MIL BULL 343 : A
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DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
Publisher
Withdrawn date
07-23-2013
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Covers documents applicable to aircraft engines and propellers.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
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| 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, AND CORROSION-RESISTANT AND HEAT-RESISTANT STEEL) (S/S BY A-A-59452) |
| AND10050 Revision 21:2005 | Bosses, Standard Dimensions for Gasket Seal Straight Thread |
| MIL-M-45202 Revision C:1981 | Magnesium Alloy, Anodic Treatment of (S/S by ASTM-D1732) |
| MIL C 16173 : E | CORROSION PREVENTIVE COMPOUND, SOLVENT CUTBACK, COLD APPLICATION |
| MIL-E-25109 Base Document:1955 | Engine, Aircraft, Reciprocating, General Specification for (S/S by SAE-AS25109) |
| SAE ARP373C | Propeller Shaft Torque Ratings |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| 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 (No S/S Document) |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL-A-25175 Revision C:1976 | Air Transport, Nontactical, Packing for (No S/S Document) |
| MIL-STD-280 Revision A:1969 | Definitions of Item Levels, Item Exchangeability, Models, and Related Terms (S/S by MIL-HDBK-505) |
| O-A-548 Revision D:1974 | Antifreeze/Coolant, Engine: Ethylene Glycol, Inhibited, Concentrated (S/S by A-A-870) |
| 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 (No S/S Document) |
| 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 XII ENGINE ACCESSORY (NO S/S DOCUMENT) |
| MIL-T-6736 Revision B:1965 | TUBING, CHROME-MOLYBDENUM, 4130 STEEL, SEAMLESS AND WELDED, AIRCRAFT QUALITY (USERS MAY REFER TO SAE-AMS-T-6736) AS A POSSIBLE REPLACEMENT) |
| SAE ARP1179D | Aircraft Gas Turbine Engine Exhaust Smoke Measurement |
| 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 (S/S BY AS3496) |
| MIL-P-7105 Revision B:1965 | PIPE THREADS, TAPER, AERONAUTICAL NATIONAL FORM, SYMBOL ANPT, GENERAL REQUIREMENTS FOR (S/S BY SAE-AS71051) |
| MIL-P-149 Revision D:1984 | Plastic Coating Compound, Strippable (Hot Dipping) (No S/S Document) |
| MS33658 Revision A:1959 | FITTING END, HOSE CONNECTION, STANDARD DIMENSIONS FOR (S/S BY SAE-AS5132) |
| 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 Deg. C TO +300 Deg. C) |
| MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION (S/S BY SAE-AMS-T-6845) |
| 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 (S/S BY AS3493) |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| MS20002 Revision E:1972 | WASHER, COUNTERSUNK AND PLAIN, HIGH STRENGTH (S/S BY NASM20002) |
| MS8009 Revision D:2016 | Hose Assembly, Polyetetrafluorethylene, Permanently Attached fittings, High Temperature, Medium Pressure, Flange-to-Flange |
| MIL-C-5040 Revision H:1994 | Cord, Fibrous, Nylon (S/S by PIA-C-5040) |
| 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 on (S/S by SAE-AMS-M-3171) |
| MIL-T-8808 Revision B:1981 | TUBING, STEEL, CORROSION-RESISTANT (18-8 STABILIZED), AIRCRAFT HYDRAULIC QUALITY (USE SAE-AMS5556 AND SAE-AMS5557) |
| MIL-B-26195 Revision C:1987 | Boxes, Wood-Cleated, Skidded, Load-Bearing Base (S/S by ASTM D6256/D6256M) |
| MIL-STD-480 Revision B:1988 | Configuration Control - Engineering Changes, Deviations and Waivers (S/S by MIL-STD-973) |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| 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 (S/S BY AS3495) |
| 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 (NO S/S DOCUMENT) |
| MS5011 Revision A:1981 | NUT, PROPELLER HUB RETAINING (NON CONTROLLABLE TYPE) (NO S/S DOCUMENT) |
| 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) (ASG) (S/S BY SAE-AMS6448) |
| MS 27423 : A | PROTECTOR PROPELLER SHAFT, PLASTIC |
| MS9135 Base Document:1965 | GASKET, TYPE XI ENGINE ACCESSORY DRIVE (S/S BY AS3492) |
| MS9137 Base Document:1965 | GASKET - TYPE XIII ENGINE ACCESSORY DRIVE (S/S BY AS3494) |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| MIL-C-38373 Revision B:1975 | Cap, Fluid Tank Filler (No S/S Document) |
| 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 (No S/S Document) |
| 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, Systems (S/S by MIL-STD-464) |
| QQ-W-423 Revision B:1969 | Wire, Steel, Corrosion-Resisting (S/S by ASTM-A313 and ASTM-A580) |
| MS9006 Revision C:1963 | RECESSES-CROSS, LOW TORQUE DRIVE, DIMENSIONS AND GAGE DIMENSIONS FOR (S/S BY NASM9006) |
| 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 (S/S BY SAE-AMS-T-9046) |
| 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 (S/S by MIL-L-46010) |
| MS51938 Revision C:1991 | Seal, Metallic, Lead and Wire (S/S By FF-S-2738) |
| MIL F 27272 : B | FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MS33678 Revision A:2004 | Connector, Receptacle, Electric, 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 SUBSTANTIATION FOR AEROSPACE PROPULSION SYSTEM ITEMS (NO S/S DOCUMENT) |
| AND10065 Revision 2:1946 | CONNECTION ASSEMBLY - FLEXIBLE, FLUID, STANDARD DESIGN OF (NO S/S DOCUMENT) |
| MIL B 121 : F | BARRIER MATERIAL, GREASEPROOFED, WATERPROOFED, FLEXIBLE |
| TT-E-527 Revision D:1988 | ENAMEL, ALKYD, LUSTERLESS, LOW VOC CONTENT (NO S/S DOCUMENT) |
| MIL E 5009 : D | |
| MIL T 6735 : A | TUBING, CHROME-MOLYBDENUM, 4135 STEEL, SEAMLESS AIRCRAFT QUALITY |
| MIL-T-5021 Revision D:1969 | TEST, AIRCRAFT AND MISSILE WELDING OPERATORS QUALIFICATION (SEE MIL-STD 1595) |
| PPP-T-60 Revision E:1986 | Tape: Packaging, Waterproof (S/S by ASTM D5486/ASTM-D5486M) |
| 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 (S/S BY SAE-AS4395) |
| 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) (S/S BY SAE-AMS-QQ-C-320) |
| MIL-STD-453 Revision C:1984 | Inspection, Radiographic (S/S By ASTM-E1742) |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| SAE AS870E | WRENCHING CONFIGURATION, BI-HEXAGONAL (12 POINT) DRIVE, DESIGN STANDARD FOR |
| MS5007 Revision A:1981 | CONE, PROPELLER HUB, FRONT (NO S/S DOCUMENT) |
| TT-T-548 Revision F:1991 | TOLUENE, TECHNICAL (S/S BY A-A-59107) |
| 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 (NO S/S DOCUMENT) |
| MS33588 Revision E:1984 | Nuts, Self-Locking, Aircraft, Reliability and Maintainability Usage Requirements for (S/Sby NASM33588) |
| MIL-E-8593 Revision A:1975 | Engines, Aircraft, Turboshaft and Turboprop, General Specification for |
| TT-S-735 Revision A:1988 | STANDARD TEST FLUIDS, HYDROCARBON (S/S BY ASTM-D471) |
| MIL-S-7886 Revision B:1962 | Spark Plug, Shielded, Aircraft Reciprocating Engine, General Specification For |
| AND10152 Revision 3:1953 | SHAFT ENDS - PROPELLER (NO S/S DOCUMENT) |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK (S/S BY NASM20995) |
| 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) (S/S BY SAE-AMS6382, AND SAE-AMS6349) |
| MIL-G-5572 Revision F:1969 | Gasoline, Aviation: Grades 80/87, 100/130, 115/145 (S/S by ASTM-D910) |
| MS33537 Revision E:1974 | INSERT, SCREW THREAD, HELICAL COIL, INCH SERIES, COARSE AND FINE THREAD, STANDARD ASSEMBLY DIMENSIONS FOR (S/S BY NASM33537) |
| 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 & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| 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 (S/S by MIL-STD-1949) |
| MS8001 Revision E:2016 | Hose Assembly, Polyetrafluorothylene, 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 (Future Acquisition should specify one AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7) |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| ASTM D 1457 : 1992 | Specification for Polytetrafluorethylene (PTFE) Molding and Extrusion Materials (Withdrawn 1996) |
| MS8008 Revision D:2016 | Hose Assembly, Polytetrafluorethylene, Permanently Attached Fittings, High Temperature, Medium Pressure, Flareless-to-Flange |
| MIL-P-514 Revision D:1966 | PLATE, IDENTIFICATION, INSTRUCTION AND MARKING, BLANK (S/S BY A-A-50271) |
| 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 (S/S BY MIL-HDBK-1559) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-L-22851 Revision D:1990 | Lubricating Oil, Aircraft Piston Engine (Ashless Dispersant) (S/S by SAE-J1899) |
| MIL-F-5509 Revision D:1978 | Fitting, Flared Tube, Fluid Connection (see Notice 2 for Additional Superseding Information) |
| 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 (S/S BY SAE-AMS-QQ-S-763) |
| 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 (No S/S Document) |
| 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 (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M) |
| MIL I 26600 : LATEST | INTERFERENCE CONTROL REQUIREMENTS, AERONAUTICAL EQUIPMENT |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL E 5556 : LATEST | |
| MIL-L-6082 Revision E:1990 | Lubricating Oil, Aircraft Piston Engine (Non-Dispersant Mineral Oil) (S/S by SAE-J1966) |
| AND20005 Revision 4:1976 | DRIVE - TYPE XV ENGINE ACCESSORY (NO S/S DOCUMENT) |
| MIL-S-5000 Revision E:1982 | STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS-S-5000) |
| PPP-B-601 Revision H:1989 | BOXES, WOOD, CLEATED-PLYWOOD (S/S BY ASTM-D6251) |
| 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) (S/S BY SAE-AMS-S-6758) |
| 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 CODES (S/S BY MIL-STD-2073-2) |
| MIL-I-26860 Revision B:1972 | Indicator, Humidity, Plug, Color Change (S/S by SAE-AS26860) |
| TT-I-735 Revision A:1963 | Isopropyl Alcohol |
| AND10049 : 0003 | BOSSES - FLUID CONNECTION, INTERNAL STRAIGHT THREAD |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461) |
| MS5008 Revision D:1996 | Cone, Propeller Hub, Rear |
| MIL T 713 : E | TWINE, FIBROUS, IMPREGNATED, LACING AND TYING |
| 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) (S/S BY A-A-59551) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MS33666 Revision C:1975 | PACKING, PREFORMED - AERONAUTICAL ELASTOMERIC, RANGE OF SIZES (S/S BY SAE-AS568) |
| MIL-H-775 Revision E:1987 | Hose, Hose Assemblies, Rubber, Plastic, Fabric, or Metal (Including Tubing) and Associated Hardware: Packaging of |
| MIL-STD-721 Revision C:1981 | DEFINITIONS OF TERMS FOR RELIABILITY AND MAINTAINABILITY (NO S/S DOCUMENT) |
| MIL I 25017 : E | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (METRIC) |
| MIL-F-7194 Revision C:1981 | Filter, Reciprocating Engine, Induction Air, Aircraft (No S/S Document) |
| MIL-G-3056 Revision F:1991 | Gasoline, Automotive, Combat (S/S By ASTM-D4814) |
| 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 (S/S by ASTM-D6880) |
| 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 (S/S BY NAS1715) |
| MS33660 Revision D:1999 | TUBING END, HOSE CONNECTION, STANDARD DIMENSIONS FOR (S/S BY SAE-AS5131) |
| AND20006 Revision 7:1989 | Drive-Type XVI Engine Accessory |
| MIL-T-5544 Revision C:1991 | THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM (S/S BY SAE-AMS2518) |
| 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 (NO S/S DOCUMENT) |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| 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 (See Notice 3 for Replacement Information) |
| MS27417 Revision A:2009 | Cap - Propeller Shaft Thread, Shipping |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| NN-P-530 Revision E:1977 | Plywood, Flat Panel (S/S by A-A-55057) |
| AND10305 Revision 5:1949 | INSTALLATION CLEARANCE-TYPE XII AND TYPE XVII DRIVE (GENERATOR-POWER TAKE-OFF) (NO S/S DOCUMENT) |
| MS9144 Revision A:1962 | GASKET - TYPE XX ENGINE ACCESSORY DRIVE (S/S BY SAE-AS9144) |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-N-290) |
| 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 (S/S BY AS3491) |
| O-E-760 Revision D:1987 | ETHYL ALCOHOL (ETHANOL); DENATURED ALCOHOL; PROPRIETARY SOLVENTS AND SPECIAL INDUSTRIAL SOLVENTS (S/S BY A-A-59282, A-A-51693, A-A-53880) |
| 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 Systems (S/S by MIL-STD-7179) |
| PPP-B-640 Revision D:1966 | Boxes, Fiberboard, Corrugated, Triple Wall (S/S by ASTM-D5168) |
| MIL-S-6049 Revision A:1967 | STEEL, CHROME-NICKEL-MOLYBDENUM (8740) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) (S/S BY SAE-AMS6322, SAE-AMS6325 AND SAE-AMS6327) |
| MS5009 Revision A:1981 | RING, RETAINING - PROPELLER HUB, SNAP (NO S/S DOCUMENT) |
| MIL E 25113 : NOTICE 3 | ENGINE, AIRCRAFT, RECIPROCATING, PRELIMINARY FLIGHT RATING TEST FOR |
| MS33602 Base Document:1967 | BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR (S/S BY NASM33602) |
| 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 (S/S BY SAE-AS568) |
| 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 (S/S by NASM23964) |
| MS21125 Revision F:1983 | BOLT, SELF RETAINING, POSITIVE LOCKING, CRES 90 KSI FSU, 63 KSI FTU, PAN HEAD, 450 DEG. F AND 650 DEG. F (S/S BY NASM21125) |
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