MIL-STD-882 Revision E:2012
Current
Current
The latest, up-to-date edition.
System Safety
Available format(s)
PDF
Language(s)
English
Published date
05-11-2012
Publisher
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
TASK SECTION 100 - MANAGEMENT
TASK SECTION 200 - ANALYSIS
TASK SECTION 300 - EVALUATION
TASK SECTION 400 - VERIFICATION
APPENDIX A - GUIDANCE FOR THE SYSTEM
SAFETY EFFORT
APPENDIX B - SOFTWARE SYSTEM SAFETY
ENGINEERING AND ANALYSIS
Classifies the Department of Defense (DoD) Systems Engineering (SE) approach to eliminating hazards, where possible, and minimizing risks where those hazards cannot be eliminated. Specifies hazards as they apply to systems/products/equipment/infrastructure (including both hardware and software) throughout design, development, test, production, use, and disposal.
This system safety standard practice identifies the Department of Defense (DoD) Systems Engineering (SE) approach to eliminating hazards, where possible, and minimizing risks where those hazards cannot be eliminated. Applicable DoD Instruction (DoDI) 5000 series defines the risk acceptance authorities. This Standard covers hazards as they apply to systems / products / equipment / infrastructure (including both hardware and software) throughout design, development, test, production, use, and disposal. When this Standard is required in a solicitation or contract but no specific task is identified, only Sections 3 and 4 are mandatory. The definitions in 3.2 and all of Section 4 delineate the minimum mandatory definitions and requirements for an acceptable system safety effort for any DoD system.
| DevelopmentNote |
NEW CHILD NOT 1 2022 IS NOW ADDED
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| DocumentType |
Standard
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| Pages |
105
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| ProductNote |
NEW CHILD NOT 1 2022 IS NOW ADDED
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| Supersedes |
| 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 Base Document:1988 | 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 Base Document:1979 | SHELTER, S-80A AND S-82A |
| MIL-T-5842 Revision B:1985 | TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
| MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-DTL-53135 Base Document:1996 | 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 |
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| MIL-STD-1629 Revision A:1980 | 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 |
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| GEIA TA HB 0009 : 2013 | RELIABILITY PROGRAM HANDBOOK |
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| JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
| BS ISO/IEC 33071:2016 | Information technology. Process assessment. An integrated process capability assessment model for Enterprise processes |
| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| MIL-PRF-85676 Revision A:2006 | LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
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| IEEE 1887-2017 | IEEE Guide for Wayside Energy Storage Systems for DC Traction Applications |
| MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
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| MIL-P-6457 Revision E:1974 | POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
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| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| MIL-A-52767 Revision D:1989 | AIR CONDITIONER: VERTICAL AND HORIZONTAL, COMPACT |
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| MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
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| 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 |
| SAE JA7496:2022 | Cyber-Physical Systems Security Engineering Plan (CPSSEP) |
| MIL-DTL-53133 Revision C:2002 | GENERATOR SETS, SKID MOUNTED, TACTICAL, QUIET, DIESEL ENGINE DRIVEN, ALTERNATING CURRENT 5 THROUGH 60 KILOWATTS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-83477 Revision A:1976 | AIR CONDITIONER, A/M32C-18 TRAILER MOUNTED, DIESEL ENGINE DRIVEN |
| MIL-DTL-53126 Revision A:2012 | POWER DISTRIBUTION, ILLUMINATION SYSTEMS, ELECTRICAL, GENERAL SPECIFICATION FOR |
| UFC 4-133-01 : CHANGE 1 | UNIFIED FACILITIES CRITERIA - AIR TRAFFIC CONTROL AND AIR OPERATIONS FACILITIES |
| UFC 4-141-04 : Change 1 | UNIFIED FACILITIES CRITERIA - EMERGENCY OPERATIONS CENTER PLANNING AND DESIGN |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| SAE AS 6228 : 2014 | SAFETY REQUIREMENTS FOR PROCUREMENT, MAINTENANCE AND USE OF HAND-HELD POWERED TOOLS |
| MIL-PRF-32335 Base Document:2010 | TRICON REFRIGERATED CONTAINER SYSTEM (TRCS) |
| MIL-DTL-32496 Base Document:2014 | GENERATOR SETS, SKID MOUNTED, TRAILER MOUNTED ADVANCED MEDIUM-SIZED MOBILE POWER SOURCES, TACTICAL DIESEL FUEL DRIVEN, ALTERNATING CURRENT 5 THROUGH 60 KILOWATTS, GENERAL SPECIFICATION FOR |
| 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 Base Document:1983 | CONCENTRATOR, OXYGEN, GGU-7/A |
| ASTM F 3201 : 2016 | Standard Practice for Ensuring Dependability of Software Used in Unmanned Aircraft Systems (UAS) |
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| MIL-PRF-53090 Revision B:2016 | BLADE, MINE CLEARING |
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| MIL-H-4607 Revision E:1987 | HEATER, ENGINE AND SHELTER, GROUND |
| MIL-E-4158 Revision E:1973 | ELECTRONIC EQUIPMENT, GROUND GENERAL REQUIREMENTS FOR |
| MIL-B-53107 Base Document:1990 | BRIDGE, LIGHT ASSAULT 23 METER SPAN |
| AFGS-87219 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
| SAE ARP 5764 : 2013(R2018) | AEROSPACE ACTIVE INCEPTOR SYSTEMS FOR AIRCRAFT FLIGHT AND ENGINE CONTROLS |
| MIL-P-85710 Base Document:1986 | 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 |
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| MIL-STD-973 Base Document:1992 | CONFIGURATION MANAGEMENT |
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| MIL-F-85596 Base Document:1983 | FIN, RETARDER, AIR INFLATABLE BSU-85/B |
| MIL-P-87210 Base Document:1984 | PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
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| MIL-P-85723 Base Document:1986 | PROJECTILE, 20 MILLIMETER, SEMI-ARMOR PIERCING, HIGH EXPLOSIVE INCENDIARY PGU-28/B |
| MIL-STD-1388-2 Revision B:1991 | DOD REQUIREMENTS FOR A LOGISTIC SUPPORT ANALYSIS RECORD |
| MIL-R-87245 Base Document:1986 | 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 Revision G:1983 | |
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| MIL-STD-1543 Revision B:1988 | RELIABILITY PROGRAM REQUIREMENTS FOR SPACE AND LAUNCH VEHICLES |
| MIL-P-24568 Revision A:1986 | POWER SUPPLY, D.C., FOR OXYGEN GENERATOR |
| MIL-T-27200 Revision C:1975 | TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-I-8700 Revision A:1970 | 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 |
| 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 | IEEE Standard Criteria for Programmable Digital Devices 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 Base Document:2013 | DESIGN CRITERIA STANDARD - USAF AIRCRAFT ARRESTING SYSTEMS |
| MIL-PRF-32390 Base Document:2011 | 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 Revision D:1988 | 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 Base Document:1988 | MAINTAINABILITY DESIGN TECHNIQUES |
| MIL-DTL-32392 Revision A:2013 | 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 Base Document:1979 | GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
| MIL-P-83126 Revision A:1980 | 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 Base Document:2002 | WEAPON SYSTEM INTEGRITY GUIDE (WSIG) |
| MIL-S-23069 Revision A:1983 | SAFETY REQUIREMENTS, MINIMUM, FOR AIR LAUNCHED GUIDED MISSILES |
| RG.AERO 00040 : 1999 | GENERAL RECOMMENDATION FOR THE PROGRAMME MANAGEMENT SPECIFICATION |
| MIL-STD-2067 Base Document:1978 | AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR |
| JSSG-2010-12 Base Document:1998 | 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 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-HDBK-514 Base Document:2003 | OPERATIONAL SAFETY, SUITABILITY, & EFFECTIVENESS FOR THE AERONAUTICAL ENTERPRISE |
| MIL-A-0083216 Revision C:1976 | 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 Revision F:1992 | BRIDGE, ARMOURED VEHICLE LAUNCHED, SCISSORING TYPE, CLASS 60, ALUMINUM, 60 FOOT SPAN |
| MIL-P-85573 Base Document:1983 | 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 Revision B:1993 | GUNFIRE SIMULATOR: 12725085-1 |
| SAE ARP 5150 : 2013 | SAFETY ASSESSMENT OF TRANSPORT AIRPLANES IN COMMERCIAL SERVICE |
| MIL-E-18927 Revision E:1983 | 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 | 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 Revision A:1991 | 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 Revision A:1987 | WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| MIL-STD-1367 Revision A:1989 | 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 Base Document:1985 | 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 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| MIL-STD-633 Revision G:2013 | 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 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-HDBK-525 Base Document:2013 | ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) INTEGRITY PROGRAM |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-D-18300 Revision H:1993 | DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
| MIL-D-8708 Revision C:1991 | 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 Base Document:1994 | 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 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
| MIL-C-87970 Base Document:1982 | 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 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL-G-25591 Revision E:1981 | GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
| EIA 836 CD : B2010(R2015) | CONFIGURATION MANAGEMENT DATA EXCHANGE AND INTEROPERABILITY |
| MIL-P-24587 Base Document:1979 | POWER SUPPLY, UNINTERRUPTIBLE, SOLID STATE (NAVAL SHIPBOARD) |
| MIL-T-85549 Base Document:1982 | Test Program Set (TPS) - Operational Test Program Sets (OTPS) For F/A-18 Units Under Test (UUT), General Specification For |
| MIL-M-4820 Revision E:1979 | MOTOR GENERATOR, SKID MOUNTED TYPE MD 4 |
| MIL-STD-1606 Revision A:1983 | 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 Base Document:2013 | TRUCK, FORKLIFT, 10,000 LB CAPACITY, VARIABLE REACH, ROUGH TERRAIN |
| MIL-P-85767 Base Document:1986 | 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 Base Document:1969 | TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
| MIL-A-85434 Revision A:1983 | 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 Revision A:1981 | 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 |
| ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| AOP 52 : 2016 | GUIDANCE ON SOFTWARE SAFETY DESIGN AND ASSESSMENT OF MUNITION-RELATED COMPUTING SYSTEMS |
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