MIL-I-81550 Revision C:1983
|
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 Revision C:1981
|
MOLDING AND POTTING COMPOUND |
MIL-R-9299 Revision C:1968
|
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 Revision D:2016
|
AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
MIL A 8892 : 0
|
AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
MIL-A-46146 Revision B:1990
|
ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) |
QQ-P-35 Revision C:1988
|
PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL |
MIL A 8893 : 0
|
AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE |
MIL-A-8863 Revision C:1993
|
AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
MIL-M-46062 Revision C:1985
|
MAGNESIUM ALLOY CASTINGS, HIGH STRENGTH |
MIL-STD-2066 Base Document:1981
|
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 Revision E:1980
|
ALUMINUM ALLOY, BAR, ROD, SHAPES, STRUCTURAL SHAPES, TUBE AND WIRE, EXTRUDED, GENERAL SPECIFICATION FOR |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL-T-81556 Revision A:1983
|
TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
MIL-T-81259 Revision B:1991
|
TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR |
MIL-H-6875 Revision H:1989
|
HEAT TREATMENT OF STEEL RAW MATERIALS |
MIL-A-22771 Revision D:1984
|
ALUMINUM ALLOY FORGINGS, HEAT TREATED |
MIL B 85110 : A
|
BAR, REPEATABLE RELEASE HOLDBACK, AIRCRAFT LAUNCHING, GENERAL DESIGN REQUIREMENTS FOR |
MIL-G-25871 Revision B:1978
|
GLASS, LAMINATED, AIRCRAFT GLAZING |
MIL-STD-5400 Base Document:1992
|
ELECTRONIC EQUIPMENT, AIRBORNE, GENERAL REQUIREMENTS FOR |
ASTM G 85 : 2011 : REDLINE
|
Standard Practice for Modified Salt Spray (Fog) Testing |
MIL-S-8802 Revision F:1990
|
SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION |
MIL A 008861 : A
|
|
MIL-E-6051 Revision D:1967
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
MIL-A-8870 Revision C:1993
|
AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
MIL-STD-45662 Revision A:1988
|
CALIBRATION SYSTEMS REQUIREMENTS |
QQ-C-390 Revision B:1983
|
COPPER ALLOY CASTINGS (INCLUDING CAST BAR) |
MIL S 5002 : D
|
SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
QQ-A-367 Revision H:1973
|
ALUMINUM ALLOY FORGINGS |
MIL-G-5485 Revision D:1993
|
GLASS; LAMINATED, FLAT, BULLET RESISTANT |
ASME B46.1 : 2009
|
SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
MIL-T-9046 Revision J:1983
|
TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE |
MIL-STD-2175 Revision A:1993
|
CASTING, CLASSIFICATION AND INSPECTION OF |
MIL-HDBK-275 Revision A:1976
|
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 Revision C:2016
|
DISSIMILAR METALS |
MIL-STD-866 Revision C:2007
|
Grinding of Chrome Plated Steel and Steel Parts Heat Treated to 180,000 PSI or Over |
MIL-P-9400 Revision C:1991
|
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 Revision B:1985
|
FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL-STD-838 Revision C:1983
|
LUBRICATION OF MILITARY EQUIPMENT |
MIL-STD-1595 Revision A:1982
|
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 Revision A:1978
|
FASTENER SYSTEMS FOR AEROSPACE APPLICATION |
MIL S 8516 : F
|
SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
MIL-L-22589 Revision D:1991
|
LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT |
MIL-STD-1757 Revision A:1983
|
LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE |
MIL-STD-2219 Revision A:2005
|
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 Revision D:2015
|
MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
MIL-STD-1587 Revision D:2017
|
MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
MIL-STD-2000 Revision A:1991
|
STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES |
ASTM E 390 : 2015 : REDLINE
|
Standard Reference Radiographs for Steel Fusion Welds |
MIL-B-7883 Revision B:1968
|
BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS |
MIL-S-8879 Revision C:1991
|
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 Revision A:1971
|
AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS |
MIL-M-38795 Revision B:1982
|
MANUAL, TECHNICAL, SYSTEM PECULIAR CORROSION CONTROL PREPARATION OF. |
MIL S 23586 : E
|
SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED |
MIL-T-29586 Base Document:1991
|
THERMOSETTING POLYMER MATRIX, UNIDIRECTIONAL CARBON FIBER REINFORCED PREPREG TAPE (WIDTHS UP TO 60 INCHES), GENERAL SPECIFICATION FOR |
MS33522 Revision C:1984
|
RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED AND FRICTION RETAINER SPINDLE, (RELIABILITY MAINTAINABILITY) DESIGN AND CONSTRUCTION REQUIREMENTS |
MIL-A-21180 Revision D:1984
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
MIL-T-83399 Base Document:1972
|
TEST FOR REMOVAL OF FLUX RESIDUES |
MIL S 81733 : C
|
SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
MIL-A-8866 Revision C:1987
|
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
MIL-S-29574 Base Document:1989
|
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 Base Document:1980
|
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 Revision B:1971
|
SEALING COMPOUND, LOW ADHESION, FOR REMOVABLE PANELS AND FUEL TANK INSPECTION PLATES |
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL-W-6858 Revision D:1978
|
WELDING RESISTANCE, SPOT AND SEAM |
MIL-R-9300 Revision B:1968
|
RESIN, EPOXY, LOW-PRESSURE LAMINATING |
NAS411:2013
|
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 Revision B:1964
|
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 Revision C:1991
|
WELDING FLASH CARBON AND ALLOY STEEL |
MIL-F-83142 Revision A:1969
|
FORGING, TITANIUM ALLOYS, PREMIUM QUALITY |
MIL-F-7179 Revision G:1993
|
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
MIL A 83444 : 0
|
AIRPLANE DAMAGE TOLERANCE REQUIREMENTS |
MIL-A-8860 Revision B:1987
|
AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
MIL-S-7742 Revision D:1991
|
SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
MIL-STD-295 Base Document:1956
|
BILL OF MATERIAL, PREPARATION OF |