MIL L 7808 : K (1)
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
Superseded date
02-05-1997
Superseded by
Published date
12-01-2013
Publisher
Sorry this product is not available in your region.
Covers requirements for one type of lubricating oil.
| Committee |
FSC 9150
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| DocumentType |
Standard
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| SAE MA2094 | Test Methods for Tube-Fitting Assemblies, Metric (ISO 10583) |
| MIL C 83383 : C | CIRCUIT BREAKER, REMOTE CONTROL THERMAL, TRIP FREE, GENERAL SPECIFICATION FOR |
| AFGS-87213 Revision B:1993 | DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
| MIL-STD-1216 Base Document:1969 | PREVENTIVE COMPOUNDS, PHOSPHATE COATINGS AND INHIBITORS |
| ASTM F 2161 : 2010 : REDLINE | Standard Guide for Instrument and Precision Bearing Lubricants-Part 1 Oils |
| 01/704905 DC : DRAFT MAR 2001 | PREN 3155-041 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 041 - CONTACTS, ELECTRICAL, COAXIAL, SIZE 12, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| MIL PRF 62548 : A | LEAD, IGNITION |
| SAE MA4098 | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 204 °C, 35 000 kPa Hydraulic and Pneumatic, Metric |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-T-9906 Revision C:1988 | TAPE, IDENTIFICATION, AEROSPACE, VEHICLE TUBING MARKER |
| MIL-S-7124 Revision B:1966 | SEALING COMPOUND, POLYSULFIDE, ACCELERATOR REQUIRED FOR AIRCRAFT STRUCTURES |
| MIL-S-29574 Base Document:1989 | SEALING COMPOUND, POLYTHIOETHER, FOR AIRCRAFT STRUCTURES, FUEL AND HIGH TEMPERATURE RESISTANT, FAST CURING AT AMBIENT AND LOW TEMPERATURE |
| MIL-C-81703 Base Document:1971 | CONNECTOR, ELECTRIC, CIRCULAR, MINIATURE, RACK AND PANEL OR PUSH-PULL COUPLING, ENVIRONMENT RESISTING |
| 00/708806 DC : DRAFT MAY 2000 | PREN 3155-059 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 059: CONTACTS, ELECTRICAL, COAXIAL, SHIELDED, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS R. PRODUCT STANDARD |
| MIL-PRF-29598 Base Document:1996 | FILM, PROTECTIVE, LEADING EDGE (PRESSURE-SENSITIVE) |
| MIL-C-47238 Revision A:1987 | CABLE, ELECTRICAL, SHIELDED AND JACKETED, SPECIAL PURPOSE |
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL C 28840 : A | CONNECTOR ELECTRICAL, CIRCULAR THREADED, HIGH DENSITY, HIGH SHOCK SHIPBOARD, CLASS D - GENERAL SPECIFICATION FOR |
| SAE MA1568A | Nut, Self Locking - UNS S66286, 425°C & 650°C, 1100 MPa, MJ Thread, Procurement Specification For, Metric |
| MIL-T-81714 Revision E:1988 | TERMINAL JUNCTION SYSTEM (TJS), ENVIRONMENT RESISTANT GENERAL SPECIFICATION FOR |
| MIL H 27267 : B | HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE |
| ASTM D 3149 : 2006 | Standard Specification for Crosslinked Polyolefin Heat-Shrinkable Tubing for Electrical Insulation |
| MIL S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| PREN 3372-001 : 200P1 | AEROSPACE SERIES - CONNECTORS, ELECTRICAL, CIRCULAR, MEDIUM AND HIGH CONTACT DENSITY, SCOOP-PROOF WITH BAYONET COUPLING, OPERATING TEMPERATURES -65 DEGREES C TO 175 DEGREES C OR 200 DEGREES C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION |
| MIL-I-38338 Revision D:1991 | INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
| MIL D 87213 : 0 | DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| PREN 3155-060 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 060: CONTACTS, ELECTRICAL, COAXIAL, SIZE 12, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3155-058 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 058: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3218-001 : 200P1 | AEROSPACE SERIES - CONNECTORS, RECTANGULAR, WITH METALLIC SHELLS AND SCREW-LOCKING - PART 001: TECHNICAL SPECIFICATION |
| SAE AS85848A | Sleeving, for Identification Marking, Heat Shrinkable, General Specification for |
| SAE AS 1501 : 1994 | HOSE, AIR DUCT, FLEXIBLE, NONMETALLIC, AIRCRAFT |
| ASTM F 1387 : 1999 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| BS EN 3372-001:2007 | Aerospace series. Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures -65°C to 175°C or 200°C continuous Technical specification |
| BS EN 3155-013:2006 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 8, female, type D, solder, class R. Product standard |
| BS EN 3155-061:2006 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, shielded, size 12, female, type D, solder, class R. Product standard |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL F 83798 : B | FITTING, RUBBER HOSE, LIGHTWEIGHT MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL S 83731 : A | SWITCH, TOGGLE, UNSEALED AND SEALED TOGGLE, GENERAL SPECIFICATION FOR |
| MIL C 38159 : B | CONNECTOR, ELECTRIC, RAMP POWER, 480/277 VOLTS, GENERAL SPECIFICATION FOR |
| MIL-N-52110 Revision F:1982 | NOZZLE, FUEL & OIL SERVICING, NONAUTOMATIC SHUTOFF & NOZZLES, FUEL SERVICING AUTOMATIC SHUTOFF |
| MIL-DTL-22529 Revision D:1996 | GROMMET, EDGING |
| MIL-C-81797 Revision A:1994 | COATING, INORGANICALLY BONDED ALUMINUM (ELECTROPHORECTICALLY DEPOSITED) |
| MIL R 46846 : B | RUBBER, SYNTHETIC, HEAT-SHRINKABLE |
| MIL C 28876 : D | CONNECTORS, FIBER OPTIC, CIRCULAR, PLUG AND RECEPTACLE STYLE, MULTIPLE REMOVABLE TERMINI, GENERAL SPECIFICATION FOR |
| MIL L 46147 : B | LUBRICANT, SOLID FILM, AIR CURED (CORROSION INHIBITING) |
| MIL C 3702 : B | CABLE, POWER, ELECTRICAL, IGNITION, HIGH TENSION |
| MIL-C-81511 Revision F:1992 | CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT ENVIRONMENT RESISTING, AND ACCESSORIES GENERAL SPECIFICATION FOR |
| SAE AS1969 | Coupling Assembly, Self-Sealing, Quick Disconnect Fuel and Oil System Components |
| MIL F 83870 : A | FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
| 00/708805 DC : DRAFT MAY 2000 | PREN 3155-058 - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 058: CONTACTS, ELECTRICAL, COAXIAL, SHIELDED, SIZE 16, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| MIL-C-7413 Revision B:1970 | COUPLING, QUICK DISCONNECT, AUTOMATIC SHUTOFF, GENERAL SPECIFICATION FOR |
| MIL-STD-726 Revision H:1985 | PACKAGING REQUIREMENTS CODE |
| MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
| MIL S 9395/39 : B | SWITCH, PRESSURE, [GAGE] TYPE 11 LOW LEVEL TO 5 AMPERES |
| MIL H 83796 : 0 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| MIL-P-38336 Revision A:1994 | PRIMER COATING, INORGANIC, ZINC DUST PIGMENTED, SELF-CURING, FOR STEEL SURFACES |
| MIL-I-81765 Revision A:1987 | INSULATING COMPONENT, MOLDED, ELECTRICAL, HEAT SHRINKABLE, GENERAL SPECIFICATION FOR |
| MIL-I-17563 Revision C:1992 | IMPREGNANTS FOR ALUMINUM, COPPER, IRON, MAGNESIUM AND ZINC ALLOY CASTINGS |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
| MIL-T-25363 Revision D:1973 | TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-B-85598 Base Document:1988 | BEARINGS, ELASTOMERIC GENERAL SPECIFICATION FOR |
| XP PREN 3660-001 : 1994 XP | AEROSPACE SERIES - CABLE OUTLET ACCESSORIES FOR CIRCULAR AND RECTANGULAR ELECTRICAL AND OPTICAL CONNECTORS - PART 001: TECHNICAL SPECIFICATION |
| MIL-STD-1344 Revision A:1977 | TEST METHODS FOR ELECTRICAL CONNECTORS |
| MIL-B-24781 Base Document:1993 | BATTERBOARD SYSTEMS, SYNTHETIC |
| 01/702542 DC : DRAFT JAN 2001 | PREN 3155-067 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 067: CONTACTS, ELECTRICAL, COAXIAL, SIZE 08, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| MIL-C-24360 Revision A:1969 | CABLE ASSEMBLY, AIRCRAFT AUTONAVIGATOR ALIGNMENT, UMBILICAL |
| SAE MA2007A | Hose Assembly, Tetrafluoroethylene, Lightweight, 204 °C, 21 000 kPa Hydraulic, Metric |
| SAE AMS3625D | Elastomeric Tubing, Electrical Insulation Crosslinked Silicone, Pigmented, Flexible, Heat-Shrinkable 1.750 to 1 Shrink Ratio |
| MIL-I-6869 Revision D:1971 | IMPREGNANTS FOR ALUMINUM ALLOY AND MAGNESIUM ALLOY CASTINGS |
| MIL I 25017 : E | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (METRIC) |
| MIL W 83420 : E | WIRE, ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL |
| MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
| MIL-B-0022227 Revision B:1976 | BEARING, BALL, ANNULAR, GENERATOR AND MOTOR GENERATOR |
| MIL-C-81562 Revision B:1983 | COATING, CADMIUM, TIN CADMIUM AND ZINC (MECHANICALLY DEPOSITED) |
| MIL P 26915 : C | PRIMER COATING, ZINC DUST PIGMENTED, FOR STEEL SURFACES |
| PREN 3567-001 : 200P1 | AEROSPACE SERIES - COUPLERS FOR USE IN MULTIPLEX DATA BUS SYSTEMS IN ACCORDANCE WITH STANAG 3838 - TECHNICAL SPECIFICATION |
| SAE MA2151 | Clamp Assemblies, Saddle or Omega Style, Two Point Mount, Multiple Shapes, Metric |
| ASTM D 3150 : 2011-09 | SPECIFICATION FOR CROSSLINKED AND NONCROSSLINKED POLY(VINYL CHLORIDE) HEAT-SHRINKABLE TUBING FOR ELECTRICAL INSULATION |
| BS EN 2997-1:1997 | Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures 175°C continuous, 200°C continuous, 260°C peak Technical specification |
| SAEITC TS156-2 | TS156 Performance Specification for Insert Salvage Metric Thinwall Screw Locking, Inconel 718 Silver Coated |
| SAEITC TS149-2 | TS149 Technical Specification for All Metal Self-Locking Nuts (UNJ Threads) 1550 MPa (225,000 lbf/in²) Minimum Tensile Strength at Ambient Temperature |
| SAEITC TS153-2 | TS153 Performance Specification of Insert Salvage, Imperial, Thinwall Screw Locking, Inconel 718 Silver Coated |
| MIL-C-83982 Base Document:1974 | COMPOUND, SEALING, FLUID RESISTANT |
| MIL-C-22751 Revision D:1971 | COATING SYSTEM, EPOXY-POLYAMIDE, CHEMICAL AND SOLVENT RESISTANT, PROCESS FOR APPLICATION OF |
| MIL I 23053 : D | INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE MODIFIED FLUOROPOLYMER, CROSSLINKED |
| MIL-C-27725 Revision B:1969 | COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS |
| MIL-L-50096 Revision A:1963 | LABORATORY, PETROLEUM, BASE |
| 01/702543 DC : 0 | PREN 3155-068 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 068: CONTACTS, ELECTRICAL, COAXIAL, SIZE 08, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| SAE AMST81914A | Tubing, Plastic, Flexible, Convoluted, Conduit, General Specification For |
| 01/704903 DC : DRAFT MAR 2001 | PREN 3155-039 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 039: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| MIL S 8805/43 : G | SWITCH, SENSITIVE, PLUNGER, 7 AMPERES RESILIENT SEAL, FLUID RESISTANT |
| MIL S 8805/48 : F | SWITCH, SENSITIVE, ROLLER LEVER, SELF RETURN, RESILIENT SEAL, FLUID RESISTANT |
| 01/702544 DC : 0 | PREN 3155-069 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 069: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS P - PRODUCT STANDARD |
| ASTM B 635 : 2000 : R2004 : EDT 1 | Standard Specification for Coatings of Cadmium-Tin Mechanically Deposited |
| SAE MA620 | Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft Metric |
| SAE AS13441 | Test Methods for Electrical Connectors |
| L-T-100 Revision B:1988 | TAPE, PRESSURE-SENSITIVE ADHESIVE, POLYESTER FILM |
| MIL F 83296 : 0 | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC) |
| MIL-C-81751 Revision B:1972 | Coating, Metallic-Ceramic |
| XP PREN 3567-001 : 1993 XP | AEROSPACE SERIES - COUPLERS FOR USE IN MULTIPLEX DATA BUS SYSTEMS IN ACCORDANCE WITH STANAG 3838 - PART 001: TECHNICAL SPECIFICATION |
| MIL C 25516 : D | CONNECTOR, ELECTRICAL, MINIATURE, COAXIAL, ENVIRONMENT RESISTANT TYPE, GENERAL SPECIFICATION FOR |
| MIL-B-81820 Revision F:1994 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION, GENERAL SPECIFICATION FOR |
| MIL-P-46111 Revision C:1978 | PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
| MIL-C-81907 Base Document:1972 | COATING SYSTEM, POLYURETHANE, ALIPHATIC, WEATHER RESISTANT, PROCESS FOR APPLICATION OF |
| MIL-B-8942 Revision A:1965 | Bearings, Plain, TFE Lined, Self-Aligning |
| MIL-A-81801 Revision A:1994 | ANODIC COATINGS FOR ZINC AND ZINC ALLOYS |
| 91/83289 DC : DRAFT DEC 1991 | PREN 3624 - AEROSPACE SERIES - POLYSULPHIDE SEALANTS, TWO-COMPONENT - TECHNICAL SPECIFICATION |
| MIL-T-81914 Base Document:1973 | TUBING, PLASTIC, FLEXIBLE, CONVOLUTED, CONDUIT, GENERAL SPECIFICATION FOR |
| MIL-B-81819 Revision B:1987 | BEARING, PLAIN, (SLIDING SPHERICAL, SLEEVE & THRUST) SELF LUBRICATING, HIGH SPEED OSCILLATION, GENERAL SPECIFICATION FOR |
| MIL S 3950 : F | SWITCH, TOGGLE ENVIRONMENTALLY SEALED, GENERAL SPECIFICATION FOR |
| SAE AMSDTL23053 | Insulation Sleeving, Electrical, Heat Shrinkable, General Specification For |
| PREN 6047-001 : 200P1 | AEROSPACE SERIES - CONNECTORS, ELECTRICAL, CIRCULAR, COUPLED BY THREADED RING, FOR HIGH CURRENT OPERATING TEMPERATURE +200 DEGREE C CONTINUOUS, AND FIRE RESISTANT - TECHNICAL SPECIFICATION |
| SAE AS8796 | Hose, Air Duct, Flexible, Aircraft |
| ASTM D 3144 : 2000 : R2006 | Standard Specification for Crosslinked Poly(Vinylidene Fluoride) Heat-Shrinkable Tubing for Electrical Insulation |
| SAE AS4726A | Nuts, Self-Locking, UNS S66286 Classification: 220 ksi/850 °F Procurement Specification |
| ASTM D 3149 : 2006 : R2013 | Standard Specification for Crosslinked Polyolefin Heat-Shrinkable Tubing for Electrical Insulation (Withdrawn 2020) |
| EN 3567-001:2001 | Aerospace series - In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B - Part 001: Technical specification |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| BS ISO 8829-2:2006 | Aerospace. Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Non-metallic braid |
| 01/704904 DC : DRAFT MAR 2001 | PREN 3155-040 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 040 - CONTACTS, ELECTRICAL, COAXIAL, SIZE 12, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| MIL-B-85560 Base Document:1983 | BEARING, FIBER REINFORCED PLASTIC, SLEEVE, PLAIN AND FLANGED, SELF LUBRICATING GENERAL SPECIFICATION FOR |
| BWB TL 4330-0020 : 1ED 1996 | FILTER ELEMENT |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL-C-8956 Revision A:1970 | CLAMP, LOOP TUBE SUPPORT |
| MIL-D-8181 Revision B:1965 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-G-83380 Base Document:1979 | GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
| MIL-E-5607 Revision F:1983 | ENGINE, GAS TURBINE, PREPARATION FOR STORAGE AND SHIPMENT OF, PROCESS FOR |
| MIL C 8188 : C | CORROSION PREVENTIVE OIL, GAS TURBINE ENGINE, AIRCRAFT SYNTHETIC BASE |
| SAE AS85080A | Insulation Sleeving, Electrical, Shrinkable Without Heat, General Specification For |
| MIL L 62548 : 1987 | LEAD, IGNITION |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL W 25038 : F | WIRE, ELECTRICAL, HIGH TEMP, FIRE RESISTANT, AND FLIGHT CRITICAL, GENERAL SPECIFICATION FOR |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| MIL-S-38399 Revision A:1975 | STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
| MIL-DTL-23053 Revision E:1996 | INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE, GENERAL SPECIFICATION FOR |
| MIL D 22706 : F | DUCT AND SCUFF COVER, PNEUMATIC, FLEXIBLE |
| MIL B 83054 : B | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| MIL-I-47049 Base Document:1974 | INSULATION TUBING, SILICONE RUBBER, HEAT SHRINKABLE |
| PREN 4067-001 : 200P2 | AEROSPACE SERIES - CONNECTORS, ELECTRICAL, CIRCULAR, SCOOP-PROOF, COUPLED BY THREADED RING, FIRE-RESISTANT, OPERATING TEMPERATURE 260 DEGREES C PEAK - TECHNICAL SPECIFICATION |
| MIL A 25676 : D | ADAPTOR, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT |
| ASTM B 635 : 2000 : R2009 | Standard Specification for Coatings of Cadmium-Tin Mechanically Deposited |
| SAE AS1371A | Nuts, Self-Locking, Corrosion Resistant Steel High Strength, Prevailing Torque, All Metal 800°F (427°C) Use, UNJ Thread Form |
| SAE AMSR83485A | Rubber, Fluorocarbon Elastomer, Improved Perfrormance At Low Temperatures |
| PREN 3155-059 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 059: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| SAE AS81765A | Insulating Components, Molded, Electrical, Heat Shrinkable, General Specification For |
| SAE AS4098A | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 400 °F, 5000 psi Hydraulic and Pneumatic |
| ISO 8829-2:2006 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid |
| ASTM F 1387 : 1999 : R2012 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| ASTM D 3144 : 2000 : R2013 : EDT 1 | Standard Specification for Crosslinked Poly(Vinylidene Fluoride) Heat-Shrinkable Tubing for Electrical Insulation |
| ASTM D 3144 :2000 | Standard Specification for Crosslinked Poly(Vinylidene Fluoride) Heat-Shrinkable Tubing for Electrical Insulation |
| ASTM F 1387 : 1999 : R2005 | Standard Specification for Performance of Piping and Tubing Mechanically Attached Fittings |
| ASTM D 2903 : 2011-09 | SPECIFICATION FOR CROSSLINKED CHLORINATED POLYOLEFIN HEAT-SHRINKABLE TUBING FOR ELECTRICAL INSULATION |
| BS EN 3155-059:2006 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, size 16, female, type D, solder, class R. Product standard |
| BS EN 2350:1991 | Circuit breakers. Technical specification |
| BS EN 3567-001:2001 | Aerospace series. In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B Technical specification |
| BS EN 3155-012:2006 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, triaxial, size 8, male, type D, solder, class R. Product standard |
| BS EN 3155-060:2006 | Aerospace series. Electrical contacts used in elements of connection Contacts, electrical, coaxial, shielded, size 12, male, type D, solder, class R. Product standard |
| EN 3372-001:2007 | Aerospace series - Connectors, electrical, circular, medium and high contact density, scoop-proof with bayonet coupling, operating temperatures - 65 °C to 175 °C or 200 °C continuous - Part 001: Technical specification |
| EN 3155-013:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 013: Contacts, electrical, triaxial, size 8, female, type D, solder, class R - Product standard |
| EN 3155-012:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 012: Contacts, electrical, triaxial, size 8, male, type D, solder, class R - Product standard |
| EN 3155-059:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 059: Contacts, electrical, coaxial, size 16, female, type D, solder, class R Product standard |
| EN 3155-060:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 060: Contacts, electrical, coaxial, size 12, male, type D, solder, class R Product standard |
| EN 2350:1990 | Aerospace series - Circuit breakers - Technical specification |
| EN 3155-061:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 061: Contacts, electrical, coaxial, size 12, female, type D, solder, class R Product standard |
| MIL-B-81934 Revision B:1991 | BEARING, SLEEVE, PLAIN AND FLANGED, SELF LUBRICATING |
| MIL-DTL-22706 Revision G:1997 | DUCT AND SCUFF COVER, PNEUMATIC, FLEXIBLE |
| DIN 65054:1989-06 | AEROSPACE; PRESSURE SENSITIVE ADHESIVE FILMS FOR MARKING; TECHNICAL SPECIFICATION |
| MIL H 83298 : A | HOSE, TETRAFLUOROETHYLENE, HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC |
| MIL-B-8943 Revision A:1966 | BEARINGS, JOURNAL - PLAIN AND FLANGED, TFE-LINED |
| DOD-STD-35-121 Base Document:1978 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, EYELETS, FERRULES, AND GROMMETS |
| MIL G 38195 : G | GENERATOR SET, GAS TURBINE ENGINE 60 KW 400 HERTZ, GENERAL PURPOSE |
| MIL-R-83485 Base Document:1976 | RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES |
| MIL-W-7072 Revision B:1962 | WIRE, ELECTRIC 600 VOLT, ALUMINUM, AIRCRAFT GENERAL SPECIFICATION FOR [ASG] |
| MIL-T-7928 Revision G:1976 | TERMINAL, LUG SPLICES, CONDUCTOR, CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR |
| GGG-W-657 Revision C:1970 | WRENCH, SOCKET (SPIN TYPE, SCREWDRIVER GRIP) |
| MIL-D-26124 Revision B:1977 | DUCT AND DUCT ASSEMBLY, PNEUMATIC, FLEXIBLE |
| MIL T 25435 : B | TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL R 3043 : B | RESIN COATING, UNPIGMENTED FOR ENGINE COMPONENTS AND METAL PARTS |
| MIL G 9398 : C | GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT |
| MIL-S-83519 Revision A:1984 | SPLICE, SHIELD TERMINATION, SOLDER STYLE, INSULATION, HEAT SHRINKABLE, ENVIRONMENT RESISTANT, GENERAL SPECIFICATION FOR |
| MIL G 22529 : B NOTICE 1 | GROMMET, PLASTIC |
| MIL C 25955 : 0 | CONNECTOR, ELECTRICAL, ENVIRONMENT RESISTING MINIATURE, WITH SNAP-IN CONTACTS |
| 00/707786 DC : 0 | PREN 4165-001 - AEROSPACE SERIES - CONNECTORS, ELECTRICAL, RECTANGULAR, MODULAR - OPERATING TEMPERATURES 175 DEGREES C CONTINUOUS - PART 001: TECHNICAL SPECIFICATION |
| SAE AMS3593B | Tubing, Plastic, Electrical Insulation Irradiated Polyvinylidene Fluoride, Semi-Rigid, Heat-Shrinkable Marker Sleeving Grade Low Outgassing |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| SAE AS4388 | Hose Assembly PTFE Heavy Duty, -65 To 400 °F (-55 To 204 °C) 8000 psi (56 000 kPa) Hydraulic and Pneumatic |
| SAE MA2150 | Clamps, Loop or P Style, Single Point Mount, Multiple Shapes, Metric |
| PREN 3155-012 : 200P2 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 012: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3155-013 : 200P2 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 013: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3155-061 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 061: CONTACTS, ELECTRICAL, COAXIAL, SIZE 12, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3716-001 : 200P1 | AEROSPACE SERIES - CONNECTOR, SINGLE-WAY, WITH TRIAXIAL INTERFACE, FOR TRANSMISSION OF DIGITAL DATA - PART 001: TECHNICAL SPECIFICATION |
| ASTM B 635 : 2000 | Standard Specification for Coatings of Cadmium-Tin Mechanically Deposited |
| SAE AMSC81562A | Coatings, Cadmium, Tin-Cadmium and Zinc (Mechanically Deposited) |
| SAE MA2079 | Hose Assembly, Convoluted Polytetrafluoroethylene, High Temperature, Medium Pressure, Aircraft, Metric |
| SAE MA1943A | Nuts, Self-Locking, UNS N07001 730°C, 1100 MPa, and 1210 MPa Procurement Specification For, Metric |
| ASTM B 635 : 2000 : R2015 | Standard Specification for Coatings of Cadmium-Tin Mechanically Deposited |
| ASTM D 543 : 2014 : REDLINE | Standard Practices for Evaluating the Resistance of Plastics to Chemical Reagents |
| I.S. EN 2350:1991 | AEROSPACE SERIES - CIRCUIT BREAKERS - TECHNICAL SPECIFICATION |
| ASTM E 1 : 2014 : REDLINE | Standard Specification for ASTM Liquid-in-Glass Thermometers |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| MIL-STD-290 Revision H:2013 | PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS |
| MIL-L-27502 Base Document:1972 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, ESTER BASE |
| SAE AMS5544K | Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted, Annealed |
| ASTM D 2934 : 1989 | Method of Testing for Compatibility of Vulcanized Rubber Seals--Compatibility with Service Fluids (Withdrawn 1993) |
| MIL-S-13282 Revision B:1973 | SILVER AND SILVER ALLOYS |
| ANSI/NCSL Z540 1 : 94(R2002) | CALIBRATION - CALIBRATION LABORATORIES AND MEASURING AND TEST EQUIPMENT - GENERAL REQUIREMENTS |
| SAE AMS4616F | Silicon Bronze Bars, Rods, Forgings, and Tubing 92Cu - 3.2Si - 2.8Zn - 1.5Fe Stress Relieved |
| SAE AMS6490H | Steel Bars, Forgings, and Tubing 4.0Cr - 4.2Mo - 1.0V (0.77 - 0.85C) (M-50) Premium Aircraft-Quality for Bearing Applications Consumable Electrode Vacuum Melted |
| ASTM D 972 : 2016 : REDLINE | Standard Test Method for Evaporation Loss of Lubricating Greases and Oils |
| SAE AMS4908G | Titanium Alloy Sheet and Strip 8mn Annealed, 110 Ksi (760 Mpa) Yield Strength |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| MIL C 8188 : C | CORROSION PREVENTIVE OIL, GAS TURBINE ENGINE, AIRCRAFT SYNTHETIC BASE |
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