MIL BULL 343 : A
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DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
Withdrawn date
23-07-2013
Publisher
Sorry this product is not available in your region.
Covers documents applicable to aircraft engines and propellers.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
| MS33509 Revision A:1953 | Adapter Installation - Type XII Or XVI Drive Starter Jaw |
| SAE AMS5689F | Steel, Corrosion and Heat Resistant, Wire 18Cr - 10.5Ni - 0.40Ti (SAE 30321) Solution Heat Treated |
| SAE AS963B | DRIVE-STUDDED, ACCESSORY, (127) 5.000 BC ROUND, DESIGN STANDARD FOR |
| SAE ARP755D | Aircraft Propulsion System Performance Station Designation and Nomenclature |
| WW-H-1053 Revision A:1987 | HOSE, METAL (FLEXIBLE, ALUMINUM ALLOY, CORROSION RESISTANT AND HEAT RESISTANT STEEL) |
| AND10050 Revision 21:2005 | BOSSES, STRAIGHT DIMENSIONS FOR GASKET SEAL STRAIGHT THREAD |
| MIL-M-45202 Revision C:1981 | MAGNESIUM ALLOY, ANODIC TREATMENT OF |
| MIL C 16173 : E | CORROSION PREVENTIVE COMPOUND, SOLVENT CUTBACK, COLD APPLICATION |
| MIL-E-25109 Base Document:1955 | ENGINES, AIRCRAFT, RECIPROCATING, GENERAL SPECIFICATION FOR |
| SAE ARP373C | Propeller Shaft Torque Ratings |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR |
| MIL P 6074 : A | PRESERVATION, PACKAGING AND PACKING OF PROPELLERS, PROPELLER SPARES AND PROPELLER ACCESSORIES |
| MS33787 Revision D:1984 | WRENCHING ELEMENT, EXTERNAL SPLINE, DIMENSIONS FOR |
| MIL I 27686 : F | INHIBITOR, ICING, FUEL SYSTEM |
| SAE AS127D | PROPELLER SHAFT END, FLANGED TYPE - NO. 1, 2, 3, 4, 5, & 6 |
| SAE AS848 | ATTACHMENT POINTS, ENGINE, REMOTE TRIMMING MAIN FUEL CONTROL |
| MIL-E-5607 Revision F:1983 | ENGINE, GAS TURBINE, PREPARATION FOR STORAGE AND SHIPMENT OF, PROCESS FOR |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL-A-25175 Revision C:1976 | AIR TRANSPORT, NONTACTICAL, PACKING FOR |
| MIL-STD-280 Revision A:1969 | DEFINITIONS OF ITEM LEVELS, ITEM EXCHANGEABILITY, MODELS, AND RELATED TERMS |
| O-A-548 Revision D:1974 | ANTIFREEZE COOLANT, ENGINE, ETHYLENE GLYCOL, INHIBITED, CONCENTRATED |
| MIL C 3702 : B | CABLE, POWER, ELECTRICAL, IGNITION, HIGH TENSION |
| MS9826 Revision B:2007 | CLAMP, LOOP-CUSHIONED, JOGGLED, CORROSION RESISTANT STEEL, .265 HOLE |
| SAE AMS2645K | FLUORESCENT PENETRANT INSPECTION |
| MIL-I-8599 Revision B:1975 | INSTALLATION OF RECIPROCATING ENGINE INDUCTION AIR FILTERS, DESIGN REQUIREMENTS FOR |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MS33786 Revision B:2013 | Fitting, Installation, Flared Tube and Hose, Swivel |
| AND20002 Revision 3:1953 | DRIVE - TYPE 12 ENGINE ACCESSORY |
| MIL-T-6736 Revision B:1965 | TUBING, CHROME MOLYBDENUM 4130 STEEL, SEAMLESS, AIRCRAFT QUALITY [ASG] |
| SAE ARP1179D | Aircraft Gas Turbine Engine Exhaust Smoke Measurement |
| SAE AS 972 : 1977 | SPLINE DETAILS, ACCESSORY DRIVES AND FLANGES |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MS3325 Base Document:1968 | DRIVE PAD-ACCESSORY, 2.653 BC SQUARE, DESIGN STANDARD FOR |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-P-26366 Revision A:1962 | PROPELLER SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MS9139 Base Document:1965 | GASKET TYPE XVI, XVII-C, -D, -E, AND -F, ENGINE ACCESSORY DRIVE |
| MIL-P-7105 Revision B:1965 | PIPE THREADS, TAPER, AERONAUTICAL NATIONAL FORM, SYMBOL ANPT. GENERAL REQUIREMENTS FOR |
| MIL-P-149 Revision D:1984 | PLASTIC COATING COMPOUND, STRIPPABLE [HOT DIPPING] |
| MS33658 Revision A:1959 | FITTING END, HOSE CONNECTION, STANDARD DIMENSIONS FOR |
| AND20000 : REV 4 | DRIVE - TYPE X ENGINE ACCESSORY |
| MIL-D-3464 Revision E:1987 | DESICCANTS, ACTIVATED, BAGGED, PACKAGING USE AND STATIC DEHUMIDIFICATION |
| MS28034 Revision B:2007 | BULBS, TEMPERATURE, ELECTRICAL RESISTANCE (-70 DEGREES C TO +300 DEGREES C) |
| MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION |
| MIL HDBK 106 : 0 | MULTI LEVEL CONTINUOUS SAMPLING PROCEDURES AND TABLE FOR INSPECTION BY ATTRIBUTES (HANDBOOK H 106) |
| MIL H 27267 : B | HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE |
| MS9136 Base Document:1965 | GASKET TYPE XII, XIV-A, XIV-B, XIV-E, XVII-A AND XVII-B ENGINE ACCESSORY DRIVE |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| MS20002 Revision E:1972 | WASHER, COUNTERSUNK AND PLAIN, HIGH STRENGTH |
| MS8009 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLANGE-TO-FLANGE |
| MIL-C-5040 Revision H:1994 | Cord, Fibrous, Nylon |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MS8002 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLANGE |
| MIL-M-3171 Revision C:1966 | MAGNESIUM ALLOY PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION |
| MIL-T-8808 Revision B:1981 | TUBING, STEEL, CORROSION RESISTANT (18.8 STABILIZED) AIRCRAFT HYDRAULIC QUALITY |
| MIL-B-26195 Revision C:1987 | BOXES, WOOD CLEATED, SKIDDED, LOAD BEARING BASE |
| MIL-STD-480 Revision B:1988 | CONFIGURATION CONTROL - ENGINEERING CHANGES, DEVIATIONS AND WAIVERS |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC) |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| MS9138 Base Document:1965 | GASKET TYPE XIV-C AND XIV-D ENGINE ACCESSORY DRIVE |
| MS8004 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLANGE-TO-FLANGE |
| RR-C-271 Revision G:2016 | CHAINS AND ATTACHMENTS, CARBON AND ALLOY STEEL |
| SAE AMS5643U | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution Heat Treated, Precipitation Hardenable |
| MIL-V-5635 Revision A:1966 | VIBRATOR, IGNITION COIL AIRCRAFT ENGINE STARTING, TYPE AN4181 |
| MS5011 Revision A:1981 | NUT-PROPELLER HUB RETAINING (NON CONTROLLABLE TYPE) |
| SAE AMS5743J | Steel, Corrosion and Heat-Resistant, Bars and Forgings 15.5Cr - 4.5Ni - 2.9Mo - 0.10N Solution Heat Treated, Sub-Zero Cooled, Equalized, and Over-Tempered |
| MIL STD 473 : LATEST | MAINTAINABILITY VERIFICATION/DEMONSTRATION/EVALUATION FOR AERONAUTICAL SYSTEMS |
| MIL STD 1557 : A NOTICE 3 | DESIGNATION OF AIRCRAFT PROPULSION RECIPROCATING ENGINES |
| MIL-S-8503 Revision B:1978 | STEEL BARS, CHROME-VANADIUM (6150) AIRCRAFT QUALITY |
| MS 27423 : A | PROTECTOR PROPELLER SHAFT, PLASTIC |
| MS9135 Base Document:1965 | GASKET, TYPE XI ENGINE ACCESSORY DRIVE |
| MS9137 Base Document:1965 | GASKET TYPE XIII ENGINE ACCESSORY DRIVE |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
| MS3326 Base Document:1968 | DRIVE PAD - ACCESSORY, 5,000 BC SQUARE, DESIGN STANDARD FOR |
| MIL-C-5545 Revision C:1983 | CORROSION PREVENTIVE, AIRCRAFT ENGINE, HEAVY OIL TYPE |
| MIL-C-6529 Revision C:1958 | CORROSION PREVENTIVE, AIRCRAFT ENGINE |
| SAE AS959B | Drive - Studded, Accessory, 2.653 B.C. Square, Design Standard For |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| QQ-W-423 Revision B:1969 | FEDERAL SPECIFICATION - WIRE, STEEL, CORROSION RESISTING |
| MS9006 Revision C:1963 | RECESSES-CROSS, LOW TORQUE DRIVE, DIMENSIONS AND GAGE DIMENSIONS FOR |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| SAE ARP1153A | Method for Determining Relative Specific Gravity Polytetrafluoroethylene Tubing |
| 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 |
| MS3329 Revision A:1969 | DRIVE PAD - ACCESSORY, 10,000 BC ROUND, DESIGN STANDARD FOR |
| MS8000 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE |
| MS3328 Revision A:1969 | DRIVE PAD - ACCESSORY, 8,000 BC ROUND, DESIGN STANDARD FOR |
| MIL-D-70327 Base Document:1959 | DRAWINGS, ENGINEERING AND ASSOCIATED LISTS |
| SAE ARP1256D | Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines |
| SAE AS291F | Surface Texture, Roughness, Waviness and Lay |
| MIL-L-8937 Revision D:1982 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, [NATO CODE NUMBER S 1738] |
| MS51938 Revision C:1991 | SEAL, METALLIC, LEAD & WIRE |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| MS33678 Revision A:2004 | CONNECTOR, RECEPTACLE, ELECTRICAL, INTEGRAL MOUNTING |
| MS8005 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE |
| MIL-STD-1529 Base Document:1955 | VENDOR SUBSTANTABLE FOR AEROSPACE PROPULSION SYSTEM ITEMS |
| AND10065 Revision 2:1946 | CONNECTION ASSEMBLY - FLEXIBLE, FLUID, STANDARD DESIGN OF |
| MIL B 121 : F | BARRIER MATERIAL, GREASEPROOFED, WATERPROOFED, FLEXIBLE |
| TT-E-527 Revision D:1988 | ENAMEL, ALKYD, LUSTERLESS, LOW VOC CONTENT |
| SAE ARP 492 : 2014 | AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST |
| MIL E 5009 : D | |
| MIL T 6735 : A | TUBING, CHROME-MOLYBDENUM, 4135 STEEL, SEAMLESS AIRCRAFT QUALITY |
| MIL-T-5021 Revision D:1969 | MILITARY SPECIFICATION. TESTS; AIRCRAFT AND MISSILE WELDING OPERATORS' QUALIFICATION |
| PPP-T-60 Revision E:1986 | TAPE, PACKAGING, WATERPROOF |
| MIL C 7024 : D | CALIBRATING FLUID, AIRCRAFT FUEL SYSTEM COMPONENTS |
| AND20004 : NOTICE 1 | DRIVE - TYPE XIV ENGINE ACCESSORY |
| MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| SAE AS961B | Drive - Studded, Accessory, 5.000 B.C. Square, Design Standard For |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) |
| MIL-STD-453 Revision C:1984 | INSPECTION, RADIOGRAPHIC |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| SAE AS870E | WRENCHING CONFIGURATION, BI-HEXAGONAL (12 POINT) DRIVE, DESIGN STANDARD FOR |
| SAE AS 970 : 1993 | DRIVE - ACCESSORY, 8.000 BC ROUND, QAD, DESIGN STANDARD FOR |
| SAE AS 967 : 1993 | DRIVE - STUDDED, ACCESSORY, 10.000 BC ROUND, DESIGN STANDARD FOR |
| MS5007 Revision A:1981 | CONE, PROPELLER HUB, FRONT |
| TT-T-548 Revision F:1991 | TOLUENE, TECHNICAL |
| MS8007 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLANGE |
| MS27379 Revision A:1969 | ADAPTER, FLUID TANK FILLER |
| MS33588 Revision E:1984 | NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
| MIL-E-8593 Revision A:1975 | ENGINE, AIRCRAFT, TURBOPROP, GENERAL SPECIFICATION FOR [ASG] |
| TT-S-735 Revision A:1988 | STANDARD TEST FLUIDS, HYDROCARBON |
| MIL-S-7886 Revision B:1962 | SPARK PLUG, SHIELDED, AIRCRAFT RECIPROCATING ENGINE, GENERAL SPECIFICATION FOR |
| AND10152 Revision 3:1953 | SHAFT ENDS - PROPELLER |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK |
| VV-P-236 Revision A:1977 | PETROLATUM, TECHNICAL |
| MIL L 6081 : C | LUBRICATING OIL, JET ENGINE |
| MIL-S-5626 Revision C:1968 | STEEL, CHROME MOLYBDENUM [4140] BARS, RODS, AND FORGING STOCK FOR AIRCRAFT APPLICATION |
| MIL-G-5572 Revision F:1969 | GASOLINE, AVIATION, GRADES 80/87, 100/130, 115/145 |
| SAE AS 969 : 1993 | DRIVE - ACCESSORY, 8.000 BC ROUND, QAD, DESIGN STANDARD FOR |
| MS33537 Revision E:1974 | INSERT, SCREW THREAD, HELICAL COIL, COARSE AND FINE THREAD, STANDARD DIMENSIONS FOR |
| MIL-P-26367 Revision A:1966 | PROPELLER SYSTEMS, AIRCRAFT, MODEL SPECIFICATION FOR (OUTLINE AND INSTRUCTIONS FOR PREPARATION) |
| MIL-E-5007 Revision D:1973 | ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR |
| MS8003 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLANGE |
| AN4076 : REV 4 NOTICE 4 | FITTING AND ENGINE CYLINDER HEAD TEMPERATURE MEASURING ELEMENT |
| MIL P 7936 : LATEST | PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY |
| MIL E 5008 : B | |
| IEC 60225:1966 | Octave, half-octave and third-octave band filters intended for the analysis of sounds and vibrations |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MIL E 25110 : NOTICE 3 | ENGINES, AIRCRAFT, RECIPROCATING, MODEL SPECIFICATION FOR |
| RR-W-365 Revision A:1980 | WIRE FABRIC (INSECT SCREENING) |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL T 25524 : D | TURBINE FUEL, AVIATION, THERMALLY STABLE |
| MIL B 131 : H | BARRIER MATERIAL, WATER VAPOR PROOF, GREASEPROOF, FLEXIBLE HEAT SEALABLE |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-I-6868 Revision E:1976 | INSPECTION PROCESS, MAGNETIC PARTICLE |
| MS8001 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLARELESS |
| MIL-B-7883 Revision B:1968 | BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS |
| NAS618:2010 | FASTENER - RECOMMENDED SHANK, HOLE AND HEAD-TO-SHANK FILLET RADIUS LIMITS FOR |
| MIL-S-8879 Revision C:1991 | SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR |
| ASTM D 1457 : 1992 | Specification for Polytetrafluorethylene (PTFE) Molding and Extrusion Materials (Withdrawn 1996) |
| MS8008 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLANGE |
| MIL-P-514 Revision D:1966 | PLATE, IDENTIFICATION, INSTRUCTION AND MARKING BLANK |
| MS33587 Revision B:1972 | TRANSMITTER INSTALLATION CLEARANCE, FUEL AND OIL PRESSURE |
| MIL-STD-1559 Revision A:1984 | NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-L-22851 Revision D:1990 | LUBRICATING OIL, AIRCRAFT PISTON ENGINE, (ASHLESS DISPERSANT) |
| MIL-F-5509 Revision D:1978 | FITTING, FLARED TUBE, FLUID CONNECTION |
| MIL W 25038 : F | WIRE, ELECTRICAL, HIGH TEMP, FIRE RESISTANT, AND FLIGHT CRITICAL, GENERAL SPECIFICATION FOR |
| QQ-S-763 Revision F:1996 | STEEL BARS, WIRE, SHAPES AND FORGINGS; CORROSION RESISTANT |
| MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
| MIL T 9107 : LATEST | TEST REPORTS, PREPARATION OF |
| SAE AMS 3380E : 2012 | HOSE, POLYTETRAFLUOROETHYLENE TFE FLUOROCARBON RESIN, WIRE BRAID REINFORCED |
| MIL-C-5584 Revision D:1988 | CONTAINER, SHIPPING AND STORAGE, METAL REUSABLE |
| MS18069 Revision B:1985 | Compounds, Adhesive, Aircraft Design and Use Limitations for Threaded Components Retained, Sealed or Locked By |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| MIL I 26600 : LATEST | INTERFERENCE CONTROL REQUIREMENTS, AERONAUTICAL EQUIPMENT |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF |
| MIL E 5556 : LATEST | |
| MIL-L-6082 Revision E:1990 | LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL) |
| AND20005 Revision 4:1976 | DRIVE - TYPE XV ENGINE ACCESSORY |
| MIL-S-5000 Revision E:1982 | STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK |
| PPP-B-601 Revision H:1989 | BOXES, WOOD, CLEATED PLYWOOD |
| MIL E 6058 : B NOTICE 1 | ENGINE, AIRCRAFT, RECIPROCATING, PREPARATION FOR SHIPMENT AND STORAGE OF |
| MIL-S-6758 Revision B:1993 | STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) |
| SAE ARP502 | PROPELLER SHAFT ENDS – FLANGED SMALL AIRCRAFT ENGINE |
| MIL STD 879 : A NOTICE 2 | DESIGNATION OF AIRCRAFT PROPULSION GAS TURBINE ENGINES |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
| MIL-STD-726 Revision H:1985 | PACKAGING REQUIREMENTS CODE |
| MIL-I-26860 Revision B:1972 | INDICATOR, HUMIDITY, PLUG, COLOR CHANGE |
| TT-I-735 Revision A:1963 | ISOPROPYL ALCOHOL |
| AND10049 : 0003 | BOSSES - FLUID CONNECTION, INTERNAL STRAIGHT THREAD |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS |
| MS5008 Revision D:1996 | CONE, PROPELLER HUB, REAR |
| MIL T 713 : E | TWINE, FIBROUS, IMPREGNATED, LACING AND TYING |
| SAE AS 971 : 1993 | DRIVE - ACCESSORY, 10.000 BC ROUND, QAD, DESIGN STANDARD FOR |
| SAE AS1132J | Bolts, Screws and Nuts - External Wrenching UNJ Thread, Inch - Design Standard |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| SAE AS681K | Gas Turbine Engine Performance Presentation for Computer Programs |
| QQ-W-343 Revision G:1997 | WIRE, ELECTRICAL, COPPER (UNINSULATED) |
| QQ-P-416 Revision F:1991 | PLATING, CADMIUM (ELECTRODEPOSITED) |
| MS33666 Revision C:1975 | PACKING, PREFORMED AERONAUTICAL, ELASTOMERIC, RANGE OF SIZES (ASG) |
| MIL-H-775 Revision E:1987 | HOSE, RUBBER OR FABRIC (INCLUDING TUBING); AND FITTINGS, NOZZLES AND STRAINERS, PACKAGING OF |
| MIL-STD-721 Revision C:1981 | DEFINITIONS OF EFFECTIVENESS TERMS FOR RELIABILITY MAINTAINABILITY, HUMAN FACTORS, AND SAFETY |
| MIL I 25017 : E | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (METRIC) |
| MIL-F-7194 Revision C:1981 | FILTER, RECIPROCATING ENGINE, INDUCTION AIR, AIRCRAFT |
| MIL-G-3056 Revision F:1991 | GASOLINE, AUTOMOTIVE, COMBAT |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| MS 26531 : LATEST | VIBRATION TEST RIG |
| MIL I 6865 : LATEST | INSPECTION, RADIOGRAPHIC |
| PPP-B-621 Revision D:1981 | BOXES, WOOD, NAILED AND LOCK CORNER |
| MS3327 Revision A:1969 | DRIVE PAD - ACCESSORY, 5,000 BC, ROUND, DESIGN STANDARD FOR |
| SAE AMS5644E | Steel, Bars and Forgings, Corrosion Resistant 17Cr - 7Ni - 1Al |
| MS9825 Revision A:1972 | CLAMP, LOOP-CUSHIONED, JOGGLED, CORROSION-RESISTING STEEL, .204 HOLE |
| MS33660 Revision D:1999 | TUBING END HOSE CONNECTION, STANDARD DIMENSIONS FOR |
| AND20006 Revision 7:1989 | Drive-Type XVI Engine Accessory |
| MIL-T-5544 Revision C:1991 | THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM |
| FED-STD-141 Revision D:2001 | PAINT, VARNISH, LACQUER AND RELATED MATERIALS, METHODS OF INSPECTION, SAMPLING AND TESTING |
| SAE AS977 | COUPLING - CLAMP, GROOVE V-BAND, FORGED 6.400, 9.400, 11.400 FLANGE OD |
| AND20007 Revision 1:1953 | DRIVE - TYPE XVII ENGINE ACCESSORY |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| AN4052 Revision 8:2013 | Coupling, Shaft, Rigid |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
| MS27417 Revision A:2009 | CAP - PROPELLER SHAFT THREAD, SHIPPING |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| NN-P-530 Revision E:1977 | PLYWOOD, FLAT PANEL |
| AND10305 Revision 5:1949 | INSTALLATION CLEARANCE - TYPE 12 AND TYPE 17 DRIVE (GENERATOR - POWER TAKE-OFF) |
| MS9144 Revision A:1962 | GASKET TYPE XX ENGINE ACCESSORY DRIVE |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) |
| IEC 60179:1973 | Precision sound level meters |
| MIL L 21260 : D | LUBRICATING OIL, INTERNAL COMBUSTION ENGINE, PRESERVATIVE AND BREAK IN |
| MS9134 Base Document:1965 | GASKET TYPE X OR XV ENGINE ACCESSORY DRIVE |
| SAE AS 965 : 1993 | DRIVE - STUDDED, ACCESSORY, 8.000 BC ROUND, DESIGN STANDARD FOR |
| O-E-760 Revision D:1987 | ETHYL ALCOHOL (ETHANOL), DENATURED ALCOHOL, PROPRIETARY SOLVENTS & SPECIAL INDUSTRIAL SOLVENTS |
| MIL E 25112 : 0 | ENGINE, AIRCRAFT, RECIPROCATING, ACCEPTANCE TESTS FOR |
| MS8006 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLARELESS |
| MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
| PPP-B-640 Revision D:1966 | BOX, FIBERBOARD, CORRUGATED, TRIPLE-WALL |
| MIL-S-6049 Revision A:1967 | STEEL, CHROME NICKEL MOLYBDENUM [8740] BARS, RODS AND FORGING STOCK FOR AIRCRAFT APPLICATION |
| MS5009 Revision A:1981 | RING, RETAINING - PROPELLER HUB, SNAP |
| MIL E 25113 : NOTICE 3 | ENGINE, AIRCRAFT, RECIPROCATING, PRELIMINARY FLIGHT RATING TEST FOR |
| MS33602 Base Document:1967 | BOLT, SELF RETAINING AIRCRAFT RELIABILITY AND MAINTAINABILITY DESIGN AND USAGE REQUIREMENTS FOR |
| MIL X 6141 : LATEST | X-RAY LABORATORY, PROCEDURE FOR CERTIFICATION |
| MIL-S-7742 Revision D:1991 | SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
| MS33668 Revision B:1975 | PACKING, PREFORMED, ELASTOMERIC, TUBE FITTING, RANGE OF SIZES |
| SAE AMS2640K | MAGNETIC PARTICLE INSPECTION |
| O-M-232 Revision M:2016 | METHANOL (METHYL ALCOHOL) |
| MIL-B-23964 Revision D:1981 | BOLT, SELF-RETAINING, POSITIVE LOCKING |
| MS21125 Revision F:1983 | BOLT SELF RETAINING POSITIVE LOCKING CRES 90 KSI FSU 63 KSI FTU PAN HEAD 450 DEG F & 650 DEG F |
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