|
SAE AS 1248 : 2012
|
MINIMUM STANDARD FOR GASEOUS OXYGEN PRESSURE REDUCERS |
|
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 P 81655 : 0
|
PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
|
MIL F 27272 : B
|
FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
|
MIL H 26626 : D
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, OXYGEN |
|
MIL P 9388 : B
|
PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
|
MIL T 5483 : D
|
TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
|
MIL T 27305 : C
|
TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
|
MIL C 7135 : F
|
COMPRESSOR, PNEUMATIC, 3000 PSI 2 SCFM AERO 2A AERO 2A-1 AERO 2B AND AERO 2B-1 |
|
SAE AS 1472 : 2013
|
HOSE ASSEMBLY, LOW PRESSURE, POTABLE WATER |
|
MIL P 83207 : B
|
PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
|
MIL H 25475 : B
|
HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
|
MIL H 8891 : A
|
HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
|
MIL STD 1655 : 0
|
FITTINGS, FLARELESS, CLASSIFICATION OF DEFECTS OF |
|
MIL C 7413 : B
|
COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR |
|
MIL H 5440 : H
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
|
MIL G 23337 : 0
|
GAGE - PRESSURE, DIAL INDICATING |
|
MIL T 26017 : C
|
TEST STAND, HYDRAULIC SYSTEM COMPONENTS, TYPE MK-3A (STAND, TEST, AIRCRAFT HYDRAULIC SYSTEM, ELECTRIC MOTOR DRIVEN, TYPE MK-3A) |
|
MIL P 8564 : D
|
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
|
MIL C 25973 : B
|
CONVERTER, LIQUID OXYGEN, GCU-12A/A |
|
MIL H 38390 : C
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE PNEUMATIC, HIGH PRESSURE |
|
MIL H 38360 : B
|
HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC |
|
MIL I 18802 : A
|
INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
|
MIL DTL 25666/3 : 0
|
CONVERTER, LIQUID OXYGEN GCU-10/A |
|
MIL I 85487 : 0
|
IGNITER, ROCKET MOTOR, MARK 297 MOD 1 |
|
MIL F 83296 : 0
|
FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
|
MIL V 87223 : 0
|
VALVE, PRESSURE, ANTI-G SUIT, MXU-804/A AND MXU-805/A |
|
MIL G 5514 : G
|
GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
|
MIL A 38726 : 0
|
ADAPTER ASSEMBLY, REUSABLE, FLEXIBLE HOSE, LOW PRESSURE |
|
MIL C 52716 : A NOTICE 1
|
COMPRESSOR AIR, RECIPROCATING ELECTRIC MOTOR DRIVEN 4 CFM 3100 PSIG (NOMINAL) |
|
MIL F 5509 : D
|
FITTING, FLARED TUBE, FLUID CONNECTION |
|
MIL R 47321 : 0
|
REGULATOR, PRESSURE |
|
MIL A 47309 : A
|
AMPLIFIER, PNEUMATIC |
|
MIL O 87226 : 0
|
OXYGEN SYSTEMS, AIRCRAFT |
|
MIL H 26633 : C
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, OXYGEN |
|
AN 919 : 0009
|
REDUCER - EXTERNAL THREAD FLARED TUBE |
|
SAE AS 1896 : 2013
|
COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC |
|
MIL P 25632 : B
|
PITOT STATIC TUBE, ELECTRICALLY HEATED, TEMPERATURE CONTROLLED, 115 VOLT, 4OO HZ, TYPE MA-1 |
|
MIL C 85247 : 0
|
COMPUTER, AIR DATA CP-1005A/A |
|
MIL DTL 25666/4 : 0
|
CONVERTER, LIQUID OXYGEN GCU-12A/A |
|
SAE AS 6302 : 2016
|
TRANSMITTER, PRESSURE, FUEL, 0-600 PSI |
|
MIL F 27656 : C
|
FILTER UNIT, FLUID, PRESSURE MXU-4O8/M, ABSOLUTE 5 MICRON, HYDRAULIC |
|
SAE AS 18802 : 2013
|
FUEL AND OIL LINES, AIRCRAFT, INSTALLATION OF |
|
MIL E 24572 : B
|
EXTINGUISHER, FIRE, BROMOTRIFLUOROMETHANE (HALON 13O1) SYSTEMS (FIXED PIPE, PNEUMATICALLY ACTUATED, NAVAL SHIPBOARD USE) |
|
MIL P 9389 : A
|
PUMP PRESSURE, OIL AND FREE AIR, TYPE MA AND 3 |
|
MIL P 83206 : B
|
PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
|
SAE AIR 825/2 : 2012
|
EFFECTS OF ACUTE ALTITUDE EXPOSURE IN HUMANS: REQUIREMENTS FOR PHYSIOLOGICAL PROTECTION |
|
MIL V 87255 : 0
|
VALVE, PRESSURE, ANTI-G SUIT, HIGH FLOW |
|
MIL P 85573 : 0
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
|
MIL E 18927 : E
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
SAE AS 4897 : 1994
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE (PTFE), LOW PRESSURE, 450 DEGREES F AND FIREPROOF, PROCUREMENT SPECIFICATION FOR |
|
MIL D 19326 : H
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL F 8615 : D
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
|
MIL S 8932 : A
|
SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL P 85315 : 0
|
PUMP, EJECTOR, AIR VEHICLE FUEL, GENERAL SPECIFICATION FOR |
|
MIL H 26666 : D (1)
|
HOSE ASSEMBLY, PNEUMATIC, HIGH PRESSURE |
|
MIL J 5513 : C
|
JOINT, HYDRAULIC SWIVEL |
|
MIL T 6302 : B
|
TRANSMITTER, PRESSURE, FUEL 0-600 PSI |
|
MIL P 38136 : A
|
PITOT STATIC TUBE COMPENSATED TRU 62/A |
|
MIL A 83039 : B
|
AIR CONDITIONER A/M32C-10A AIR CYCLE FOR AIRCRAFT GROUND SUPPORT |