MIL-M-24041 Revision C:1981
|
MOLDING AND POTTING COMPOUND |
MIL-S-9041 Revision B:1975
|
SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND HONEYCOMB CORE FOR AIRCRAFT STRUCTURAL APPLICATIONS |
SAE AMS 6910 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 8AL - 1MO - 1V, DUPLEX ANNEALED |
SAE AMS A 21180 : 2011
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
SAE AMS S 8802 : 2015
|
SEALING COMPOUND, FUEL RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
SAE AMS 6925 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED |
MIL-STD-1530 Revision D:2016
|
AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
SAE AMS C 27725 : 2016
|
COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES C) |
NAS1514:2011
|
RADIOGRAPHIC STANDARD FOR CLASSIFICATION OF FUSION WELD DISCONTINUITIES |
MIL-STD-129 Revision R:2014
|
Military Marking for Shipment and Storage |
MIL-A-46146 Revision B:1990
|
ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) |
MIL R 25988/4 : 0
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 80 |
SAE AS 29512 : 2016
|
HYDROCARBON FUEL RESISTANT, TUBE FITTING, O-RING MOLDED FROM AMS-P-5315 RUBBER |
SAE AMS 6900 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 5AL - 2.5SN, ANNEALED |
ISO 15614-13:2012
|
Specification and qualification of welding procedures for metallic materials Welding procedure test Part 13: Upset (resistance butt) and flash welding |
SAE AMS 4940 : 2012
|
TITANIUM SHEET, STRIP, AND PLATE COMMERCIALLY PURE ANNEALED, 25.0 KSI (172 MPA) YIELD STRENGTH |
SAE AMS 4915 : 2013
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1V - 1MO SINGLE ANNEALED |
SAE AMS 6932 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V EXTRA LOW INTERSTITIAL, ANNEALED |
SAE AMS 4911 : 2014
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
SAE AS 81550A : 2014
|
INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE |
ASTM B 265 : 2015 : REDLINE
|
Standard Specification for Titanium and Titanium Alloy Strip, Sheet, and Plate |
SAE AMS P 5510 : 2013
|
O-RING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS, TYPE 1 HYDRAULIC (-65 TO 160 DEGREES F) |
SAE AMS 4989 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 3AL - 2.5V, ANNEALED |
SAE AMS 2175 : 2010
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
MIL-DTL-83397 Revision B:2009
|
RUBBER, POLYURETHANE, CASTABLE, HUMIDITY RESISTANT |
SAE AMS R 83285 : 2011
|
RUBBER, ETHYLENE-PROPYLENE, GENERAL PURPOSE |
MIL-PRF-23586 Revision F:1996
|
SEALING COMPOUND (WITH ACCELERATOR), SILICONE RUBBER, ELECTRICAL |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE AMS 2770 : 2015
|
HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS |
SAE AS 28775 : 2013
|
PACKING, PREFORMED, - MS28775 O-RING |
MIL-T-81556 Revision A:1983
|
TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
AWS C3.7M/C3.7 : 2011
|
SPECIFICATION FOR ALUMINUM BRAZING |
SAE AMS C 8073 : 2013
|
CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED GLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS |
SAE AS 3581 : 2012
|
PACKING, PREFORMED - O-RING SEAL AMS 7259 |
SAE AMS 4918 : 2014
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, ANNEALED |
SAE AMS 6921 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED AND AGED |
SAE AMS 7276H : 2011
|
RUBBER: FLUOROCARBON (FKM) HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
SAE AS 3208 : 1976
|
PACKING, PREFORMED - AMS 7276 - SEAL |
AWS C3.6M/C3.6 : 2016
|
SPECIFICATION FOR FURNACE BRAZING |
SAE AMS 4990 : 2015
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED AND AGED |
SAE AMS 4919 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 6AL - 2SN - 4ZR - 2MO - 0.08SI DUPLEX ANNEALED |
SAE AMS 6905 : 2014
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 2.0MO, DUPLEX ANNEALED |
SAE AMS 3216 : 2005
|
ELASTOMER: FLUOROCARBON (FKM) RUBBER HIGH-TEMPERATURE - FLUID RESISTANT LOW COMPRESSION SET 70 TO 80 |
AWS D1.2/D1.2M : 2014
|
STRUCTURAL WELDING CODE - ALUMINUM |
MIL R 25988/1 : A
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 70 |
SAE AMS 4902 : 2013
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY-PURE, ANNEALED 40.0 KSI (276 MPA) YIELD STRENGTH |
SAE AMS 3384 : 2013
|
Rubber, Fluorocarbon Elastomer (FKM) 70 to 80 Hardness, Low Temperature Sealing Tg -22 °F (-30 °C) For Elastomeric Shapes or Parts in Gas Turbine Engine Oil, Fuel and Hydraulic Systems |
SAE AMS 6940 : 2011
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3.0AL - 2.5V, ANNEALED |
SAE AMS A 22771 : 2012
|
ALUMINUM ALLOY FORGINGS, HEAT TREATED |
JSSG-2010 Base Document:1998
|
Crew Systems |
SAE AMS 2759 : 2014
|
HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS |
AWS C3.5M/C3.5 : 2016
|
SPECIFICATION FOR INDUCTION BRAZING |
SAE AMS 2301 : 2015
|
STEEL CLEANLINESS, AIRCRAFT QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE |
SAE AMS P 83461 : 1998
|
Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C) |
SAE AS 568 : 2014
|
AEROSPACE SIZE STANDARD FOR O-RINGS |
MIL-HDBK-275 Revision A:1976
|
GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
SAE AMS 2430 : 2015
|
SHOT PEENING |
SAE AMS 6907 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, DUPLEX ANNEALED |
SAE AMS 6915 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 7.0AL - 4.0MO, ANNEALED |
MIL-STD-889 Revision C:2016
|
DISSIMILAR METALS |
AWS D17.2/D17.2M : 2013
|
SPECIFICATION FOR RESISTANCE WELDING FOR AEROSPACE APPLICATIONS |
MIL R 25988/2 : 0
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 3 |
SAE AMS 4917 : 2012
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11CR - 3.0AL - SOLUTION HEAT TREATED |
SAE AMS 6931 : 2014
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, ANNEALED |
AWS C3.4M/C3.4 : 2016
|
SPECIFICATION FOR TORCH BRAZING |
A-A-59588 Revision B:2012
|
Rubber, Silicone |
MIL-STD-866 Revision C:2007
|
Grinding of Chrome Plated Steel and Steel Parts Heat Treated to 180,000 PSI or Over |
SAE AS 1933 : 2013
|
AGE CONTROLS FOR HOSE CONTAINING AGE-SENSITIVE ELASTOMERIC MATERIAL |
SAE AMS QQ A 367 : 2012
|
ALUMINUM ALLOY FORGINGS |
SAE AMS 2750 : 2012
|
PYROMETRY |
MIL R 25988/3 : 0
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 60 |
SAE AMS 6926 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED AND AGED |
SAE AMS 7287 : 2012
|
FLUOROCARBON ELASTOMER (FKM) HIGH TEMPERATURE/HTS OIL RESISTANT/FUEL RESISTANT LOW COMPRESSION SET/70 TO 80 HARDNESS, LOW TEMPERATURE TG -22 DEGREES F (-30 DEGREES C) FOR SEALS IN OIL/FUEL/SPECIFIC HYDRAULIC SYSTEMS |
SAE AS 83461/2 : 2016
|
STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
SAE AMS 6920 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
SAE AMS 3100 : 2013
|
ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS |
SAE AMS R 7362 : 2012
|
NITRILE RUBBER, SYNTHETIC, SOLID, SHEET, STRIP AND FABRICATED PARTS, SYNTHETIC OIL RESISTANT |
SAE ARP 5316 : 2014
|
STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
SAE AMS 7259 : 2013
|
RUBBER: FLOUROCARBON (FKM), HIGH TEMPERATURE/FLUID RESISTANT, LOW COMPRESSION SET/85 TO 95 HARDNESS, FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
MIL-A-46106 Revision B:1989
|
ADHESIVE-SEALANTS, SILICONE, RTV, ONE-COMPONENT |
SAE AMS 4910 : 2017
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN ANNEALED |
MIL-HDBK-83377 Base Document:1997
|
ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
SAE AMS 4907 : 2013
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6.0AL - 4.0V, EXTRA LOW INTERSTITIAL, ANNEALED |
SAE AMS 2772 : 2016
|
HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
MIL-STD-1568 Revision D:2015
|
Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
SAE AMS 2303 : 2016
|
STEEL CLEANLINESS, AIRCRAFT QUALITY, MARTENSITIC CORROSION-RESISTANT STEELS, MAGNETIC PARTICLE INSPECTION PROCEDURE |
MIL-PRF-83483 Revision E:2014
|
ANTISEIZE THREAD COMPOUND, MOLYBDENUM DISULFIDE-PETROLATUM |
SAE AMS 4921 : 2016
|
TITANIUM BARS, WIRE, FORGINGS, AND RINGS COMMERCIALLY PURE, 70 KSI (483 MPA) YIELD STRENGTH |
SAE AMS 4988 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED |
FED-STD-191 Revision A:1978
|
TEXTILE TEST METHODS |
SAE AMS H 81200 : 2014
|
HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS |
SAE AMS 3218 : 2005
|
ELASTOMER: FLUOROCARBON (FKM) RUBBER HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET 85 TO 95 |
SAE AS 83461/1 : 2016
|
M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
SAE AS 29561 : 2015
|
O-RING, SYNTHETIC LUBRICANT RESISTANT MOLDED FROM AMS-R-7362 RUBBER |
SAE AS 28778 : 2016
|
O-RING, STRAIGHT THREAD TUBE FITTING BOSS MOLDED FROM AMS-P-5510 RUBBER |
SAE AMS 4904 : 2015
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
SAE AMS 4909 : 2016
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
SAE AMS 6906 : 2015
|
TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION HEAT TREATED AND AGED |
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
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) |
SAE AMS F 7190 : 2016
|
FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL-HDBK-838 Base Document:1997
|
LUBRICATION OF MILITARY EQUIPMENT |
A-A-59877 Base Document:2010
|
Insulating Compound, Electrical, Embedding |
MIL-PRF-8516 Revision G:1997
|
SEALING COMPOUND, SYNTHETIC RUBBER, ELECTRIC CONNECTORS AND ELECTRIC SYSTEMS, CHEMICALLY CURED |
SAE AMS 4903 : 2015
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED |
SAE AMS 2300 L : 2015
|
STEEL CLEANLINESS, PREMIUM AIRCRAFT-QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE |
SAE AMS 3856 : 2016
|
CLOTH, UPHOLSTERY, FLAME RESISTANT |
SAE AMS 6930 : 2014
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, SOLUTION HEAT TREATED AND AGED |
SAE AMS 4916 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
SAE AS 3209 : 2013
|
PACKING, PREFORMED - AMS 7276, 'O' RING |
SAE AMS P 5315 : 2013
|
ACRYLONITRILE-BUTADIENE (NBR) RUBBER FOR FUEL-RESISTANT SEALS 60 TO 70 |
AWS D1.1/D1.1M : 2015
|
STRUCTURAL WELDING CODE-STEEL |
MIL-PRF-6855 Revision F:2009
|
RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES, GENERAL SPECIFICATION FOR |
MIL-HDBK-6870 Revision B:2012
|
NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
MIL-DTL-25988 Revision C:2006
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES |
SAE AMS 6936 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6AL - 6V - 2SN, ANNEALED |
SAE AMS 6935 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 6.0V - 2.0SN, SOLUTION HEAT TREATED AND AGED |
MIL-STD-1798 Revision C:2013
|
MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
ASTM E 162 : 2016 : REDLINE
|
Standard Test Method for Surface Flammability of Materials Using a Radiant Heat Energy Source |
SAE AMS C 7438 : 2014
|
CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
AWS D17.1/D17.1M : 2012
|
SPECIFICATION FOR FUSION WELDING FOR AEROSPACE APPLICATIONS |
SAE AMS 6901 : 2015
|
TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
SAE AS 29513 : 2016
|
PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, 'O' RING |
SAE AMS 4901 : 2015
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 70.0 KSI (485 MPA) |
MIL-S-25392 Revision B:1968
|
SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND POLYURETHANE FOAMED-IN-PLACE CORE, FOR AIRCRAFT STRUCTURAL APPLICATIONS |
SAE AMS 4900 : 2014
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 55.0 KSI (379 MPA) YIELD STRENGTH |
SAE AMS 4970 : 2016
|
TITANIUM ALLOY BARS, WIRE, AND FORGINGS 7AL - 4MO SOLUTION AND PRECIPITATION HEAT TREATED |