MIL I 81550 : C
|
INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE |
MIL W 87161 : 0
|
WIRE STRAND, NONFLEXIBLE, FOR AIRCRAFT CONTROL |
MIL S 46059 : C NOTICE 1
|
STEEL, CARBON & ALLOY, EXTRUDED SHAPES |
MIL HDBK 5 : G_VOL2
|
METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
MIL M 24041 : C
|
MOLDING AND POTTING COMPOUND |
MIL R 9299 : C
|
RESIN, PHENOLIC, LAMINATING |
SAE AMS 4890 : 2012
|
COPPER-BERYLLIUM ALLOY CASTINGS, 97CU - 2.1BE - 0.52CO - 0.28SI, SOLUTION HEAT TREATED (TB00) |
MIL STD 1530 : D
|
AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
MIL A 8892 : 0
|
AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
MIL A 46146 : B
|
ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) |
QQ P 35 : C
|
PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL |
MIL A 8893 : 0
|
AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
MIL A 8863 : C
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
MIL M 46062 : C
|
MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH |
MIL STD 2066 : 0
|
CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN |
SAE AMS 5581 : 2010
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS OR WELDED TUBING, 62NI - 21.5CR - 9.0MO - 3.7CB (NB), ANNEALED |
QQ A 200 : E
|
ALUMINUM ALLOY, BAR, ROD, SHAPES, STRUCTURAL SHAPES, TUBE AND WIRE, EXTRUDED, GENERAL SPECIFICATION FOR |
MIL STD 810 : G
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL T 81556 : A
|
TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
MIL T 81259 : B
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
MIL H 6875 : H
|
HEAT TREATMENT OF STEEL RAW MATERIALS |
MIL A 22771 : D
|
ALUMINUM ALLOY FORGINGS, HEAT TREATED |
MIL B 85110 : A
|
BAR, REPEATABLE RELEASE HOLDBACK, AIRCRAFT LAUNCHING, GENERAL DESIGN REQUIREMENTS FOR |
MIL G 25871 : B
|
GLASS, LAMINATED, AIRCRAFT GLAZING |
MIL STD 5400 : 0
|
ELECTRONIC EQUIPMENT, AIRBORNE, GENERAL REQUIREMENTS FOR |
ASTM G 85 : 2011 : REDLINE
|
Standard Practice for Modified Salt Spray (Fog) Testing |
MIL S 8802 : F
|
SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION |
MIL A 008861 : A
|
|
MIL E 6051 : D
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
MIL A 8870 : C
|
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
MIL STD 45662 : A
|
CALIBRATION SYSTEMS REQUIREMENTS |
QQ C 390 : B
|
COPPER ALLOY CASTINGS (INCLUDING CAST BAR) |
MIL S 5002 : D
|
SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
QQ A 367 : H
|
ALUMINUM ALLOY FORGINGS |
MIL G 5485 : D
|
GLASS; LAMINATED, FLAT, BULLET RESISTANT |
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 P 7034 : D
|
PULLEY, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT |
MIL STD 889 : C
|
DISSIMILAR METALS |
MIL STD 866 : C
|
GRINDING OF CHROME PLATED STEEL AND STEEL PARTS HEAT TREATED TO 180,000 PSI OR OVER |
MIL P 9400 : C
|
PLASTIC LAMINATE AND SANDWICH CONSTRUCTION PARTS, AIRCRAFT STRUCTURAL PROCESS SPECIFICATION REQUIREMENTS |
MIL A 8862 : 0
|
AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
MIL F 7190 : B
|
FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL STD 838 : C
|
LUBRICATION OF MILITARY EQUIPMENT |
MIL STD 1595 : A
|
QUALIFICATION OF AIRCRAFT, MISSILE AND AEROSPACE FUSION WELDERS |
MIL I 6870 : E
|
INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL STD 1515 : A
|
FASTENER SYSTEMS FOR AEROSPACE APPLICATION |
MIL S 8516 : F
|
SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
MIL L 22589 : D
|
LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT |
MIL STD 1757 : A
|
LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE |
MIL STD 2219 : A
|
FUSION WELDING FOR AEROSPACE APPLICATIONS |
MIL H 83282 : C
|
HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
MIL STD 1568 : D
|
MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
MIL STD 1587 : D
|
MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
MIL STD 2000 : A
|
STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES |
ASTM E 390 : 2015 : REDLINE
|
Standard Reference Radiographs for Steel Fusion Welds |
MIL B 7883 : B
|
BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS |
MIL S 8879 : C
|
SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR |
MIL A 008870 : A
|
AIRPLANE STRENGTH AND RIGIDITY FLUTTER, DIVERGENCE AND OTHER AEROELASTIC INSTABILITIES |
MIL A 8871 : A
|
AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS |
MIL M 38795 : B
|
MANUAL, TECHNICAL, SYSTEM PECULIAR CORROSION CONTROL PREPARATION OF. |
MIL S 23586 : E
|
SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED |
MIL T 29586 : 0
|
THERMOSETTING POLYMER MATRIX, UNIDIRECTIONAL CARBON FIBER REINFORCED PREPREG TAPE (WIDTHS UP TO 60 INCHES), GENERAL SPECIFICATION FOR |
MS 33522 : C
|
RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED AND FRICTION RETAINER SPINDLE, (RELIABILITY MAINTAINABILITY) DESIGN AND CONSTRUCTION REQUIREMENTS |
MIL A 21180 : D
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
MIL T 83399 : 0
|
TEST FOR REMOVAL OF FLUX RESIDUES |
MIL S 81733 : C
|
SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
MIL A 8866 : C
|
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
MIL S 29574 : 0
|
SEALING COMPOUND, POLYTHIOETHER, FOR AIRCRAFT STRUCTURES, FUEL AND HIGH TEMPERATURE RESISTANT, FAST CURING AT AMBIENT AND LOW TEMPERATURE |
ASTM B 194 : 2015 : REDLINE
|
Standard Specification for Copper-Beryllium Alloy Plate, Sheet, Strip, and Rolled Bar |
MIL STD 1599 : 0
|
BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS |
SAE AMS 5343 : 2014
|
STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB (NB) - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H1000), 150 KSI (1034 MPA) TENSILE STRENGTH (17-4) |
MIL A 008862 : A
|
AIRPLANE STRENGTH AND RIGIDITY, LANDING AND GROUND HANDLING LOADS |
MIL S 8784 : B
|
SEALING COMPOUND, LOW ADHESION, FOR REMOVABLE PANELS AND FUEL TANK INSPECTION PLATES |
MIL D 8708 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL W 6858 : D
|
WELDING RESISTANCE, SPOT AND SEAM |
MIL R 9300 : B
|
RESIN, EPOXY, LOW-PRESSURE LAMINATING |
NAS 411 : 0
|
HAZARDOUS MATERIALS MANAGEMENT PROGRAM |
MIL A 008865 : A NOTICE 1
|
AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
SAE AMS 5593 : 2016
|
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 45.5NI - 25.5CR - 3.2CO - 3.2MO - 3.2W - 18.5FE, SOLUTION HEAT TREATED |
MIL B 5087 : B
|
BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
MIL G 81322 : E
|
GREASE, AIRCRAFT, GENERAL PURPOSE, SIDE TEMPERATURE RANGE, NATO CODE NUMBER G-395 |
MIL C 6021 : H NOTICE 1
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
MIL W 6873 : C
|
WELDING FLASH CARBON AND ALLOY STEEL |
MIL F 83142 : A
|
FORGING, TITANIUM ALLOYS, PREMIUM QUALITY |
MIL F 7179 : G
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
MIL A 83444 : 0
|
AIRPLANE DAMAGE TOLERANCE REQUIREMENTS |
MIL A 8860 : B
|
AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
MIL S 7742 : D
|
SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
MIL STD 295 : 0
|
BILL OF MATERIAL, PREPARATION OF |