MIL BULL 343 : A
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
Publisher
Withdrawn date
23-07-2013
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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Withdrawn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, 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 |
| 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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