MIL-I-81550 Revision C:1983
|
INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE
|
MIL S 25057 : B
|
SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR
|
MIL T 25920 : C
|
TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION
|
MIL-E-22285 Base Document:1959
|
EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF
|
MIL C 25427 : A
|
COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT
|
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
|
MIL-H-38360 Revision B:1966
|
HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC
|
MIL H 25579 : E
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
|
MIL A 8064 : B NOTICE 1
|
ACTUATOR AND ACTUATING SYSTEMS, AIRCRAFT ELECTROMECHANICAL, GENERAL REQUIREMENTS FOR
|
MIL-D-8181 Revision B:1965
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR
|
MIL-STD-889 Revision C:2016
|
DISSIMILAR METALS
|
MIL E 5009 : D
|
|
MIL-STD-831 Base Document:1963
|
TEST REPORTS, PREPARATION OF
|
MIL C 27536 : B
|
COUPLING, CLAMP, GROOVED, V-BAND
|
MIL S 8516 : F
|
SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED
|
MIL-E-5007 Revision D:1973
|
ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
|
MIL-STD-143 Revision B:1969
|
STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
|
MIL-STD-882 Revision E:2012
|
System Safety
|
TT-P-59 Revision E:1975
|
PAINT, READY, MIXED, INTERNATIONAL ORANGE (NOT FOR RESIDENTIAL USE)
|
MIL-STD-203 Revision G:1991
|
AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT
|
MIL S 23586 : E
|
SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED
|
MIL-STD-250 Revision D:1974
|
AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT
|
MIL F 38363 : B (3)
|
FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
|
MIL-E-38453 Revision A:1971
|
ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR
|
MIL-C-7413 Revision B:1970
|
COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR
|
MIL-D-17984 Revision A:1956
|
DATA PRESENTATION REQUIREMENTS, INSTALLED PERFORMANCE AND AIR INDUCTION SYSTEMS (ASG)
|
MS33611 Revision A:1983
|
TUBE BEND RADII
|
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
|
MIL C 7958 : A
|
CONTROL, PUSH PULL, FLEXIBLE AND RIGID
|
MIL H 8795 : D
|
HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT
|
MIL-A-9482 Base Document:1954
|
ANTI-ICING EQUIPMENT FOR AIRCRAFT HEATED SURFACE TYPE, GENERAL SPECIFICATION FOR
|
MIL-W-5088 Revision L:1991
|
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
|
MIL-F-7179 Revision G:1993
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
|
MS33790 Base Document:1958
|
BEND DATA, MINIMUM, HYDRAULIC, PNEUMATIC, FUEL AND OIL HOSE
|
MS33602 Base Document:1967
|
BOLT, SELF RETAINING AIRCRAFT RELIABILITY AND MAINTAINABILITY DESIGN AND USAGE REQUIREMENTS FOR
|