D
|
AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
|
MIL STD 633 : G
|
STANDARD FAMILY OF MOBILE ELECTRIC POWER GENERATING SOURCES - GENERAL DESCRIPTION INFORMATION AND CHARACTERISTIC DATA |
|
MIL-STD-40051-1 Revision C:2015
|
PREPARATION OF DIGITAL TECHNICAL INFORMATION FOR INTERACTIVE ELECTRONIC TECHNICAL MANUALS (IETMS) |
|
MIL L 85762 : A
|
LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
|
MIL HDBK 525 : 0
|
ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) INTEGRITY PROGRAM |
|
JSSG 2009 : A
|
AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE) |
|
MIL-D-18300 Revision H:1993
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
|
MIL D 8708 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
|
AIHA Z10 : 2012
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
|
ASTM F 1337 : 2010 : R2015
|
Standard Practice for Human Systems Integration Program Requirements for Ships and Marine Systems, Equipment, and Facilities |
|
MIL HDBK 1024/1 : 0
|
AVIATION OPERATIONAL AND SUPPORT FACILITIES |
|
MIL STD 2084 : 0
|
GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT |
|
DEFSTAN 00-25(PT21)/1(2004) : 2004
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 21: SYSTEM SAFETY DOMAIN |
|
MIL I 83117 : B
|
INDICATOR, ANGLE OF ATTACK |
|
MIL C 87970 : 0
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
|
MIL H 53076 : 1987
|
HEMTT TANKER AVIATION REFUELING SYSTEM (HTARS) |
|
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
|
MIL L 85314 : A
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
|
MIL G 25591 : E
|
GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
|
EIA 836 CD : B2010(R2015)
|
CONFIGURATION MANAGEMENT DATA EXCHANGE AND INTEROPERABILITY |
|
MIL P 24587 : 0
|
POWER SUPPLY, UNINTERRUPTIBLE, SOLID STATE (NAVAL SHIPBOARD) |
|
MIL T 85549 : 0
|
TEST PROGRAM SET (TPS) OPERATIONAL TEST PROGRAM SETS (OTPS) FOR F/A-18 (UNITS UNDER TEST (UUU), GENERAL SPECIFICATION FOR |
|
MIL-M-4820 Revision E:1979
|
MOTOR GENERATOR, SKID MOUNTED TYPE MD 4 |
|
MIL STD 1606 : A
|
TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS |
|
ADS-65-HDBK : 2004
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
|
MIL A 49314 : 0
|
ANTENNAS, UHF SATCOM, PORTABLE, FOLDABLE (LIGHT WEIGHT, MEDIUM WEIGHT & HEAVY DUTY), GENERAL SPECIFICATION FOR |
|
MIL PRF 32470 : 0
|
TRUCK, FORKLIFT, 10,000 LB CAPACITY, VARIABLE REACH, ROUGH TERRAIN |
|
MIL P 85767 : 0
|
PROJECTILE, 20 MILLIMETER, TARGET PRACTICE PGU-27/B |
|
MIL-STD-2105 Revision D:2011
|
HAZARD ASSESSMENT TESTS FOR NON-NUCLEAR MUNITIONS |
|
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL T 81821 : 0
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
|
MIL A 85434 : A
|
AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
|
ANSI/ASSE Z244.1 : 2016
|
THE CONTROL OF HAZARDOUS ENERGY LOCKOUT, TAGOUT AND ALTERNATIVE METHODS |
|
DEFSTAN 00-250(PT1)/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 1: OVERARCHING PEOPLE-RELATED REQUIREMENTS |
|
MIL D 52842 : A
|
DRIER, X-RAY, FILM FORCED AIR, WALL MOUNTED |
|
SAE ARP 5794 : 2014
|
CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
|
ANSI/ASSE A10.17 : 2006 : R2011
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
|
SAE ARP 4943 : 2008
|
GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR |
|
SAE ARP 1595 : 2013(R2019)
|
DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
|
ISO/TS 18667:2018
|
Space systems — Capability-based Safety, Dependability, and Quality Assurance (SD&QA) programme management |
|
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
SAE ARP 5415 : 2008
|
USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING |
|
SAE ARP6128:2013
|
UNMANNED SYSTEMS TERMINOLOGY BASED ON THE ALFUS FRAMEWORK |
|
AAS3P-11 : 2017
|
SAFETY AND SUITABILITY FOR SERVICE ASSESSMENT TESTING FOR SURFACE AND UNDERWATER LAUNCHED MUNITIONS |
|
AAS3P-10 : 2011
|
SAFETY AND SUITABILITY FOR SERVICE ASSESSMENT TESTING FOR SHOULDER LAUNCHED MUNITIONS |
|
DI-MISC-81397 Revision C:2014
|
HAZARDOUS MATERIALS MANAGEMENT PROGRAM (HMMP) REPORT |