MIL A 83783 : 0
|
ADAPTER, TEST, MX-9042/G |
DOD C 24529 : 0
|
CHARGERS, BATTERY, LIFT TRUCK AND PALLET TRANSPORTER BATTERY SERVICE (METRIC) |
DEFSTAN 00-250(PT3)SEC13/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 13 - THE WORKPLACE |
MIL S 52256 : C
|
SURVEYING INSTRUMENT; AZIMUTH GYRO, LIGHTWEIGHT |
MIL DTL 15514 : G
|
TELEPHONE EQUIPMENT, SOUND POWERED TELEPHONE HANDSET, HEADSET - CHEST SET, AND HEADSET - CHEST SET, NOISE ATTENUATING |
MIL R 71126 : 0
|
RIFLE, 7.62 MILLIMETER, SNIPER W/DAY OPTICAL SIGHT AND CARRYING CASES - M24 |
AFGS 87213 : B
|
DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
MIL I 24728 : A
|
INTERCONNECTION BOX, FIBER OPTIC, METRIC, GENERAL SPECIFICATION FOR |
MIL PRF 32366 : 0
|
GRIP/BIPOD, FORWARD |
MIL L 85762 : A
|
LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
MIL C 52972 : A
|
COMPRESSOR UNIT, 5 CFM, 3200 PSI, DIESEL ENGINE DRIVEN, DIVING AIR |
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 C 87979 : 0
|
CLOCK, AIRCRAFT, ELECTRONIC |
MIL E 16400 : H
|
ELECTRONIC, INTERIOR COMMUNICATIONS AND NAVIGATION EQUIPMENT, NAVAL SHIP AND SHORE, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT1)SEC4/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
MIL DTL 53135 : 0
|
AUXILIARY POWER UNIT, 10 KW, 120/240 VAC, 60 HZ |
DEFSTAN 00-970(PT1)SEC4/4(2006) : 2006
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 4: DESIGN AND CONSTRUCTION |
MIL S 55389 : 0
|
SUPPRESSOR, ELECTRICAL TRANSIENT, MX-7778A/GRC |
MIL DTL 32403 : 0
|
FIRE EXTINGUISHER, EMPLOYING HFC-227EA AGENT ENHANCED WITH SPECIAL SODIUM BICARBONATE POWDER (HFC-227EA/SBC[S]), PORTABLE, WITH BRACKET |
MIL PRF 32080 : G
|
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 |
MIL B 734 : E
|
BREAKER, PAVING, GASOLINE POWERED, SELF CONTAINED |
MIL DTL 0045150 : M
|
CHASSIS, TRAILER, 2-WHEEL CART TYPE 1/4 TO 3-1/2 TON |
MIL A 23798 : C
|
AIR CONDITIONER, FAN-COIL ASSEMBLY |
MIL M 8555 : C
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
17/30334566 DC : 0
|
BS ISO 10968 - EARTH-MOVING MACHINERY - OPERATOR'S CONTROLS |
SAE AMS 3695 : 2014
|
ADHESIVE FILM, EPOXY-BASE, FOR HIGH DURABILITY STRUCTURAL ADHESIVE BONDING |
03/304741 DC : DRAFT APR 2003
|
IEC 60601-1-6 ED.1 - MEDICAL ELECTRICAL EQUIPMENT - PART 1-6: GENERAL REQUIREMENTS FOR SAFETY - COLLATERAL STANDARD - USABILITY |
MIL T 53048 : C
|
TANK, FABRIC, COLLAPSIBLE; AIR COLUMN SUPPORTED, OPEN TOP, WATER STORAGE 3000 GALLONS |
MIL PRF 71185 : A
|
DYNAMIC REFERENCE UNIT-HYBRID-REPLACEMENT (DRU-H-R) |
MIL PRF 85676 : A
|
LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
MIL STD 188/322 : 0
|
SUBSYSTEM DESIGN ENGINEERING AND EQUIPMENT TECHNICAL DESIGN STANDARDS FOR LONG HAUL LINE OF SIGHT (LOS) DIGITAL MICROWAVE RADIO TRANSMISSION |
MIL A 85055 : 0
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
DIN EN 894-4:2010-11
|
Safety of machinery - Ergonomics requirements for the design of displays and control actuators - Part 4: Location and arrangement of displays and control actuators |
MIL C 52980 : B
|
COMPRESSOR, RECIPROCATING AND ROTARY, GASOLINE ENGINE DRIVEN, AIR |
MIL DTL 23599 : C
|
HOOK, RESCUE |
MIL DTL 32529 : 0
|
POWER ELECTRONIC CONVERSION EQUIPMENT, NAVAL SHIPBOARD |
DEFSTAN 00-250(PT3)SEC12/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 12 - OPERATIONS, MAINTENANCE & SUPPORT |
MIL PRF 32272 : A
|
INTEGRATED POWER MANAGEMENT CENTER (IPMC) |
MIL HDBK 11991 : 0
|
DESIGN OF ELECTRICAL, ELECTRONIC, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPONS SYSTEMS |
MIL HDBK 470 : A
|
DESIGNING AND DEVELOPING MAINTAINABLE PRODUCTS AND SYSTEMS - VOLUME 1 |
MIL C 555 : L
|
COMPRESSOR, AIR RECIPROCATING AND ROTARY, DIESEL ENGINE DRIVEN |
MIL B 53081 : 0
|
BERM LINER ASSEMBLIES |
MIL P 85833 : 0
|
PROTECTIVE ASSEMBLY, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL |
DEFSTAN 00-25(PT20)/1(2004) : 2004
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 20: HEALTH HAZARD ASSESSMENT DOMAIN |
MIL F 24638 : 0
|
FREQUENCY CHANGER, SOLID STATE, AIR COOLED (NAVAL SHIPBOARD) |
MIL I 82787 : 0
|
IGNITER ASSEMBLY, ROCKET MOTOR MK 104 |
MIL STD 1522 : A
|
STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS |
ANSI A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
MIL PRF 32518 : 0
|
INTERIOR HEAD IMPACT PROTECTION FOR USE IN U.S. ARMY MILITARY VEHICLE INTERIORS |
NASA KSC STD Z 0006 : 1995
|
DESIGN OF HYPERGOLIC PROPELLANTS GROUND SUPPORT EQUIPMENT, STANDARD FOR |
MIL PRF 32389 : 0
|
LOAD BANK, ELECTRICAL |
MIL A 49067 : A
|
AIR TRAFFIC CONTROL CENTRAL AN/TSW-7A |
MIL D 70789 : A
|
DYNAMIC REFERENCE UNIT (DRU) |
MIL C 28858 : A
|
COUPLER GROUP, ANTENNA, OA-9123/SRC |
MIL V 62547 : A (1)
|
VALVE AND CYLINDER ASSEMBLIES, HALON |
MIL STD 203 : G
|
AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT |
NFL 76 011 : 1997
|
AEROSPACE SERIES - CONTROL AND VIEWING ELEMENTS - INTERACTIVE FRONT FACE - TECHNICAL SPECIFICATION |
MIL M 87268 : 1992
|
MANUALS, INTERACTIVE ELECTRONIC TECHNICAL - GENERAL CONTENT, STYLE, FORMAT & USER-INTERACTION REQUIREMENTS |
MIL S 28867 : 0
|
SWITCH, TRANSFER, FREQUENCY STANDARD |
MIL HDBK 412 : 0
|
SITE SURVEY & FACILITY DESIGN HANDBOOK FOR SATELLITE EARTH STATIONS |
MIL T 83823 : 0
|
TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
MIL STD 2080 : 0
|
MAINTENANCE ENGINEERING, PLANNING AND ANALYSIS FOR AERONAUTICAL SYSTEMS, SUBSYSTEMS, EQUIPMENT AND SUPPORT EQUIPMENT |
MIL B 385 : G
|
BREAKERS, PAVING, PNEUMATIC-POWERED (7/8-INCH HEXAGON BY 2-3/4-INCH CHUCK AND 7/8-INCH HEXAGON BY 3-1/4-INCH CHUCK) |
MIL HDBK 1473 : A
|
COLOR AND MARKING OF ARMY MATERIEL |
JSSG 2010 7 : 0
|
CREW SYSTEMS - CRASH PROTECTION HANDBOOK |
SAE AS 6479 : 2014
|
SPLICER, FUSION, FIBER OPTIC, AEROSPACE |
MIL F 85406 : 0
|
FUSE SYSTEM, JOINT SERVICE ELECTRONIC BOMB FMU-139/B |
MIL STD 1816 : 0
|
PRESERVATION, PACKAGING & PACKING OF RUBBER & NYLON FUEL, OIL & WATER-ALCOHOL CELLS |
MIL T 25620 : C
|
TESTER, OXYGEN MASK, HEADSET AND MICROPHONE, TYPE MQ-1A |
MIL R 85669 : 0
|
REPEATER SET, RADIO, POD AN/ARQ-49 |
MIL D 87213 : 0
|
DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL I 49394 : A
|
INTERROGATOR SET AN/TPX-46A(V)7 |
MIL A 28890 : 0
|
ANTENNA GROUP, OE-207/BR |
NASA PRC 9002 : 2012
|
PROCESS SPECIFICATION FOR PART MARKING |
MIL B 53067 : 0
|
BOAT, RECONNAISSANCE/LANDING ASSAULT, INFLATABLE: 3-, 7-, 15-PERSON |
MIL B 24535 : A
|
BURNER, CARBON MONOXIDE AND HYDROGEN, CATALYTIC TYPE (MARK V) |
ARINC 837 : 2011
|
DESIGN GUIDELINES FOR AIRCRAFT CABIN HUMAN MACHINE INTERFACES |
JSSG 2010 5 : 0
|
CREW SYSTEMS AIRCRAFT LIGHTING HANDBOOK |
MIL S 0053085 : A
|
SURVEY INSTRUMENT AUTOMATED, INTEGRATED (AISI) |
SAE ARP 4945 : 2013
|
AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
AAMI HE75 : 2009(R2013)
|
HUMAN FACTORS ENGINEERING - DESIGN OF MEDICAL DEVICES |
ARINC 791-1 : 2014
|
MARK 1 AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM - PART 1: PHYSICAL INSTALLATION AND AIRCRAFT INTERFACES |
SAE AIR 1093 : 2002
|
NUMERAL, LETTER AND SYMBOL DIMENSIONS FOR AIRCRAFT INSTRUMENT DISPLAYS |
SAE ARP 5677 : 2012
|
HUMAN ENGINEERING CONSIDERATIONS FOR AIRBORNE IMPLEMENTATION OF ENHANCED SYNTHETIC VISION SYSTEMS |
SAE USCAR 25-1 : 2008
|
ERGONOMICS SPECIFICATION FOR ELECTRICAL CONNECTIONS |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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 |
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)/12(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)/8(2011) : 2011
|
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 |
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
SAE ARP 6253 : 2017
|
LEDS AND AIRCRAFT APPLICATIONS |
MIL C 85521 : 0
|
CONCENTRATOR, OXYGEN, GGU-7/A |
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 |
MIL P 71012 : A
|
PISTOL, SEMIAUTOMATIC, COMPACT, 9MM: M11 |
MIL R 81876 : B
|
RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
MIL C 28779 : B
|
COMBINER, EXTENDED FREQUENCY RANGE CU-2OO7 (/SRR) |
MIL STD 2097 : A
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL PRF 53090 : B
|
BLADE, MINE CLEARING |
MIL P 52632 : D
|
POWER PLANT, UTILITY:MUST HOSPITAL SYSTEM |
MIL C 0052980 : C
|
COMPRESSORS, RECIPROCATING AND ROTARY, AIR DIESEL-ENGINE-DRIVEN, OR GASOLINE-ENGINE-DRIVEN |
AAMI HE74 : 2001
|
HUMAN FACTORS DESIGN PROCESS FOR MEDICAL DEVICES |
MIL R 85111 : A
|
RECOVERY ASSIST SECURING AND TRAVERSING SYSTEM FOR LAMPS MK 111 HELICOPTER |
MIL A 24775 : 0
|
AIR CONDITIONING FAN COIL UNITS, HORIZONTAL AND VERTICAL TYPES, NAVAL SHIPBOARD |
DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
DEFSTAN 00-970(PT1)SEC4/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
MIL B 53107 : 0
|
BRIDGE, LIGHT ASSAULT 23 METER SPAN |
DEFSTAN 00-970(PT1)SEC4/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION |
DEFSTAN 00-970(PT1)SEC4/6(2010) : 2010
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FORD SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
MIL HDBK 244 : A
|
GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
MIL T 52942 : C
|
TRUCK, FIRE FIGHTING: PUMPER, 1000 GPM; LADDER/WATER TOWER COMBINATION |
MIL P 85710 : 0
|
PARACHUTES, PERSONNEL, EMERGENCY ESCAPE GENERAL DESIGN SPECIFICATION FOR |
MIL STD 2156 : 0
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
DEFSTAN 00-250(PT4)/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 4: HFI METHOD, TOOLS AND TECHNIQUES |
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 |
DEFSTAN 00-250(PT3)SEC8/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 8 - PEOPLE IN SYSTEMS |
MIL C 00555 : K
|
COMPRESSORS, AIR, RECIPROCATING AND ROTARY, DIESEL ENGINE DRIVEN |
MIL S 12840 : H
|
SADDLE ASSEMBLY, STEEL AND PLYWOOD, FOR 24-TON, 2-PART PNEUMATIC FLOAT, PONTOON BRIDGE |
DEFSTAN 00-970(PT1)SEC4/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION |
MIL PRF 83817 : C
|
TRUCK, LIFT, FORK, 4,000 POUND CAPACITY, VARIABLE REACH, ROUGH TERRAIN |
MIL S 4880 : G NOTICE 1
|
SWEEPER, MAGNET, SELF-PROPELLED |
MIL HDBK 2067 : 0
|
AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR |
DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
MIL PRF 32521 : A
|
EXPEDITIONARY SHELTER PROTECTION SYSTEM (ESPS) PANEL MODULE |
MIL STD 188/125 : A
|
HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C41 FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS - VOLUME 1 - FIXED FACILITIES (METRIC) |
GEIA HEB 1 : 2005
|
HUMAN ENGINEERING - PRINCIPLES AND PRACTICES |
RIA R15.02 1 : 1990
|
INDUSTRIAL ROBOTS AND ROBOT SYSTEMS - HAND-HELD ROBOT CONTROL PENDANTS - HUMAN ENGINEERING DESIGN CRITERIA |
NASA KSC STD P 0001 : 1992
|
PREPARATION OF EQUIPMENT OR SYSTEM PROCUREMENT/PERFORMANCE SPECIFICATIONS, STANDARD FOR |
AIHA Z10 : 2012
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
MIL STD 705 : D
|
MOBILE ELECTRIC POWER SYSTEMS |
MIL H 5440 : H
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
DEFSTAN 00-25(PT14)/1(2000) : 2000
|
HUMAN FACTORS FOR DESIGNERS OF EQUIPMENT - PART 14: MILITARY LAND VEHICLE DESIGN |
MIL HDBK 258 : 0
|
INTERFACE CONTROL DOCUMENT FOR INFRARED DETECTING SET AN/AAS-36 |
MIL D 55361 : 0
|
DETECTOR, TRACKING SERVO BRIDGE |
DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
MIL T 52964 : 0
|
TOPOGRAPHIC SUPPORT SYSTEM OPERA STORAGE & RETRIEVAL, DISTRIBUTION DRAFTING SUPPORT, COMPILATION, SURVEY, RECTIFIER I & II MOSAICKING DRAFTING, COLLECTION, ANALYSIS, INFORMATION AND SYNTHESIS SECTIONS, SEMITRAILER MOUNTED |
AIHA Z10 : 2012
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
ASTM F 1166 : 2007 : R2013
|
Standard Practice for Human Engineering Design for Marine Systems, Equipment, and Facilities |
MIL DTL 15024 : F
|
PLATES AND TAGS FOR IDENTIFICATION OF EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL STD 1904 : B
|
DESIGN AND TEST REQUIREMENTS FOR LEVEL A AMMUNITION PACKAGING |
MIL P 10360 : G
|
PUMP, CENTRIFUGAL 4 INCH AND 6 INCH, GASOLINE ENGINE AND DIESEL ENGINE DRIVEN FOR WATER |
MIL I 85671 : 0
|
INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
MIL B 53083 : 0
|
BAG, WATERPROOF, LOAD CARRYING; SPECIAL OPERATIONS WATERPROOF BAG (SOWB) |
IEEE 15288.2 : 2014
|
TECHNICAL REVIEWS AND AUDITS ON DEFENSE PROGRAMS |
MIL P 52746 : C
|
PUMP ASSEMBLY, FLAMMABLE LIQUID, CENTRIFUGAL, SELF PRIMING 2 INCH 100 GPM AT 100 FEET TOTAL DYNAMIC HEAD |
MIL T 49124 : 0
|
TEST SET, LASER RANGEFINDER, TS-3620( )/GVS-5 |
MIL E 83510 : A
|
EARPHONE ELEMENT |
MIL W 52875 : B
|
WATER QUALITY ANALYSIS SET: PREVENTIVE MEDICINE |
MIL STD 907 : B
|
ENGINEERING AND DESIGN CRITERIA FOR SHELTERS, EXPANDABLE AND NONEXPANDABLE |
MIL STD 884 : C
|
ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION |
MIL M 87977 : 0
|
MAINTENANCE PLATFORM, AIRCRAFT |
EI GUIDANCE ON MANAGING HUMAN : 1ED 2010
|
GUIDANCE ON MANAGING HUMAN AND ORGANISATIONAL FACTORS IN DECOMMISSIONING |
FAA AC 20-175 : 2011
|
CONTROLS FOR FLIGHT DECK SYSTEMS |
MIL DTL 32572 : 0
|
ANCHOR WINDLASS, ELECTRO-MECHANICAL, VERTICAL, TWO-SPEED AND VARIABLE-SPEED |
MIL DTL 0083833 : B
|
3000 GALLON AERIAL BULK FUEL DELIVERY SYSTEM BLADDER |
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
AAMI HE74 : 2001 : R2009
|
HUMAN FACTORS DESIGN PROCESS FOR MEDICAL DEVICES |
DEFSTAN 00-970(PT1)SEC4/5(2007) : 2007
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 4: DESIGN AND CONSTRUCTION |
MIL R 52255 : D
|
REPAIR KIT AND REPAIR KIT COMPONENTS, FOR COLLAPSIBLE FABRIC TANKS, DRUMS, AND BOATS |
MIL S 87233 : 0
|
SUPPORT EQUIPMENT SYSTEMS (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL DTL 83833 : C
|
3000 GALLON AERIAL BULK FUEL DELIVERY SYSTEM BLADDER |
MIL STD 2525 : D
|
JOINT MILITARY SYMBOLOGY |
MIL D 52840 : 0
|
DETECTOR, BATCH INTERFACE |
DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
MIL I 82826 : 0
|
IGNITER ASSEMBLY |
MIL F 24713 : 0
|
FREQUENCY CHANGER, STATIC, AIR COOLED (NAVAL SHIPBOARD) |
MIL HDBK 2097 : A
|
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 H 11511 : G
|
HEATER, SPACE, MULTIFUEL, WITH BLOWER 60,000 BTU/HR |
DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
MIL A 85648 : 0
|
AMPLIFIER, TRAVELING WAVE TUBE |
MIL STD 2131 : A
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL PRF 32278 : B
|
GAUGE, TACTICAL AUTOMATED TANK (TATG) - FUELS OPERATIONAL READINESS CAPABILITY EQUIPMENT (FORCE) |
MIL PRF 32363 : 0
|
SLING, TACTICAL |
MIL B 53102 : 0
|
BERM LINER ASSEMBLIES, ARCTIC SERVICE |
DEFSTAN 00-250(PT3)SEC10/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 10 - SYSTEMS SAFETY |
MIL M 85831 : 0
|
MASK, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE, NON-OXYGEN |
MIL C 4150 : J
|
CASE, TRANSIT AND STORAGE, WATERPROOF AND WATER-VAPORPROOF |
MIL E 11991 : E
|
ELECTRONIC, ELECTRICAL, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPON SYSTEMS, GENERAL SPECIFICATION FOR |
MIL HDBK 87244 : 0
|
AVIONICS/ELECTRONICS INTEGRITY |
MIL S 83129 : A
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
MIL C 52037 : F
|
COMPRESSOR UNIT, RECIPROCATING, POWER DRIVEN, AIR, 15 CFM 3,500 PSI |
DEFSTAN 00-250(PT3)SEC11/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 3: TECHNICAL GUIDANCE - SECTION 11 - TRAINING |
MIL T 53055 : C
|
TANK, 3,000 GALLON & 4600 GALLON FABRIC, COLLAPSIBLE, DRINKING WATER, SEMI-TRAILER MOUNTED |
MIL R 52915 : B
|
RECHARGE/RECOVERY UNIT, FIRE EXTINGUISHER, MONOBROMOTRIFLUOROMETHANE (CF3BR) PNEUMATIC POWERED |
MIL DTL 85110 : B
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
SAE J 1775 : 2015
|
BLEED-AIR PNEUMATIC SYSTEMS FOR GAS TURBINE EQUIPPED MARINE AND AMPHIBIOUS CRAFT |
STANAG 7067 : 0
|
TYPE AND LOCATION OF ELECTRICAL CONNECTORS FOR HELICOPTER ROCKET LAUNCHERS |
SAE AIR 1664 : 2013
|
AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS |
SAE AS 5658 A : 2016
|
PLATFORM/SUBSYSTEM COMMON INTERFACE CONTROL DOCUMENT FORMAT |
SAE AS 6169A : 2013
|
INTERFACE STANDARD, AIRBORNE EO/IR SYSTEMS, MECHANICAL |
SAE AIR 1826 : 2016
|
ACOUSTICAL CONSIDERATIONS FOR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM DESIGN |
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
ASTM F 2318 : 2015
|
Standard Specification for Rotary Wing Basic Life Support, Advanced Life Support, and Specialized Medical Support Air Ambulances |
IEC 62508:2010
|
Guidance on human aspects of dependability |
CSA Z1004 : 2012 : R2017
|
WORKPLACE ERGONOMICS - A MANAGEMENT AND IMPLEMENTATION STANDARD |
MIL HDBK 115 : C
|
U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
VDI/VDE 3850-3 : 2015
|
DEVELOPMENT OF USABLE USER INTERFACES FOR TECHNICAL PLANTS - FEATURES, DESIGN AND APPLICATIONS OF USER INTERFACES WITH TOUCHSCREEN |
MIL T 62735 : 0
|
TRUCKS & TRUCK TRACTORS, MODIFIED, COMMERCIAL |
MIL HDBK 516 : C
|
AIRWORTHINESS CERTIFICATION CRITERIA |
MIL A 52435 : D
|
AIR CONDITIONER: BASE MOUNTED, AIR-COOLED, 208-VOLT, 3-PHASE, 50- AND 60-HERTZ AC, SINGLE- PACKAGE, 36,000 BTU/HR |
MIL HDBK 759 : C
|
HANDBOOK FOR HUMAN ENGINEERING DESIGN GUIDELINES |
UFC 4-133-01N : Change 5
|
UNIFIED FACILITIES CRITERIA - NAVY AIR TRAFFIC CONTROL FACILITIES |
MIL P 52539 : B
|
PIPELINE WELD SET TESTING |
MIL G 18473 : B
|
GENERATOR, MOTOR, AND AUXILIARY EQUIPMENT, DIRECT CURRENT, NAVAL SHIP PROPULSION |
MIL HDBK 772 : 0
|
MILITARY PACKAGING ENGINEERING |
MIL E 87235 : 0
|
EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL PRF 87819/5 : A
|
HEADSET-MICROPHONE, HEARING PROTECTIVE TYPE MODERATE AMBIENT NOISE LEVELS, UP TO 105 DB, ENLARGED EARCUP, INFLIGHT AIRCREW HEADSET-MICROPHONE, M87819/5-01 |
ISA RP60.3 : 1985
|
HUMAN ENGINEERING FOR CONTROL CENTERS |
DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
DEFSTAN 00-250(PT0)/1(2008) : 2008
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 0: HUMAN FACTORS INTEGRATION |
SAE ARP 6467 : 2014
|
HUMAN FACTORS MINIMUM REQUIREMENTS AND RECOMMENDATIONS FOR THE FLIGHT DECK DISPLAY OF DATA LINKED NOTICES TO AIRMEN (NOTAMS) |
DEFSTAN 00-25(PT8)/1(1989) : 1989
|
HUMAN FACTORS FOR DESIGNERS OF EQUIPMENT - PART 8: AUDITORY INFORMATION |
IEEE 1474.2 : 2003
|
USER INTERFACE REQUIREMENTS IN COMMUNICATIONS BASED TRAIN CONTROL (CBTC) SYSTEMS |
SAE AIR 6464 : 2013
|
EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES |
MIL DTL 83538 : D
|
CONNECTORS AND ACCESSORIES, ELECTRICAL, CIRCULAR, UMBILICAL, ENVIRONMENT RESISTANT, REMOVABLE CRIMP CONTACTS FOR MIL-STD-1760 APPLICATIONS (METRIC), GENERAL SPECIFICATION FOR |
MIL T 52991 : A
|
TABLE, SCRIBING, TRACING, DRAFTING, FLIP TOP |
MIL B 82640 : 0
|
BOOT ASSEMBLY, TOXIC, INFECTIOUS, OR VESICANT SUBSTANCES, PROTECTIVE |
MIL PRF 32379 : 0
|
SHIELD, BALLISTIC - SHIPBOARD CREW-SERVED WEAPON STATION |
MIL-PRF-32479A:2017
|
TRAILERS, LIFT - AIRCRAFT AND MISSILE ENGINE |
MIL T 0053055 : B
|
TANK, 3000 GALLON & 4600 GALLON FABRIC, COLLAPSIBLE, DRINKING WATER, SEMI-TRAILER MOUNTED |
04/30109749 DC : DRAFT JUL 2004
|
ISO 9355-4 - ERGONOMIC REQUIREMENTS FOR THE DESIGN OF DISPLAYS AND CONTROL ACTUATORS - PART 4: LOCATION AND ARRANGEMENT OF DISPLAYS AND CONTROL ACTUATORS |
DIN EN 894-4 E : 2010
|
SAFETY OF MACHINERY - ERGONOMICS REQUIREMENTS FOR THE DESIGN OF DISPLAYS AND CONTROL ACTUATORS - PART 4: LOCATION AND ARRANGEMENT OF DISPLAYS AND CONTROL ACTUATORS |
MIL C 85518 : 0
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
MIL F 85596 : 0
|
FIN, RETARDER, AIR INFLATABLE BSU-85/B |
MIL PRF 32381 : B
|
ACOUSTIC HAILING DEVICE (LIGHT) |
MIL-DTL-18110G:2018
|
VALVES, GATE TYPE, STEEL SIZES 2[1/2] INCHES TO 16 INCHES |
AAMI HE48 : 1993
|
HUMAN FACTORS ENGINEERING GUIDELINES AND PREFERRED PRACTICES FOR THE DESIGN OF MEDICAL DEVICES |
MIL T 28764 : 0
|
TEST SET, RADAR, AN/UPM-136 |
MIL S 87241 : 0
|
SIMULATOR, FLIGHT (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL D 23222 : A
|
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
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 D 81641 : 0
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
SAE AS 5116 : 2003
|
MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR GROUND ICE DETECTION SYSTEMS |
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 C 52973 : A
|
COMPRESSOR UNIT, 20 CFM, 5000 PSI, DIESEL-ENGINE-DRIVEN DIVING AIR |
MIL PRF 32090 : A
|
DELIVERY SYSTEM, AERIAL, BULK FUEL |
MIL B 467 : E
|
BREAKER, PAVING: PNEUMATIC |
MIL PRF 53051 : C
|
PUMPING ASSEMBLIES, WHEEL-MOUNTED, DIESEL ENGINE DRIVEN, BULK TRANSFER, FUEL AND POTABLE WATER PUMPING SERVICE |
MIL T 52777 : A NOTICE 1
|
TANK, STORAGE, UNDERGROUND, GLASS FIBER REINFORCED PLASTIC |
MIL M 28762 : C
|
MONITOR, PUMP NOISE, AN/WSQ-3 (METRIC) |
MIL HDBK 46855 : A
|
HUMAN ENGINEERING PROGRAM - PROCESS AND PROCEDURES |
MIL A 49204 : A NOTICE 1
|
ANTENNA GROUP OE254/GRC |
MIL G 82639 : 0
|
GLOVE ASSEMBLIES, TOXIC, INFECTIOUS, OR VESICANT SUBSTANCES, PROTECTIVE |
MIL STD 1295 : A
|
HUMAN FACTORS ENGINEERING DESIGN CRITERIA FOR HELICOPTER COCKPIT ELECTRO-OPTICAL DISPLAY SYMBOLOGY |
DOD HDBK 763 : 0
|
HUMAN ENGINEERING PROCEDURES GUIDE |
JSSG 2001 : B
|
AIR VEHICLE |
MIL C 85248 : A
|
CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
MIL PRF 49503 : C
|
GENERAL STYLE AND FORMAT, TEST PROGRAM SETS FOR AUTOMATIC TEST EQUIPMENT |
AFGS 87241 : A
|
SIMULATORS, FLIGHT |
MIL C 62747 : 0
|
CARRIER-CARGO, TRACKED, 6 TON-M548A3 |
MIL C 87987 : 0
|
CRANE, HYDRAULIC, WHEEL MOUNTED, 7.5 & 15 TON CAPACITIES |
MIL C 5584 : D
|
CONTAINER, SHIPPING AND STORAGE, METAL REUSABLE |
MIL W 52482 : D
|
WATER PURIFICATION UNIT, ELECTRIC MOTOR DRIVEN ERDLATOR TYPE CLARIFIER, DIATOMITE TYPE FILTER, VAN BODY MOUNTED 1,500 GPH |
MIL O 87226 : 0
|
OXYGEN SYSTEMS, AIRCRAFT |
MIL C 85642 : 0
|
COMMUNICATIONS CENTRAL AN/ASC-26 |
MIL B 10122 : E
|
BARGE, LIQUID CARGO: NONPROPELLED, STEEL, OFFSHORE, 4,160-BARREL, 120-FOOT, DESIGN 231C |
MIL PRF 32516 : 0
|
ELECTRONIC TEST EQUIPMENT, INTERMITTENT FAULT DETECTION AND ISOLATION FOR CHASSIS AND BACKPLANE CONDUCTIVE PATHS |
MIL M 8090 : F
|
MOBILITY, TOWED AEROSPACE GROUND EQUIPMENT, GENERAL REQUIREMENTS FOR |
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, 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 |
MIL A 29563 : 0
|
ANTENNA SYSTEM, AIMS SHIPBOARD, ELECTRONICALLY STEERED OE-120/UPX |
ANSI/ASSE Z10 : 2012(R2017)
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
MIL STD 46855 : A
|
HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT, AND FACILITIES |
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
SAE ARP 1088 : 2015
|
AIRCRAFT INDICATING SYSTEMS |
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
AAMI HE75 : 2009
|
HUMAN FACTORS ENGINEERING - DESIGN OF MEDICAL DEVICES |
ANSI A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
SAE AS 5498 : 2017
|
MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS |
SAE ARP 5119 : 2013
|
LOCATION OF AND DISPLAY SYMBOLOGY REQUIREMENTS FOR HEAD-DOWN ELECTRONIC FLIGHT DISPLAYS FOR STEEP IMC APPROACHES |
ANSI/ASSE A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
SAE ARP 5638 : 2005
|
RMS TERMS AND DEFINITIONS |
ASTM F 1166 : 2007
|
Standard Practice for Human Engineering Design for Marine Systems, Equipment, and Facilities |
NASA STD 3000 VOL 2 : 1995
|
MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 2 |
CSA Z1004 : 2012
|
WORKPLACE ERGONOMICS - A MANAGEMENT AND IMPLEMENTATION STANDARD |
MIL DTL 53078 : A
|
MOUNTING KIT: M1 TANK CLEARED LANE MARKING SYSTEM (CLAMS) |
NASA KSC STD E 0001 : 2008
|
DESIGN OF ELECTRICAL CONTROL AND MONITORING SYSTEMS, EQUIPMENT (GSE), AND PANELS, STANDARD FOR |
CSA Z1004:2012
|
WORKPLACE ERGONOMICS - A MANAGEMENT AND IMPLEMENTATION STANDARD |
NASA STD 8719.24 : 2011
|
NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
NASA KSC STD Z 0010 : 1983
|
DESIGN OF ENVIRONMENTAL CONTROL SYSTEMS, GROUND COOLANT SYSTEMS, COOLANT SERVICING SYSTEMS, AND GROUND SUPPORT EQUIPMENT, STANDARD FOR |
MIL HDBK 454 : B
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
EN 894-4:2010
|
Safety of machinery - Ergonomics requirements for the design of displays and control actuators - Part 4: Location and arrangement of displays and control actuators |
ANSI Z1979.8 : 1979
|
ANESTHESIA MACHINES FOR HUMAN USE, MINIMUM PERFORMANCE AND SAFETY REQUIREMENTS FOR COMPONENTS & SYSTEMS OF CONTINUOUS FLOW, |
SAE ARP 5770 : 2012
|
MECHANICAL CONTROL DESIGN GUIDE |
MIL PRF 32566 : 0
|
ENERGY-ATTENUATING FLOOR MATS FOR USE IN U.S. MILITARY GROUND VEHICLES |
ARINC 791P2-1 : 2014
|
MARK I AVIATION KU-BAND AND KA-BAND SATELLITE COMMUNICATION SYSTEM - PART 2: ELECTRICAL INTERFACES AND FUNCTIONAL EQUIPMENT DESCRIPTION |
GGG L 795 : E
|
LUBRICATING UNIT, POWER OPERATED, AND PUMPING UNITS, PRESSURE LUBRICATING, DRUM MOUNTING |
MIL DTL 9490 : E
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL HDBK 272 : A
|
NUCLEAR WEAPONS SYSTEMS, SAFETY DESIGN AND EVALUATION CRITERIA FOR |
MIL STD 2077 : B
|
TEST PROGRAM SETS GENERAL REQUIREMENTS FOR |
MIL I 85889 : 0
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL F 28811 : A
|
FREQUENCY STANDARD, CESIUM BEAM TUBE |
MIL STD 490 : A
|
SPECIFICATION PRACTICES |
MIL PRF 32390 : 0
|
ENGAGING DEVICE, AIRCRAFT ARRESTING SYSTEM - USAF PENDANT CABLE RETRACTION SYSTEMS (PCRS) |
MIL W 52874 : B
|
WATER QUALITY ANALYSIS SET, ENGINEER |
MIL B 23401 : E
|
BURNER, CARBON MONOXIDE AND HYDROGEN, CATALYTIC TYPE (MARK 4 E) NAVAL SUBMARINE USE |
MIL A 49263 : 0
|
ANTENNA AS-2731()/GRC |
API HUMAN FACTORS TASK FORCE : 2006
|
HUMAN FACTORS IN NEW FACILITY DESIGN TOOL |
SAE ARP 5589 : 2005
|
HUMAN ENGINEERING CONSIDERATIONS FOR DESIGN AND IMPLEMENTATION OF PERSPECTIVE FLIGHT GUIDANCE DISPLAYS |
MIL PRF 32144 : B
|
CLOCK, AIRCRAFT, ELECTRONIC |
JSSG 2009 : A
|
AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE) |
SAE J 2671 : 2004
|
REDUCED EFFORT BRAKES AND REDUCED EFFORT VACUUM POWERED BRAKE BACKUP SYSTEMS |
MIL A 55379 : A
|
ANTENNA GROUP, P/O DIRECTION FINDER SET AN/TRQ-30()(V) |
MIL L 52325 : D
|
LAUNCHER, TRANSPORTER, BRIDGE M48A5 OR M60A1 TANK CHASSIS |
MIL HDBK 761 : A
|
HUMAN ENGINEERING GUIDELINES FOR MANAGEMENT INFORMATION SYSTEMS - METRIC |
NASA KSC STD Z 0009 : 1994
|
DESIGN OF CRYOGENIC GROUND SUPPORT EQUIPMENT, STANDARD FOR |
DEFSTAN 23-6/4(2005) : 2005
|
TECHNOLOGY GUIDANCE FOR MILITARY LOGISTICS VEHICLES |
DEFSTAN 00-25(PT13)/1(1996) : 1996
|
HUMAN FACTORS FOR DESIGNERS OF EQUIPMENT - PART 13: HUMAN COMPUTER INTERACTION |
MIL C 28741 : A
|
CONTROL MONITOR, C-843O/UPX |
DEFSTAN 00-25(PT3)/2(1997) : 1997
|
HUMAN FACTORS FOR DESIGNERS OF EQUIPMENT - PART 3: BODY STRENGTH AND STAMINA |
A A 59918 : B
|
SELF PROPELLED CONCRETE SAW (SPCS) |
BS EN 894-4:2010
|
Safety of machinery. Ergonomics requirements for design of displays and control actuators Location and arrangement of displays and control actuators |
MIL N 49098 : A
|
NAVIGATIONAL SET, DOPPLER AN/ASN-128()(XE-2) |
MIL A 29423 : 0
|
ANTENNA: AS-()/GRC; MICROWAVE |
MIL STD 1333 : B
|
AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT |
MIL M 24365 : A NOTICE 1
|
MAINTENANCE ENGINEERING ANALYSIS, ESTABLISHMENT OF, AND PROCEDURES AND FORMATS FOR ASSOCIATED DOCUMENTATION, GENERAL SPECIFICATION FOR |
DEFSTAN 00-25(PT3)/1(1984) : 1984 CORRIGENDUM 1
|
HUMAN FACTORS FOR DESIGNERS OF EQUIPMENT - BODY STRENGTH AND STAMINA |
DOD HDBK 791 : 0
|
MAINTAINABILITY DESIGN TECHNIQUES |
MIL STD 415 : D
|
TEST PROVISIONS FOR ELECTRONIC SYSTEMS AND ASSOCIATED EQUIPMENT, DESIGN CRITERIA FOR |
MIL R 49315 : 0
|
RADIOSONDE SET ML-659(V), FAMILY OF (NO S/S DOCUMENT) |
MIL S 81771 : A
|
SEAT SYSTEM; AIRCREW, CRASH RESISTANT; GENERAL SPECIFICATION FOR |
A A 59983 : 0
|
TRANSIT LEVEL, AUTO |
MIL STD 3028 : 0
|
JOINT MODULAR INTERMODAL CONTAINER |
ADS-63-SP : 2001
|
AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS |
MIL PRF 52955 : D
|
IMPROVED POSITION AND AZIMUTH DETERMINING SYSTEM (IPADS) |
EG 202 116 : 1.2.2
|
HUMAN FACTORS (HF); GUIDELINES FOR ICT PRODUCTS AND SERVICES; "DESIGN FOR ALL" |
14/30298035 DC : 0
|
BS EN 61069-6 ED 2.0 - INDUSTRIAL-PROCESS MEASUREMENT AND CONTROL - EVALUATION OF SYSTEM PROPERTIES FOR THE PURPOSE OF SYSTEM ASSESSMENT - PART 6: ASSESSMENT OF SYSTEM OPERABILITY |
MIL P 83126 : A
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL S 52881 : B
|
SERVICING UNITS, COMPRESSED GAS, MOBILE |
MIL I 8671 : D
|
INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
MIL I 52701 : B
|
INDICATOR SOLUTION, PH DETERMINATION (RANGE 3.0 TO 11.0) |
MIL HDBK 87213 : A
|
ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS |
MIL H 46855 : B
|
HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT & FACILITIES |
MIL V 12125 : F
|
VALVE, GATE, QUICK-OPENING, CLASS 125, CAST IRON, WITH POSITION LOCK |
MIL STD 2067 : 0
|
AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR |
MIL HDBK 338 : B
|
ELECTRONIC RELIABILITY DESIGN HANDBOOK |
JSSG 2010 12 : 0
|
CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK |
MIL E 38453 : A
|
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 STD 1421 : A
|
BREATHING APPARATUS (SELF CONTAINED) |
MIL A 28772 : C
|
ANTENNA, HF, FIXED ROTATABLE LOG PERIODIC |
MIL S 52156 : D
|
SURVEYING INSTRUMENT, DISTANCE MEASURING, ELECTRONIC MICROWAVE |
MIL T 53029 : C
|
TANKS, FABRIC, COLLAPSIBLE, 10,000 20,000 AND 50,000 GALLON, DRINKING WATER |
MIL A 0083216 : C
|
AIR CONDITIONER, HORIZONTAL, 54,000 BTUH, 208/230 V |
MIL F 46851 : C
|
FAN, GUIDED MISSILE, GROUND SUPPORT EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL C 11218 : E
|
CONVEYORS, ROLLER AND WHEEL, GRAVITY AND CONVEYER SUPPORTS |
MIL C 52988 : A
|
CHAMBER, DECOMPRESSION, DIVERS, 100 PSI |
ANSI/ASSE A10.17 : 2006
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
MIL-DTL-17840D:2018
|
PUMPS, CENTRIFUGAL, CLOSE-COUPLED, NAVY STANDARD (FOR SURFACE SHIP APPLICATION) |
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 |
MIL DTL 45150 : N
|
CHASSIS, TRAILER, 2-WHEEL CART TYPE 2-1/2 TON |
MIL T 24664 : 0
|
TEST SET, RADAR, AN/UPM-() |
MIL-C-81774A:1973
|
CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
MIL STD 188/200 : 0
|
SYSTEM DESIGN AND ENGINEERING STANDARDS FOR TACTICAL COMMUNICATIONS |
MIL STD 1473 : B
|
STANDARD GENERAL REQUIREMENTS FOR COLOR AND MARKING OF ARMY MATERIAL |
MIL E 18927 : E
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
MIL DTL 2036 : E
|
ENCLOSURES FOR ELECTRIC AND ELECTRONIC EQUIPMENT, NAVAL SHIPBOARD |
SAE ARP 5764 : 2013(R2018)
|
AEROSPACE ACTIVE INCEPTOR SYSTEMS FOR AIRCRAFT FLIGHT AND ENGINE CONTROLS |
SAE AIR 4728 : 2013
|
REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
SAE AIR5691A : 2017
|
GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS |
SAE ARP 85 : 2012
|
AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES |
SAE ARP 1247 : 2018
|
AIRCRAFT GROUND SUPPORT EQUIPMENT - GENERAL REQUIREMENTS |
NFPA 1917 : 2016
|
AUTOMOTIVE AMBULANCES |
ANSI A10.17 : 2006 : R2011
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
SAE ARP 1967 : 2014
|
CONTAINERS, SHIPPING AND STORAGE, REUSABLE |
I.S. EN 894-4:2010
|
SAFETY OF MACHINERY - ERGONOMICS REQUIREMENTS FOR THE DESIGN OF DISPLAYS AND CONTROL ACTUATORS - PART 4: LOCATION AND ARRANGEMENT OF DISPLAYS AND CONTROL ACTUATORS |
ANSI/ASSE Z10 : 2012(R2017)
|
OCCUPATIONAL HEALTH AND SAFETY MANAGEMENT SYSTEMS |
ANSI/ASSE A10.17 : 2006 : R2011
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
SAE AS 8090 : 2016
|
MOBILITY, TOWED AEROSPACE GROUND EQUIPMENT, GENERAL REQUIREMENTS FOR |
ASTM F 2319 : 2004
|
Standard Specification for Fixed Wing Basic Life Support, Advanced Life Support, and Specialized Medical Support Air Ambulances (Withdrawn 2013) |
IEEE 45.3 : 2015
|
SHIPBOARD ELECTRICAL INSTALLATIONS - SYSTEMS ENGINEERING |
MIL PRF 83818 : C : 2015
|
TRUCK, FORKLIFT, 4,000 AND 6,200 POUND CAPACITY, FRONT/SIDE LOADING, INTERNAL COMBUSTION ENGINE |
MIL-STD-1474E:2015
|
NOISE LIMITS |
EN ISO 9241-13:1998
|
Ergonomic requirements for office work with visual display terminals (VDTs) - Part 13: User guidance (ISO 9241-13:1998) |
ASTM E 2517 : 2013 : REDLINE
|
Standard Specification for Cargo Bed Cover, Type III (M35A2, 2 1/2 Ton Cargo Truck/M1078, 2 1/2 Ton Lightweight Medium Tactical Vehicle (LMTV)/ M1082, 2 1/2 Ton LMTV Trailer) |
MIL PRF 29250 : C
|
LOADING JACK SYSTEM, ISO CONTAINER |
MIL E 53126 : 0
|
ELECTRICAL DISTRIBUTION 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 |
DOD STD 1788 : LATEST
|
AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
MIL E 29581 : 0
|
EARCUP, UNIT ACTIVE NOISE REDUCTION SYSTEM |
MIL S 81340 : B
|
SIGNAL, UNDERWATER SOUND (SUS) MARK 84 AND MODS |
MIL STD 648 : E
|
SPECIALIZED SHIPPING CONTAINERS |
MIL T 28820 : 0
|
TEST SET, RS 3389, OMEGA RECEIVING SET |
GGG S 58 : F
|
SAW, RADIAL OVERARM, WOODWORKING |
MIL T 49435 : 0
|
TEST SET,LASER DETECTING AN/UPM-148() |
MIL T 49136 : 0
|
TEST SET, COUNTERMEASURES SET AN/ALM-178(( |
MIL STD 912 : 0
|
PHYSICAL EAR NOISE ATTENUATION TESTING |
MIL S 87238 : 0
|
SURVIVAL AND FLOTATION SYSTEM, AIRBORNE |
MIL STD 1558 : 0
|
SIX DEGREE OF FREEDOM MOTION SYSTEM REQUIREMENTS FOR AIRCREWMEMBER TRAINING SIMULATORS |
MIL R 29583 : 0
|
RADIO SET |
MIL C 23952 : C
|
CONTROL EQUIPMENT AUTOMATIC DEGAUSSING (AUTO DEG), TYPE SSM |
MIL C 24040 : B
|
COMPUTER INDICATOR (SCALER) RADIAC, CP 792()/UD |
MIL STD 633 : G
|
STANDARD FAMILY OF MOBILE ELECTRIC POWER GENERATING SOURCES - GENERAL DESCRIPTION INFORMATION AND CHARACTERISTIC DATA |
MIL G 49140 : 0
|
GENERATOR, DIRECT CURRENT G67((/G |
MIL S 0053046 : A
|
SURVEYING EQUIPMENT, ELECTRONIC DISTANCE MEASURING, MEDIUM RANGE, (SEDME MR) |
MIL A 85672 : 0
|
AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
MIL PRF 32367 : 0
|
BIPOD, SQUAD DESIGNATED MARKSMAN (SDM) |
MIL B 29511 : 0
|
BUOY INTERFACE UNIT (BIU), J-3958/BRT-6 |
MIL T 49388 : A
|
TRAY ASSEMBLY, BATTERY CHARGING MX-10154 |
DEFSTAN 00-25(PT19)/1(2004) : 2004
|
HUMAN FACTORS FOR DESIGNERS OF SYSTEMS - PART 19: HUMAN ENGINEERING DOMAIN |
MIL STD 1180 : B
|
SAFETY STANDARDS FOR MILITARY GROUND VEHICLES |
MIL M 49275 : 0
|
MASTS, QUICK ERECT, EXPANDABLE AB-1309(V)/TRC |
MIL T 52849 : C
|
TEST KIT, PETROLEUM; AVIATION FUEL CONTAMINATION (PORTABLE) |
MIL A 29505 : 0
|
ANTENNA GROUP, TACAN, OE-273(V)/URN |
MIL S 53120 : 0
|
SUPPORT SYSTEM, SPECIAL DIVER'S AIR (SDASS) |
MIL PRF 87819/6 : A
|
HEADSET-MICROPHONE, DICHOTIC, HEARING PROTECTIVE TYPE, MODERATE AMBIENT NOISE LEVELS, UP TO 105 DB, ENLARGED EARCUP, INFLIGHT AIRCREW HEADSET-MICROPHONE, M87819/6-01 |
MIL PRF 32217 : A
|
SCALE PREVENTION IN SEWAGE COLLECTION, HOLDING AND TRANSFER (CHT) AND VACUUM CHT (VCHT) PIPING SYSTEMS FOR USE ON NAVAL SURFACE SHIPS |
MIL D 42048 : 0
|
DEPLOYABLE MEDICAL SYSTEMS, GENERAL REQUIREMENTS FOR |
DOD HDBK 343 : 0
|
DESIGN, CONSTRUCTION, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT |
MIL PRF 32548 : 0
|
OCCUPANT SEAT BELT RESTRAINTS FOR USE IN U.S. MILITARY GROUND VEHICLES |
MIL D 8708 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL DTL 62073 : H
|
TRAILER, FLATBED: 4-, 5-, AND 7.5-TON, 4-WHEEL (TANDEM) CART TYPE; TRAILER, BOLSTER: 4-TON, 4-WHEEL (TANDEM) |
MIL A 52940 : C
|
AEROSOL GENERATOR, NON-THERMAL, INSECTICIDE, ULTRA LOW VOLUME |
MIL S 24186 : B
|
SAMPLER, AIR PARTICLE, HD-732/UD |
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 P 49115 : A
|
PLATOON EARLY WARNING SYSTEM AN/TRS-2() |
MIL B 62542 : A
|
BALL SCREW LINEAR ACTUATOR |
MIL T 53068 : 0
|
TANKS, LIGHTWEIGHT, COLLAPSIBLE, PILLOW, 160 GALLON (NOMINAL), DRINKING WATER |
MIL S 53046 : 0
|
SURVEYING EQUIPMENT, ELECTRONIC DISTANCE MEASURING, MEDIUM RANGE, (SEDME-MR) |
SAE AIR 4362 : 2014
|
NBC PROTECTION CONSIDERATIONS FOR ECS DESIGN |
MIL C 87970 : 0
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
MIL H 53076 : 1987
|
HEMTT TANKER AVIATION REFUELING SYSTEM (HTARS) |
SAE ARP 4898 : 2005
|
STANDS, SHIPPING AND STORAGE, AIRCRAFT ENGINES, REUSABLE |
ANSI A10.17 : 2006 : R2011
|
SAFE OPERATING PRACTICES FOR HOT MIX ASPHALT (HMA) CONSTRUCTION |
MIL STD 411 : F
|
AIRCREW STATION ALERTING SYSTEMS |
MIL L 52413 : B
|
LIFE PRESERVER, YOKE, ORAL INFLATION, TRAPPED AIR TYPE, DESIGN 9008 |
MIL P 82634 : 0
|
PROTECTIVE CLOTHING SET, CHEMICAL AGENTS, MARK 1 MOD O |
MIL P 28739 : 0
|
PEDESTAL GROUP, ANTENNA, FOR IFF ANTENNAS AN/UPA-57 |
MIL I 27619 : G
|
INDICATORS, ATTITUDE DIRECTOR |
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 A 55368 : 0
|
AIRBORNE DATA ANNOTATION SYSTEM AN/AYA-10() |
MIL C 85392 : 0
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-7D, GENERAL SPECIFICATION FOR |
MIL G 21480 : A
|
GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
MIL T 23752 : E
|
TRITIUM AIR MONITOR, PORTABLE OR FIXED |
MIL T 52965 : 0
|
TOPOGRAPHIC SUPPORT SYSTEM (TSS), DIRECT SUPPORT SECTION, TRUCK MOUNTED |
MIL C 11071 : D
|
CLEANING MACHINE, FUEL CAN, DRUM |
MIL PRF 85726 : B
|
ENCLOSURE, STANDARD AVIONICS, FORCED AIR-COOLED, SPECIFICATION FOR |
NASA STD 5005(INT) : 2007
|
THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
ADS-65-HDBK : 2004
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
MIL A 53099 : 0
|
ARCTIC FORWARD AREA REFUELLING EQUIPMENT (AFARE) |
MIL V 85830 : 0
|
VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
MIL A 29521 : 0
|
ANTENNA GROUP, AN/BRA-34(V), AN/BRA-34A(V), AN/BRA-34B(V) |
MIL P 24764 : 0
|
POWER SUPPLIES, SHIPBOARD, ELECTRONIC, GENERAL SPECIFICATION FOR |
MIL T 49117 : 0
|
TEST SET, RECEIVER TS-3565( )/TRS-2 |
MIL PRF 32470 : 0
|
TRUCK, FORKLIFT, 10,000 LB CAPACITY, VARIABLE REACH, ROUGH TERRAIN |
MIL C 85283 : B
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-9 |
MIL DTL 5003 : E
|
FLOODLIGHT SET, ELECTRIC, TRIPOD-MOUNTED, FOUR 150-WATT FLOODLIGHTS |
MIL F 18953 : B
|
FAN, VANEAXIAL AND TUBEAXIAL, FIXED AND PORTABLE, VENTILATION, NAVAL SHIPBOARD |
MIL DTL 53077 : A
|
MOUNTING KIT: M1, ROLLER, MINE CLEARING TRACK-WIDTH, TANK MOUNTED |
MIL C 62748 : 0
|
CARRIER, 120 MM MORTAR: M1064A3 |
MIL P 52307 : B
|
PLOTTER, RECTANGULAR COORDINATES (COORDINATOGRAPH) |
MIL C 85373 : A
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW 12A |
MIL T 49305 : 0
|
TEST SET, COUNTERMEASURE SET TS-3609 ()/ALQ-156(V) |
ASTM E 2518 : 2011
|
Standard Specification for Cargo Bed Cover, Type IV (M923, 5 Ton Cargo Truck/M1083, 5 Ton Medium Tactical Vehicle (MTV)/ M1082, 5 Ton MTV Trailer) |
MIL W 5013 : L
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
SAE ARP 6023 : 2013
|
HUMAN ENGINEERING CONSIDERATIONS FOR IMPLEMENTING ENHANCED SYNTHETIC VISION SYSTEMS IN VERTICAL FLIGHT CAPABLE PLATFORMS |
MIL T 81821 : 0
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
BS 7404-4:1991
|
TELECONTROL EQUIPMENT AND SYSTEMS - SPECIFICATION FOR PERFORMANCE |
MIL A 85434 : A
|
AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
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 |
MIL P 82637 : 0
|
PROTECTIVE CLOTHING SET, TOXICOLOGICAL AGENTS AND PROPELLANTS |
SAE ARP 6461 : 2013
|
GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
DEFSTAN 00-25(PT10)/1(1992) : 1992
|
HUMAN FACTORS FOR DESIGNERS OF EQUIPMENT - PART 10: CONTROLS |
IEEE 1082-1997
|
INCORPORATING HUMAN RELIABILITY ANALYSIS INTO PROBABILISTIC RISK ASSESSMENTS FOR NUCLEAR POWER GENERATING STATIONS AND OTHER NUCLEAR FACILITIES |
MIL PRF 32070 : A
|
TEST PROGRAM SETS |
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 |
AEDP-6 : 2014
|
NATO ADVANCED DATA STORAGE INTERFACE REQUIREMENTS AND IMPLEMENTATION GUIDE |
SAE J 2672 : 2004
|
Reduced Effort Power Steering and Power Steering Backup Systems
|
SAE ARP 712 : 2017
|
GALLEY LIGHTING |
AAS3P-10 : 2011
|
SAFETY AND SUITABILITY FOR SERVICE ASSESSMENT TESTING FOR SHOULDER LAUNCHED MUNITIONS |
SAE ARP 292 : 2014
|
ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS |
ISO 9241-13:1998
|
Ergonomic requirements for office work with visual display terminals (VDTs) Part 13: User guidance |