|
A A 59155 : 0
|
NITROGEN, HIGH PURITY, SPECIAL PURPOSE |
|
NASM 1515 : 0
|
FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS |
|
SAE AMS I 7171 : 2011
|
INSULATION BLANKET, THERMAL ACOUSTICAL |
|
SAE AS 1284 : 2015
|
STANDARD TEST PROCEDURE AND LIMIT VALUE FOR SHUTOFF SURGE PRESSURE OF PRESSURE FUEL DISPENSING SYSTEMS |
|
A A 59503 : C
|
NITROGEN, TECHNICAL |
|
SAE AS 21237 : 2011
|
RING, CARGO TIEDOWN (25,000 LB), TYPE 4 |
|
STANAG 3971 : 2013
|
AIR-TO-AIR REFUELLING - ATP-56 |
|
MIL A 25896 : E
|
ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER |
|
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
|
SAE ARP 699 : 2015
|
HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT |
|
SAE AIR 781 : 1962
|
GUIDE FOR DETERMINING ENGINE STARTER DRIVE TORQUE REQUIREMENTS |
|
SAE ARP 1665 : 1997
|
DEFINITION OF PRESSURE SURGE TEST AND MEASUREMENT METHODS FOR RECEIVER AIRCRAFT |
|
SAE AIR 1102 : 2011
|
TRANSPARENT AREA WASHING SYSTEMS FOR AIRCRAFT |
|
ABMA 9 : 2015
|
LOAD RATINGS AND FATIGUE LIFE FOR BALL BEARINGS |
|
SAE AIR 1826 : 2016
|
ACOUSTICAL CONSIDERATIONS FOR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM DESIGN |
|
MIL PRF 6083 : G
|
HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
|
MIL STD 704 : F
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
|
SAE AS 943 : 1986
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE, GENERAL SPECIFICATION FOR |
|
SAE AS 81820 : 2014
|
BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION |
|
MS 3325 : 0
|
DRIVE PAD-ACCESSORY, 2.653 BC SQUARE, DESIGN STANDARD FOR |
|
MIL STD 130 : N
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
|
A A 59281 : A
|
CLEANING COMPOUND, SOLVENT MIXTURES |
|
MIL A 8863 : C
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
|
MIL PRF 46170 : E
|
HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544 |
|
MIL STD 883 : K
|
TEST METHOD STANDARD - MICROCIRCUITS |
|
ABMA 11 : 2014
|
LOAD RATINGS AND FATIGUE LIFE FOR ROLLER BEARINGS |
|
SAE AMS P 5510 : 2013
|
O-RING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS, TYPE 1 HYDRAULIC (-65 TO 160 DEGREES F) |
|
MIL STD 878 : B
|
METHOD OF DIMENSIONING AND DETERMINING CLEARANCE FOR AIRCRAFT TIRES AND RIMS |
|
STANAG 3294 : 0
|
AIRCRAFT FUEL CAPS AND FUEL CAP ACCESS COVERS |
|
SAE AS 7949 : 2004
|
BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD |
|
SAE ARP 8615 : 2011
|
FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR |
|
STANAG 3315 : 1998
|
AIRCRAFT CABIN PRESSURIZING TEST CONNECTIONS |
|
MIL STD 810 : G
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
MIL PRF 7808 : L
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
|
MIL T 81259 : B
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
|
BB E 2879 : A
|
EXTINGUISHER, FIRE, CARBON DIOXIDE (CO[2]), PORTABLE, WITH MOUNTING BRACKET, FOR AVIATION USE |
|
SAE AIR1639A : 1999
|
SAFETY CRITERIA FOR PNEUMATIC STARTING SYSTEMS |
|
STANAG 3109 : 2014
|
SYMBOL MARKING OF AIRCRAFT SERVICING AND SAFETY/HAZARDS POINTS |
|
AS 3990-1993
|
Mechanical equipment - Steelwork (Reconfirmed 2016) |
|
MIL STD 2218 : 0
|
THERMAL DESIGN, ANALYSIS & TEST PROCEDURES FOR AIRBORNE ELECTRONIC EQUIPMENT |
|
SAE AIR1184B : 2016
|
CAPACITIVE FUEL GAUGING SYSTEM ACCURACIES |
|
STANAG 3278 : 2014
|
AIRCRAFT TOWING ATTACHMENTS AND DEVICES |
|
SAE AIR 1467 : 1999
|
GAS ENERGY LIMITED STARTING SYSTEMS |
|
SAE AIR 1204 : 2009
|
CONTROL OF WATER CARRYOVER FROM THE ENVIRONMENTAL CONTROL SYSTEM AND CONDENSATION ON THE STRUCTURE |
|
STANAG 3372 : 2014
|
LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING |
|
SAE ARP 85 : 2012
|
AIR CONDITIONING SYSTEMS FOR SUBSONIC AIRPLANES |
|
MIL B 8584 : C
|
BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF |
|
JSSG 2000 : B
|
AIR SYSTEM |
|
JSSG 2007 : 0
|
JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE |
|
MS 3326 : 0
|
DRIVE PAD - ACCESSORY, 5,000 BC SQUARE, DESIGN STANDARD FOR |
|
MIL STD 1791 : C
|
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
|
SAE AS 1055 : 2013
|
FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS |
|
MIL DTL 7891 : G
|
FILLER VALVE, AIRCRAFT OXYGEN |
|
SAE AS 5877 : 2016
|
DETAILED SPECIFICATION FOR AIRCRAFT PRESSURE REFUELING NOZZLE |
|
JSSG 2010 : 1998
|
CREW SYSTEMS |
|
SAE AS 18802 : 2013
|
FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
|
SAE AS 6882 : 1999
|
WATER REPELLENT, WINDOW AND WINDSHIELD, GLASS AND PLASTIC |
|
MIL DTL 5513 : D
|
SWIVEL JOINT, HYDRAULIC |
|
SAE AS 8905 : 2012
|
FITTINGS AND CARGO RINGS, TIE-DOWN, AIRCRAFT FLOOR |
|
SAE AIR 1174 : 2001
|
INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS |
|
SAE AS 5440 : 2011
|
HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
|
SAE AMS P 83461 : 1998
|
PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEG F (135 DEG C) |
|
MS 3329 : A
|
DRIVE PAD - ACCESSORY, 10,000 BC ROUND, DESIGN STANDARD FOR |
|
MIL E 7016 : F
|
ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
|
SAE AIR 1662 : 2013
|
MINIMIZATION OF ELECTROSTATIC HAZARDS IN AIRCRAFT FUEL SYSTEMS |
|
MS 3328 : A
|
DRIVE PAD - ACCESSORY, 8,000 BC ROUND, DESIGN STANDARD FOR |
|
SAE AMS 2430 : 2015
|
SHOT PEENING |
|
MIL STD 411 : F
|
AIRCREW STATION ALERTING SYSTEMS |
|
SAE AIR 1087 : 1999
|
AIRCRAFT ACCESSORY DRAG TORQUE DURING ENGINE STARTS |
|
DOD PRF 85734 : A
|
LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE |
|
MIL HDBK 1568 : 0
|
MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
|
MIL HDBK 454 : B
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
|
SAE AIR 1667 : 2013
|
ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS |
|
SAE AS 6038 : 2011
|
BEARINGS, BALL, BELLCRANK, ANTIFRICTION, AIRFRAME |
|
NASM 1312 : 0
|
FASTENER TEST METHODS METHOD 11 TENSION FATIGUE |
|
SAE ARP 1270 : 2015
|
AIRCRAFT CABIN PRESSURIZATION CRITERIA |
|
MIL STD 7080 : 0
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
|
SAE AS 50141 : 2012
|
TUBE, PNEUMATIC TIRE, AIRCRAFT |
|
MS 9950 : 0
|
COVER ACCESSORY DRIVE 5,000 BC ROUND QAD |
|
MIL PRF 87257 : C
|
HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
|
SAE AIR 1811 : 2015
|
LIQUID COOLING SYSTEMS |
|
MS 3336 : 0
|
ACCESSORY DRIVES AIRCRAFT ENGINE, REFERENCE CHART FOR |
|
MIL STD 464 : C
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
|
SAE AS 90362 : 2016
|
CONNECTOR, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, 115/200 VOLT, 400 HERTZ |
|
MIL PRF 18148/3 : 0
|
RECEPTACLES, ELECTRIC, AIRCRAFT STORAGE BATTERY |
|
MIL PRF 83323 : D
|
TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
|
SAE AS 21236 : 2011
|
RING, CARGO TIEDOWN (10,000 LB), TYPE 3 |
|
SAE AIR 1243 D: 2013(S2018)
|
ANTI BLOW-BY DESIGN PRACTICE FOR CAP SEALS |
|
SAE AIR 1160 : 1999
|
AIRCRAFT ENGINE AND ACCESSORY DRIVES AND FLANGE STANDARDS |
|
STANAG 3098 : 2014
|
AIRCRAFT JACKING |
|
SAE ARP 994 : 2016
|
DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
|
MIL PRF 23699 : G
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE, NATO CODE NUMBERS: O-152, O-154, O-156, AND O-167 |
|
SAE AIR 1277 : 2005
|
COOLING OF MILITARY AVIONIC EQUIPMENT |
|
MIL L 22589 : D
|
LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT |
|
MS 9949 : 0
|
COVER - ACCESSORY DRIVE 8,000 BC ROUND QAD |
|
MIL STD 1568 : D
|
MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
|
MIL L 8552 : C
|
LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE] |
|
JSSG 2001 : B
|
AIR VEHICLE |
|
MIL HDBK 5400 : 0
|
ELECTRONIC EQUIPMENT, AIRBORNE GENERAL GUIDELINES FOR |
|
MIL DTL 38999 : M
|
CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET, THREADED OR BREECH COUPLING), ENVIRONMENT RESISTANT WITH CRIMP REMOVABLE CONTACTS OR HERMETICALLY SEALED WITH FIXED, SOLDERABLE CONTACTS, GENERAL SPECIFICATION FOR |
|
MIL STD 1290 : A
|
LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
|
SAE AS 8879 : 2004
|
SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
|
MIL N 25161 : C
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
|
MIL S 8812 : D
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
|
MIL STD 882 : E
|
STANDARD PRACTICE FOR SYSTEM SAFETY |
|
SAE AS 6039 : 2009
|
BEARINGS, BALL, ROD END, DOUBLE ROW, SELF-ALIGNING |
|
MIL STD 203 : G
|
AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT |
|
STANAG 3747 : 2016
|
GUIDE SPECIFICATIONS (MINIMUM QUALITY STANDARDS) FOR AVIATION TURBINE FUELS (F-24, F-27, F-34, F-35, F-37, F-40 AND F-44) |
|
SAE AIR 4069 : 2016
|
SEALING OF INTEGRAL FUEL TANKS |
|
MS 33740 : C
|
NIPPLE, PNEUMATIC STARTING, 3 INCH ID |
|
STANAG 3208 : 2009
|
AIR CONDITIONING CONNECTIONS |
|
SAE AS 21235 : 2011
|
FITTING, TIEDOWN, CARGO RING (10,000 LB) AND SEAT STUD, TYPE 2 |
|
SAE AS 5498 : 2001
|
MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS |
|
NAS 331 : 0
|
BEARING INSTALLATION AND RETENTION BY SWAGING OR STAKING |
|
MIL T 26561 : C
|
TESTER, TYPE MA-2 RECEPTION COUPLING BREAK-AWAY FORCE, PORTABLE |
|
MIL PRF 5041 : K
|
TIRES, RIBBED TREAD, PNEUMATIC, AIRCRAFT |
|
SAE AIR 1539 : 2007
|
ENVIRONMENTAL CONTROL SYSTEM CONTAMINATION |
|
STANAG 3632 : 0
|
AIRCRAFT AND GROUND SUPPORT EQUIPMENT ELECTRICAL CONNECTIONS FOR STATIC GROUNDING |
|
SAE AS 8775 : 1998
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
|
STANAG 3447 : 2016
|
AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
|
SAE ARP 731 : 2015
|
GENERAL REQUIREMENTS FOR APPLICATION OF VAPOR CYCLE REFRIGERATION SYSTEMS FOR AIRCRAFT |
|
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
|
MIL STD 1472 : G
|
HUMAN ENGINEERING |
|
SAE AS 21234 : 2011
|
FITTING, TIEDOWN, CARGO RING (5,000 LB) AND SEAT STUD, TYPE 1 |
|
MIL PRF 83282 : D
|
HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
|
MIL PRF 87260 : B
|
FOAM MATERIAL, EXPLOSION SUPPRESSION, INHERENTLY ELECTROSTATICALLY CONDUCTIVE, FOR AIRCRAFT FUEL TANKS |
|
SAE ARP 1796 : 2015
|
ENGINE BLEED AIR SYSTEMS FOR AIRCRAFT |
|
MS 9948 : 0
|
COVER - ACCESSORY DRIVE 10,000 BS ROUND QAD |
|
SAE AIR 4766/2 : 2005
|
AIRBORNE CHEMICALS IN AIRCRAFT CABINS |
|
MIL F 8815 : D
|
FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
|
SAE ARP 584D : 2012
|
COILED TUBING - CORROSION RESISTANT STEEL, HYDRAULIC APPLICATIONS, AEROSPACE |
|
MIL A 18717 : C
|
ARRESTING HOOK INSTALLATIONS, AIRCRAFT |
|
MIL HDBK 310 : 0
|
DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS |
|
SAE ARP 4386 : 2010
|
TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
|
MIL HDBK 1599 : A
|
BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS |
|
MIL STD 805 : B
|
TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
|
STANAG 7073 : 2017
|
CONNECTORS FOR AIRCRAFT ELECTRICAL SERVICING POWER |
|
SAE ARP 777 : 2014
|
GAS ACTUATORS (LINEAR AND VANE ROTARY TYPE) |
|
SAE AS 35061 : 2013(R 2018)
|
CONNECTOR, RECEPTACLE EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC OPERATING POWER |
|
AASSEP-2 : 2014
|
PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT |
|
MIL HDBK 1587 : 0
|
MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
|
SAE ARP 986 : 2015
|
GUIDE FOR QUALIFICATION TESTING OF AIRCRAFT AIR VALVES |
|
SAE AS 8914 : 2016
|
BEARING, ROLLER, SELF-ALIGNING, AIRFRAME, ANTIFRICTION |
|
STANAG 7036 : 97 AMD 1
|
FUELS TO BE INTRODUCED INTO AND DELIVERED BY THE NATO PIPELINE SYSTEM (NPS) |
|
SAE ARP 4058 : 2007
|
GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
|
AASSEP-1 : 2014
|
AIRCRAFT JACKING |
|
MIL DTL 5498 : G
|
ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
|
SAE ARP 949 : 1999
|
TURBINE ENGINE STARTING SYSTEM DESIGN REQUIREMENTS |
|
STANAG 3105 : 2014
|
PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT |
|
ISO 12103-1:2016
|
Road vehicles — Test contaminants for filter evaluation — Part 1: Arizona test dust |
|
MIL DTL 27422 : F
|
TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT |
|
MIL HDBK 189 : C
|
RELIABILITY GROWTH MANAGEMENT |
|
STANAG 1135 : 2017
|
INTERCHANGEABILITY OF FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS USED BY THE ARMED FORCES OF THE NORTH ATLANTIC TREATY NATIONS |
|
MS 3327 : A
|
DRIVE PAD - ACCESSORY, 5,000 BC, ROUND, DESIGN STANDARD FOR |
|
ASTM D 5632/D5632M : 2017 : REDLINE
|
Standard Specification for Halon 1301, Bromotrifluoromethane (CF3Br) |
|
MS 17793 : B
|
SCHEMATIC WIRING DIAGRAM (EXTERNAL AC POWER CONNECTOR AIRCRAFT) |
|
MIL STD 1798 : C
|
MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
|
ASTM D 471 : 2016-02
|
TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS |
|
JSSG 2006 : 0
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
|
SAE AS 5202 : 2005
|
PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD |
|
MIL DTL 83413/6 : C
|
CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING: RECEPTACLES, TWO PIECE, WITH INSERTS AND HOUSINGS |
|
SAE ARP 4255 : 2012
|
ELECTRICAL ACTUATION SYSTEMS FOR AEROSPACE AND OTHER APPLICATIONS |
|
SAE AIR 1609 : 2005
|
AIRCRAFT HUMIDIFICATION |
|
MIL HDBK 221 : 0
|
FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
|
SAE AIR 4246 : 2012
|
CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING |
|
STANAG 3209 : 2014
|
TYRE VALVE COUPLINGS |
|
MIL A 8860 : B
|
AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
|
SAE AS 33611 : 2015
|
TUBE BEND RADII |
|
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
|
SAE AIR 4023 : 2016
|
AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS |
|
STANAG 3212 : 2017
|
DIAMETERS FOR GRAVITY FILLING ORIFICES |
|
SAE AIR 713 : 1988
|
GUIDE FOR DETERMINING, PRESENTING, AND SUBSTANTIATING TURBINE ENGINE STARTING AND MOTORING CHARACTERISTICS |
|
MIL STD 961 : E
|
DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT |
|
SAE ARP 1107 : 2012
|
TAIL BUMPERS FOR PILOTED AIRCRAFT |