MIL-A-8865 Revision B:1987
|
AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
MS33540 Revision J:1986
|
SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR |
MIL-STD-129 Revision R:2014
|
Military Marking for Shipment and Storage |
MIL-P-5315 Revision B:1964
|
PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT |
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
MS 33633 : LATEST
|
|
MIL S 6744 : LATEST
|
|
MIL-A-8591 Revision H:1990
|
AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR |
MIL R 6855 : E
|
RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES |
MS29513 Revision C:1966
|
PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, O RING |
QQ-C-320 Revision B:1974
|
CHROMIUM PLATING (ELECTRODEPOSITED) |
MIL T 6396 : E
|
TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
MS33588 Revision E:1984
|
NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
MS20995 Revision E:1974
|
WIRE, SAFETY OR LOCK |
MIL-F-17874 Revision B:1965
|
FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF |
MIL P 7936 : LATEST
|
PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY |
MIL-N-25161 Revision C:1969
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
MIL A 8625 : F
|
ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
MIL-H-8775 Revision D:1976
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
MIL R 6106 : J
|
RELAYS, ELECTROMAGNETIC [INCLUDING ESTABLISHED RELIABILITY [ER] TYPES |
MIL-S-4040 Revision G:2012
|
Solenoid, Electrical General Specification for (No S/S Document) |
MIL-P-6906 Revision B:1969
|
PLATE, IDENTIFICATION AIRCRAFT |
MIL-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-T-7928 Revision G:1976
|
TERMINAL, LUG SPLICES, CONDUCTOR, CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR |
MIL-P-116 Revision J:1988
|
PRESERVATION, METHODS OF |
MIL-L-19537 Revision C:1965
|
LACQUER, ACRYLIC NITROCELLULOSE GLOSS (FOR AIRCRAFT USE) |
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
MIL C 5015 : G
|
CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
MIL-H-5440 Revision H:1993
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL-I-18802 Revision A:1962
|
INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
MIL C 26482 : G
|
CONNECTOR, ELECTRICAL (CIRCULAR, MINIATURE, QUICK DISCONNECT, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS, GENERAL SPECIFICATION FOR |
MIL-C-5501 Revision G:1989
|
CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL |
QQ-P-416 Revision F:1991
|
PLATING, CADMIUM (ELECTRODEPOSITED) |
MIL-P-7962 Revision D:1980
|
PRIMER COATING, CELLULOSE NITRATE MODIFIED ALKYD TYPE, CORROSION INHIBITING, FAST DRYING [FOR SPRAY APPLICATION OVER PRETREATMENT COATING |
MIL-H-4495 Revision D:1985
|
HOSE ASSEMBLY, RUBBER, AERIAL REFUELING |
MIL-B-5087 Revision B:1964
|
BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
MIL C 6021 : H NOTICE 1
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
MIL-E-7080 Revision B:1962
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
MS33547 Revision C:1957
|
PIN, SPRING, FUNCTIONAL LIMITATIONS OF (ASG) |
MIL-F-7179 Revision G:1993
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
MIL-S-7742 Revision D:1991
|
SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
MIL N 25027 : G
|
NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |