SAE AS 1284 : 2015
|
STANDARD TEST PROCEDURE AND LIMIT VALUE FOR SHUTOFF SURGE PRESSURE OF PRESSURE FUEL DISPENSING SYSTEMS |
STANAG 3971 : 2013
|
AIR-TO-AIR REFUELLING - ATP-56 |
STANAG 3370 : 2004
|
AIRCREW STATION ALERTING SYSTEMS |
SAE ARP 1665 : 1997
|
DEFINITION OF PRESSURE SURGE TEST AND MEASUREMENT METHODS FOR RECEIVER AIRCRAFT |
STANAG 3217 : 2006
|
OPERATION OF CONTROLS AND SWITCHES AT AIRCREW STATIONS |
STANAG 3802 : 2008
|
SCREWDRIVER RECESSES (HIGH PERFORMANCE) |
MIL-F-8785 Revision C:1980
|
FLYING QUALITIES OF PILOTED AIRPLANES |
ISO 46:1973
|
Aircraft — Fuel nozzle grounding plugs and sockets |
MIL-STD-130 Revision N:2007
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
STANAG 7096 : 0
|
LOCATION, ACTUATION AND SHAPE OF AIRFRAME CONTROLS |
MIL-DTL-5624 Revision W:2016
|
TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
MIL-A-8863 Revision C:1993
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
MIL-HDBK-1763 Base Document:1998
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
STANAG 7041 : LATEST
|
INTEGRATED HELMET MOUNTED DISPLAYS FOR ROTARY WING AIRCRAFT |
ATP 56 : B
|
AIR TO AIR REFUELLING |
STANAG 3806 : 0
|
AIRCRAFT HIGH PRESSURE GASEOUS NITROGEN SYSTEMS REPLENISHMENT CONNECTORS |
STANAG 3869 : 0
|
AIRCREW STATION CONTROL PANELS |
STANAG 3294 : 0
|
AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
STANAG 3315 : 1998
|
AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
STANAG 3701 : 0
|
AIRCRAFT INTERIOR COLOUR SCHEMES |
STANAG 7090 : 2007
|
GUIDE SPECIFICATIONS FOR NATO GROUND FUELS |
MIL-T-81259 Revision B:1991
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
STANAG 7044 : 0
|
FUNCTIONAL ASPECTS OF MISSION PLANNING STATION INTERFACE DESIGN |
MIL-STD-1787 Revision B:1996
|
AIRCRAFT DISPLAY SYMBOLOGY |
STANAG 3278 : 2014
|
AIRCRAFT TOWING ATTACHMENTS AND DEVICES |
STANAG 3372 : 2014
|
LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING |
STANAG 3504 : 0
|
CATHODE RAY TUBE HEAD-DOWN DISPLAYS (MONOCHROME) |
MIL-N-5877 Revision E:1992
|
NOZZLE, PRESSURE FUEL SERVICING LOCKING TYPE D 1 AND D 2 NOMINAL 1 1/2 INCH DIAMETER |
JSSG-2007 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE |
STANAG 3681 : 0
|
CRITERIA FOR PRESSURE REFUELLING OF AIRCRAFT |
STANAG 3639 : 2004
|
AIRCREW STATION DIMENSIONAL DESIGN FACTORS |
ISO 102:1990
|
Aircraft — Gravity filling orifices |
MIL-STD-1760 Revision E:2007
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
STANAG 3870 : 0
|
EMERGENCY ESCAPE/EVACUATION LIGHTING |
STANAG 3595 : 2009
|
AIRCRAFT FITTING FOR PRESSURE REPLENISHMENT OF GAS TURBINE ENGINES WITH OIL |
MIL PRF 5624 : S
|
TURBINE FUEL, AVIATION, GRADES JP-4, JP-5 AND JP-5/JP-8 ST |
MIL-STD-411 Revision F:1997
|
AIRCREW STATION ALERTING SYSTEMS |
MIL P 15024 : E
|
PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT |
MIL C 83733/17 : 0
|
CONNECTOR, RACK AND PANEL, SPRING LOADED MOUNTING ASSEMBLY |
STANAG 3237 : 1997
|
APERTURE OF TERMINAL RING OR LINK OF AIRCRAFT LIFTING SLINGS |
MIL-PRF-25017 Revision H:2011
|
INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (NATO S-1747) |
STANAG 3847 : 0
|
HELICOPTER IN-FLIGHT REFUELLING (HIFR) EQUIPMENT |
MIL-HDBK-1791 Base Document:1997
|
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
STANAG 3800 : 2001
|
NIGHT VISION IMAGING SYSTEM (NVIS) INTERIOR LIGHTING COMPATIBILITY DESIGN CRITERIA |
MIL-DTL-85110 Revision B:1997
|
BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
STANAG 3647 : 0
|
NOMENCLATURE IN AIRCREW STATIONS |
STANAG 2947 : 0
|
TECHNICAL CRITERIA FOR A CLOSED CIRCUIT REFUELLING SYSTEM |
MIL-STD-464 Revision C:2010
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
STANAG 7042 : 0
|
IMAGE INTENSIFYING NIGHT VISION DEVICES FOR AIRCRAFT |
ASTM D 910 : 2017-05
|
SPECIFICATION FOR LEADED AVIATION GASOLINES |
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
STANAG 3499 : 0
|
CHARACTERISTICS OF SUPPLY EQUIPMENT FOR LIQUID OXYGEN |
STANAG 3098 : 2014
|
AIRCRAFT JACKING |
MIL-PRF-23699 Revision G:2014
|
Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167 |
MIL-STD-809 Revision B:1986
|
ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF |
STANAG 3224 : 2005
|
AIRCRAFT INTERIOR AND EXTERIOR LIGHTING NIGHT VISION GOGGLE (NVG) AND NON-NVG COMPATIBLE |
AAP-4 : 2004
|
NATO STANDARDIZATION AGREEMENTS AND ALLIED PUBLICATIONS |
RTCA DO 208 : 91 CHG NOT 1 93
|
MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR AIRBORNE SUPPLEMENTAL NAVIGATION EQUIPMENT USING GLOBAL POSITIONING SYSTEM (GPS) |
MIL-STD-882 Revision E:2012
|
System Safety |
STANAG 3547 : 0
|
CHARACTERISTICS OF REPLENISHMENT EQUIPMENT FOR LIQUID NITROGEN |
SAE ARP 1797 : 2014
|
AIRCRAFT AND AIRCRAFT ENGINE FUEL PUMP LOW LUBRICITY FLUID ENDURANCE TEST |
MIL-STD-461 Revision G:2015
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
MIL-STD-1773 Base Document:1988
|
FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
STANAG 3994 : 2007
|
APPLICATION OF HUMAN ENGINEERING TO ADVANCED AIRCREW SYSTEMS |
STANAG 7139 : 0
|
AIRCRAFT ENGINE CONTROLS, SWITCHES, DISPLAYS, INDICATORS, GAUGES AND ARRANGEMENTS |
MIL-HDBK-1797 Base Document:1997
|
FLYING QUALITIES OF PILOTED AIRCRAFT |
STANAG 3208 : 2009
|
AIR CONDITIONING CONNECTIONS |
MIL STD 1763 : A
|
AIRCRAFT STORES CERTIFICATION PROCEDURES |
MIL STD 1807 : NOTICE 1
|
CRASH SURVIVABILITY OF AIRCRAFT PERSONNEL |
MIL-DTL-83133 Revision J:2015
|
TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
MIL-A-8861 Revision B:1986
|
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
STANAG 3766 : 2017
|
GREASE NIPPLES |
STANAG 3632 : 0
|
AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
STANAG 3447 : 2016
|
AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
MIL-HDBK-1785 Base Document:1995
|
SYSTEM SECURITY ENGINEERING PROGRAM MANAGEMENT REQUIREMENTS |
STANAG 3871 : 2004
|
NATO GLOSSARY OF AIRCRAFT - AIRCREW INTEGRATION (AI) SPECIALIST TERMINOLOGY AND ABBREVIATIONS |
STANAG 3296 : 0
|
AIRCRAFT GASEOUS OXYGEN REPLENISHMENT COUPLINGS |
MIL-STD-1472 Revision G:2012
|
HUMAN ENGINEERING |
MIL T 83133 : D
|
TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
MIL-PRF-83282 Revision D:1997
|
HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
MIL-STD-1366 Revision E:2006
|
INTERFACE STANDARD FOR TRANSPORTABILITY CRITERIA |
SAE ARP 1420 : 2002
|
GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
STANAG 2946 : 0
|
FORWARD AREA REFUELLING EQUIPMENT |
MIL F 16884 : J
|
FUEL, NAVAL DISTILLATE |
STANAG 3705 : 0
|
HUMAN ENGINEERING DESIGN CRITERIA FOR CONTROLS AND DISPLAYS IN AIRCREW STATIONS |
MIL-A-8243 Revision D:1985
|
ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
MIL-HDBK-310 Base Document:1997
|
DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS |
MIL-STD-805 Revision B:1987
|
TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
AFGS-87242 Revision A:1991
|
FLIGHT CONTROL SYSTEM - GENERAL SPECIFICATION FOR |
STANAG 3258 : 0
|
POSITION OF PILOT OPERATED NAVIGATION AND RADIO CONTROLS |
ISO 45:1990
|
Aircraft — Pressure refuelling connections |
STANAG 3219 : 0
|
LOCATION AND GROUPING OF ELECTRICAL SWITCHES IN AIRCRAFT |
MIL STD 1533 : 0
|
AIRCRAFT INTERNAL TIME DIVISION COMMAND RESPONSE MULTIPLEX DATA BUS |
STANAG 3436 : 0
|
COLOURS AND MARKINGS USED TO DENOTE OPERATING RANGES OF AIRCRAFT INSTRUMENTS |
STANAG 7140 : 0
|
AIRCRAFT FLIGHT INSTRUMENTS - LAYOUT AND DISPLAY |
STANAG 3105 : 2014
|
PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT |
STANAG 3329 : 0
|
NUMERALS AND LETTERS IN AIRCREW STATIONS |
RTCA DO 236 : C2013 CHG 1 2014
|
MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS: REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION |
JSSG-2010-5 Base Document:1998
|
Crew Systems Aircraft Lighting Handbook |
STANAG 3950 : 0
|
HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
STANAG 3209 : 2014
|
TYRE VALVE COUPLINGS |
STANAG 3682 : 0
|
ELECTROSTATIC SAFETY CONNECTION PROCEDURES FOR AVIATION FUEL HANDLING AND LIQUID FUEL LOADING/UNLOADING OPERATIONS DURING GROUND TRANSFER AND AIRCRAFT FUELLING/DEFUELLING |
STANAG 3212 : 2017
|
DIAMETERS FOR GRAVITY FILLING ORIFICES |
MIL-HDBK-1760 Revision A:2004
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |