MIL B 7874 : B
|
BOLT, MACHINE 1200 DEGREES F |
PPP T 76 : C
|
TAPE, PRESSURE SENSITIVE ADHESIVE, PACKAGING/PAPER (FOR CARTON SEALING) |
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
MS 27611 : G
|
VALVE, HYDRAULIC BLEEDER, AIRCRAFT WHEEL BRAKE |
MIL I 8500 : D
|
INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
MIL STD 129 : R
|
MILITARY MARKING FOR SHIPMENT AND STORAGE |
MIL STD 970 : 0
|
STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF |
MS 15795 : G
|
WASHER, FLAT METAL ROUND GENERAL PURPOSE (IN./MM) |
MIL STD 130 : N
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
MIL A 8863 : C
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
MIL R 8791/1 : 0
|
RETAINER, PACKING, HYDRAULIC AND PNEUMATIC, POLYTETRAFLUOROETHYLENE RESIN, (SINGLE TURN) |
PPP B 636 : J
|
BOX, SHIPPING, FIBERBOARD |
AN 960 : 0021
|
WASHER, FLAT |
MIL C 81907 : 0
|
COATING SYSTEM, POLYURETHANE, ALIPHATIC, WEATHER RESISTANT, PROCESS FOR APPLICATION OF |
MS 20002 : E
|
WASHER, COUNTERSUNK AND PLAIN, HIGH STRENGTH |
MIL C 25427 : A
|
COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT |
ASTM D 1141 : 1998 : EDT 1
|
Standard Practice for the Preparation of Substitute Ocean Water |
MIL V 19068 : A
|
VALVE, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 11 SYSTEMS |
MIL STD 2073/1 : E
|
STANDARD PRACTICE FOR MILITARY PACKAGING |
MIL H 6875 : H
|
HEAT TREATMENT OF STEEL RAW MATERIALS |
MIL A 22771 : D
|
ALUMINUM ALLOY FORGINGS, HEAT TREATED |
MS 14157 : B
|
BOLT WHEEL TENSION FLANGED STEEL 180KSI FTU 450 DEG F EXTEND SPLINE DRIVE |
MIL B 8584 : C
|
BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF |
MIL S 8802 : F
|
SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION |
MIL F 18264 : D
|
FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
MIL L 81352 : A
|
LACQUER, ACRYLIC (FOR NAVAL WEAPONS SYSTEMS) |
MIL S 5002 : D
|
SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
MIL P 23377 : G
|
PRIMER COATING, EPOXY, HIGH SOLIDS |
MIL T 9046 : J
|
TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE |
MIL STD 2175 : A
|
CASTING, CLASSIFICATION AND INSPECTION OF |
MIL HDBK 275 : A
|
GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
MIL STD 470 : B
|
MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
MIL STD 889 : C
|
DISSIMILAR METALS |
MIL B 121 : F
|
BARRIER MATERIAL, GREASEPROOFED, WATERPROOFED, FLEXIBLE |
PPP T 60 : E
|
TAPE, PACKAGING, WATERPROOF |
MIL STD 6866 : 0
|
INSPECTION, LIQUID PENETRANT |
QQ C 320 : B
|
CHROMIUM PLATING (ELECTRODEPOSITED) |
MIL F 7190 : B
|
FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL STD 838 : C
|
LUBRICATION OF MILITARY EQUIPMENT |
MIL T 10727 : C
|
TIN PLATING, ELECTRODEPOSITED OR HOT-DIPPED FOR FERROUS AND NONFERROUS METALS |
MIL STD 2154 : 0
|
INSPECTION, ULTRASONIC, WROUGHT METALS, PROCESS FOR |
MIL I 6870 : E
|
INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
MIL B 6812 : E
|
BOLTS, AIRCRAFT |
QQ A 596 : E
|
ALUMINUM ALLOY PERMANENT AND SEMI-PERMANENT MOLD CASTINGS |
MIL G 5514 : G
|
GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR |
SAE AS 666 : 1982
|
CAVITY DESIGN AND O-RING SELECTION FOR STATIC SEAL USE IN AIRCRAFT TUBELESS TIRE WHEELS |
MS 14177 : B
|
ADAPTER,AIR TURBINE STARTER TO ENGINE MOUNTING |
MIL STD 882 : E
|
STANDARD PRACTICE FOR SYSTEM SAFETY |
MIL B 7838 : C
|
BOLT, INTERNAL WRENCHING 160 KSI FTU |
MS 27436 : B
|
VALVE SPECIAL, AIRCRAFT WHEEL |
MIL C 5541 : E
|
CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
MIL S 8879 : C
|
SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR |
MIL T 5041 : J
|
TIRE, PNEUMATIC, AIRCRAFT |
MIL A 8868 : B
|
AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS |
MIL A 8625 : F
|
ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
MIL H 8775 : D
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
MIL A 21180 : D
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
MS 14155 : 0
|
WASHER, RECESSED COUNTERSUNK TWO SURFACES FOR USE WITH WHEEL BOLTS AND NUTS UP TO AND INCLUDING 180 KSI FTU |
TT P 28 : H
|
PAINT, ALUMINUM, HEAT RESISTING |
MIL P 116 : J
|
PRESERVATION, METHODS OF |
MIL STD 1472 : G
|
HUMAN ENGINEERING |
QQ A 601 : F
|
ALUMINUM ALLOY SAND CASTINGS |
MIL T 18303 : B
|
TEST PROCEDURES, REPRODUCTION, ACCEPTANCE, AND LIFE FOR AIRCRAFT ELECTRONIC EQUIPMENT, FORMAT FOR |
MIL H 5440 : H
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
MIL P 81985 : 0
|
PEENING OF METALS |
QQ P 416 : F
|
PLATING, CADMIUM (ELECTRODEPOSITED) |
MIL G 83016 : NOTICE 1
|
GAGE, AIRCRAFT WHEEL, INTEGRAL, TIRE PRESSURE INDICATING |
MIL P 83461 : B
|
PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C) |
MIL C 8837 : B
|
COATING, CADMIUM (VACUUM DEPOSITED) |
MS 14156 : 0
|
NUT, WHEEL SELF LOCKING FLANGED STEEL 180 KSI FTU 450 DEG F SPINE DRIVE |
MIL T 5544 : C
|
THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM |
MIL B 8831 : B
|
BOLT, 180 KSI FTU AND 180 KSI FSU 450 DEG F PROTRUDING AND FLUSH HEAD, GENERAL SPECIFICATION FOR |
MIL G 4343 : C
|
GREASE, PNEUMATIC SYSTEMS |
MIL G 81322 : E
|
GREASE, AIRCRAFT, GENERAL PURPOSE, SIDE TEMPERATURE RANGE, NATO CODE NUMBER G-395 |
MIL STD 105 : E
|
SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
MIL C 83286 : B
|
COATING URETHANE, ALIPHATIC ISOCYANATE, FOR AEROSPACE APPLICATIONS |
MIL F 3541 : C
|
FITTING, LUBRICATION, GENERAL SPECIFICATION FOR |
FED STD 595 : C
|
COLORS USED IN GOVERNMENT PROCUREMENT |
MIL STD 785 : B
|
RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
PPP C 843 : D
|
CUSHIONING MATERIAL, CELLULOSIC |
MIL F 83142 : A
|
FORGING, TITANIUM ALLOYS, PREMIUM QUALITY |
SAE AS 707 : 2013
|
THERMAL SENSITIVE INFLATION PRESSURE RELEASE DEVICES FOR TUBELESS AIRCRAFT WHEELS |
MIL F 7179 : G
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
MIL A 8860 : B
|
AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
MIL P 81958 : 0
|
PRESSURE RELIEF DEVICES, OVERPRESSURIZATION PREVENTION, WHEEL/TIRE, AIRCRAFT |