MIL-HDBK-831 Revision A:2013
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Current
The latest, up-to-date edition.
PREPARATION OF TEST REPORTS
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
Outlines the format and content criteria to be used in the preparation of test reports covering tests on systems, subsystems, equipment, components, and parts.
| Committee |
FSC QCIC
|
| DevelopmentNote |
Supersedes MIL STD 831. (02/2004) A NOTICE 1 - Notice of Validation. (05/2018)
|
| DocumentType |
Standard
|
| Pages |
19
|
| ProductNote |
NEW CHILD NOT 1 2018 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| MIL-PRF-32239 Revision A:2014 | COATING SYSTEM, ADVANCED PERFORMANCE, FOR AEROSPACE APPLICATIONS |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-DTL-83425 Revision A:2006 | EARCUP, SOUND PROTECTIVE MX-8376/AR |
| SAE AS 5960 : 2013 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC BRAID REINFORCED, 5080 PSI (35000 KPA), 400 DEGREES F (204 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
| MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| SAE AS 6116 : 2016 | ALUMINUM FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPERABLE, FLUID SYSTEM, UP TO 1500 PSI (10340 KPA) MAXIMUM, SPECIFICATION FOR |
| SAE AS 4751 : 2005 | COUPLING ASSEMBLY, V-BAND SHEET METAL WIDE FLANGE, PNEUMATIC TUBE |
| SAE AS 1650 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING, PROCUREMENT SPECIFICATION |
| SAE AS 1946 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |
| MIL-DTL-27723 Revision F:2013 | Probe, Total Temperature, Deiceable |
| 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 AS 1710 : 2014 | COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY, THREADED TYPE WITH FERRULES |
| MIL-DTL-25427 Revision B:2009 | COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR |
| MIL-DTL-25539 Revision C:2009 | CANDLES, ILLUMINATING, SURVIVAL, HIGH MELTING POINT |
| MIL-DTL-49198 Revision B:2014 | HEADSET-MICROPHONE KIT, MK-1564( )/AIC |
| MIL-PRF-1-1718 Revision A:1998 | ELECTRON TUBE, GAS SWITCHING TYPE 8922 |
| SAE AS 5951 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 5080 PSI (35,000 KPA), 275 DEGREES F (135 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
| SAE ARP 5812 : 2017 | ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
| MIL-DTL-25469 Revision J:2014 | Valves, Filler, Liquid Oxygen, Aircraft Type |
| SAE AS 620 : 2012 | HOSE ASSEMBLIES, CONVOLUTED POLYTETRAFLUOROETHYLENE METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT |
| SAE AS 5958 : 2017 | FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR |
| SAE AIR 5992 : 2015 | DESCRIPTIONS OF SYSTEMS INTEGRATION TEST RIGS (IRON BIRDS) FOR AEROSPACE APPLICATIONS |
| SAE AS 614 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 4000 PSI, 400 DEGREES F, HEAVY DUTY, HYDRAULIC AND PNEUMATIC |
| MIL-DTL-7899 Revision D:2014 | Valve, Check, Aircraft Fuel System |
| MIL-DTL-25971 Revision D:2015 | LIGHT, AIRPORT TRAFFIC CONTROL, SDU-4/U |
| MIL-PRF-1-1609 Revision C:2004 | ELECTRON TUBE, VOLTAGE REGULATOR TYPE 8515 |
| MIL-DTL-25308 Revision C:2010 | GAGE, PRESSURE, DIAL INDICATING, HYDRAULIC, TYPE ME-1 |
| MIL-DTL-7990 Revision D:2012 | Transmitter, Temperature, Electrical Resistance, -70 Degrees to +300 Degrees C |
| MIL-DTL-27443 Revision F:2003 | PALLETS, CARGO, AIRCRAFT, TYPE HCU-6/E AND HCU-12/E |
| SAE AS 4623 : 2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
| SAE ARP 4058 : 2017 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| SAE AS 4073 : 2013(R2018) | AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
| SAE AS 8914 : 2016 | BEARING, ROLLER, SELF-ALIGNING, AIRFRAME, ANTIFRICTION |
| MIL-DTL-6645 Revision J:2001 | Parachutes, Personnel, General Specification for |
| MIL-DTL-9320 Revision E:2010 | Signal, Warning, Audible, for Headset, Type MA-1 |
| MIL-DTL-38394 Revision E:2009 | Transmitter, Pressure TRU-81/A, Oil, 0-500 PSI |
| SAE AS 5830 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF-BONDING, PROCUREMENT SPECIFICATION |
| MIL-PRF-1-1705 Revision C:2004 | ELECTRON TUBE, MAGNETRON TYPE 8896 |
| MIL-PRF-32144 Revision B:2012 | CLOCK, AIRCRAFT, ELECTRONIC |
| MIL-DTL-5790 Revision H:2008 | Transmitter, Pressure, Oil, Synchro, 0-200 PSI 320-Degree Movement, 26V, Single Phase, 400 Cycles |
| MIL-PRF-87260 Revision B:2006 | Foam Material, Explosion Suppression, Inherently Electrostatically Conductive, for Aircraft Fuel Tanks |
| SAE AS 7365 : 2013 | Duct Assembly, Ground, Conditioned Air, Metallic Reinforced, Low Pressure, 350 °F |
| MIL-DTL-5516 Revision D:2008 | Packing, Preformed, Petroleum Hydraulic Fluid Resistant, 160 Degrees F (71 Degrees C) |
| MIL-DTL-38449 Revision D:2010 | SIGNAL AND SIGNAL/INTERCOMMUNICATION AMPLIFIERS, UNIVERSAL, AERIAL REFUELING |
| SAE AS 5620 : 2017 | TITANIUM HYDRAULIC TUBING, TI-3AL-2.5V COLD WORKED AND STRESS RELIEVED, UP TO 35000 KPA (5080 PSI), REQUIREMENTS FOR QUALIFICATION TESTING AND CONTROL |
| SAE AS 604 : 2012 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC |
| SAE AS 1339 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC |
| SAE AS 1227 : 2013 | HOSE ASSEMBLY, CONVOLUTED POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, LOW PRESSURE, UP TO 400 DEGREES F, AIRCRAFT |
| MIL-DTL-9398 Revision D:2007 | GENERATOR, TACHOMETER, TWO-POLE, HIGH TEMPERATURE, AIRCRAFT |
| MIL-DTL-25867 Revision D:2006 | GAGE, PRESSURE, DIAL INDICATING, PNEUMATIC |
| SAE AS 4459 : 2013 | FITTINGS, TUBE, FLUID SYSTEM 3000 PSIG (21000 KPA) RATED PRESSURE, EXTERNALLY SWAGED, SPECIFICATION FOR |
| MIL-DTL-8954 Revision C:2006 | BASE AND ACCESSORIES, AIRPORT MARKER LIGHTS, GENERAL SPECIFICATION FOR |
| MIL-DTL-5521 Revision C:2007 | Washer, Aircraft Hydraulic Packing Back-Up |
| MIL-DTL-3971 Revision G:2016 | METERS, TIME TOTALIZING, NON-HERMETICALLY SEALED, ELECTRICAL: GENERAL SPECIFICATION FOR |
| MIL-PRF-1-1204 Revision H:2004 | ELECTRON TUBE, CATHODE RAY, TYPE 1DP1 |
| MIL-DTL-27190 Revision C:2006 | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-DTL-38159 Revision D:2015 | CONNECTORS, ELECTRIC, RAMP POWER, 416/240 VOLTS |
| SAE AS 1424 : 2014 | HOSE ASSEMBLIES, METAL, MEDIUM PRESSURE, HIGH TEMPERATURE |
| SAE AS 7510 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION |
| SAE AS 6369 : 2017 | COUPLING ASSEMBLY, V-BAND SHEET METAL WIDE FLANGE, PNEUMATIC TUBE |
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