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Withdrawn

Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Add to Watchlist

This Standard has been added successfully to your Watchlist
Please visit My Watchlist to see all standards that you are watching.

Please log in or create an account to add this standard to your Watchlist.

We could not add this standard to your Watchlist.
Please retry or contact support for assistance.

You have already added this standard to your Watchlist.
Visit My Watchlist to view the full list.

DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF

Available format(s):

Withdrawn date: 23-07-2013

Language(s):

Published date:

Publisher: US Military Specs/Standards/Handbooks

Add to Watchlist

Abstract - (Show below) - (Hide below)

Covers documents applicable to aircraft engines and propellers.

General Product Information - (Show below) - (Hide below)

Document Type	Standard
ISBN
Pages
Published
Publisher	US Military Specs/Standards/Handbooks
Status	Withdrawn

Standards Referenced By This Book - (Show below) - (Hide below)

MIL-E-5007 Revision D:1973	ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR

Standards Referencing This Book - (Show below) - (Hide below)

MS33509 Revision A:1953	ADAPTOR INSTALLATION TYPE XII OR XVI DRIVE STARTER JAW
SAE AMS 5689 : 2012	STEEL, CORROSION AND HEAT RESISTANT, WIRE 18CR - 10.5NI - 0.40TI (321) SOLUTION HEAT TREATED
SAE AS 963 : 2001	DRIVE - STUDDED, ACCESSORY, 5.000 BC ROUND, DESIGN STANDARD FOR
SAE ARP 755 : 2014	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 ARP 373C : 2012(S2018)	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 AS 127 : 2012	PROPELLOR SHAFT END, FLANGED TYPE - NO.1, 2, 3, 4, 5 & 6
SAE AS 848 : 2012	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 AMS 2645 : 1995	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 ARP 1179 : 2011	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 AMS 5643 : 2016	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 AMS 5743 : 2014	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 AS 959 : 2001	DRIVE - STUDDED, ACCESSORY, 2.653 BC 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 ARP 1153 : 2014	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 ARP 1256 : 2011	PROCEDURE FOR THE CONTINUOUS SAMPLING AND MEASUREMENT OF GASEOUS EMISSIONS FROM AIRCRAFT TURBINE ENGINES
SAE AS 291 : 2014	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 AS 961 : 2001	DRIVE - STUDDED, ACCESSORY, 5.000 BC 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 AS 870 : 2015	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	STANDARD PRACTICE FOR 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	COMPOUND, 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 ARP 502 : 2012	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 AS 1132 : 2016	BOLTS, SCREWS AND NUTS - EXTERNAL WRENCHING UNJ THREAD, INCH - DESIGN STANDARD
MIL G 26611 : D	GENERATOR, TACHOMETER GEU-7/A, MINIATURE
SAE AS 681 : 2016	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:1964(S2017)	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 16 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 AS 977 : 2012	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	COULPING, SHAFT, RIGID
MIL-W-5088 Revision L:1991	WIRING, AEROSPACE VEHICLE
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 AMS 2640 : 1996	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

Categories associated with this Standard - (Show below) - (Hide below)

Sub-Categories associated with this Standard - (Show below) - (Hide below)

Sorry this product is not available in your region.

Add To Cart