MIL C 5541 : E
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS
Available format(s)
PDF
Superseded date
11-07-2006
Superseded by
Language(s)
English
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Outlines requirements for two classes of chemical conversion coatings made by the reaction of chemical conversion materials and the surfaces of aluminum and its alloys to provide maximum corrosion resistance on military weapon systems. Coverage includes classification, applicable documents, cleaning, appearance, corrosion resistance properties, paint adhesion properties, workmanship, solution analysis records, and visual lot examination.
| Committee |
AREA MFFP
|
| DevelopmentNote |
Supersedes SAE AMS C 5541 (10/2003)
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| DocumentType |
Standard
|
| Pages |
11
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| SAE AMS 2473 : 2013 | Similar to |
| SAE AMS C 5541 : 2000 | Similar to |
| SAE AMS2474 : 2013 | Similar to |
| MIL-C-83982 Base Document:1974 | COMPOUND, SEALING, FLUID RESISTANT |
| MIL P 21698 : A | PAINT, FLUORESCENT, FOR AIRCRAFT, PROCESS FOR APPLICATION OF |
| MIL-STD-2110 Base Document:1979 | RESTORATION, OVERHAUL, AND REPAIR OF ELECTRONIC EQUIPMENT |
| MIL-S-50218 Revision B:1978 | SWITCH, NOSE CRUSH ASSEMBLY, ASSEMBLING AND PACKING (DRAGON) |
| MIL-G-23081 Revision C:1972 | Gyroscope Indicator System, Vertical |
| SAE AS 8568 : 2012 | BINOCULARS, PRISMATIC, HAND-HELD (FOR AERONAUTICAL USE) (7 X 50 AND 6 X 42 (WIDE FIELD)) |
| MIL-C-81945 Revision B:1989 | COATING COMPOUND, WEAPON INSULATION, INTUMESCENT |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| NASM20470:2013 | RIVET, SOLID, UNIVERSAL HEAD, ALUMINIUM ALLOY AND TITANIUM COLUMBIUM ALLOY |
| SAE AMS 3116 A : 2005 | PRIMER COATING; EPOXY, CHEMICAL AND SOLVENT RESISTANT NON-CHROMATED, CORROSION PREVENTIVE |
| MIL C 38240 : C | COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
| MIL-I-8580 Revision B:1965 | INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
| MIL I 24728 : A | INTERCONNECTION BOX, FIBER OPTIC, METRIC, GENERAL SPECIFICATION FOR |
| MIL-S-23665 Revision B:1968 | SONOBUOY, DETECTION DEVICES, PRESERVATION, PACKAGING AND PACKING, PROCEDURES FOR |
| DOD-S-87956 Base Document:1979 | SHELTER, S-80A AND S-82A |
| MIL-A-38307 Revision A:1981 | ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
| MIL-F-63428 Base Document:1981 | FEED ASSEMBLY, AMMO FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2 |
| MIL-P-81655 Base Document:1970 | PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
| MIL-E-16400 Revision H:1987 | ELECTRONIC, INTERIOR COMMUNICATIONS AND NAVIGATION EQUIPMENT, NAVAL SHIP AND SHORE, GENERAL SPECIFICATION FOR |
| FF-R-556 Revision D:1981 | RIVET, SOLID, SMALL, RIVET, SPLIT, SMALL, RIVET TUBULAR SMALL, FLAT WASHER (BURR) AND CAP RIVET, GENERAL PURPOSE |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL S 24317 : 0 | SWITCH, MULTI-STATION, PUSHBUTTON (ILLUMINATED AND NON-ILLUMINATED), GENERAL SPECIFICATION FOR |
| MIL-A-83577 Revision B:1988 | ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
| MIL-A-24741 Base Document:1990 | ASSEMBLIES, METAL ELECTRICAL BACKPLANE, ONE AND TWO LAYER, GENERAL SPECIFICATION FOR |
| MIL-I-7062 Revision C:1975 | INDICATOR, POSITION, CONTROL SURFACES, 28 VOLT DC, GENERAL SPECIFICATION FOR |
| TT-P-664 Revision D:1988 | PRIMER, COATING, ALKYD, CORROSION INHIBITING, LEAD AND CHROMATE FREE, VOC COMPLIANT |
| MIL-DTL-39030-14 Revision B:2003 | DUMMY LOAD, ELECTRICAL, TYPE 14 (BIFURCATED CONTACT), STRIPLINE, LOW POWER |
| MIL C 53072 : B | CHEMICAL AGENT RESISTANT COATING (CARC) SYSTEM APPLICATION PROCEDURES AND QUALITY CONTROL INSPECTION |
| MIL-G-24659 Revision A:1993 | GAGE, DIFFERENTIAL, DIAL INDICATING |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| TT-P-2760 Revision A:1994 | PRIMER COATING; POLYURETHANE, ELASTOMERIC |
| MIL T 27252 : A | TEST SET, SYNCHRO, TTU-73/E DC SELSYN, AIRCRAFT INSTRUMENTS |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
| MIL-T-83460 Base Document:1975 | TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| MIL-I-83152 Revision B:1974 | INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
| MIL M 28837 : 0 | MIXER STAGES, RADIO FREQUENCY GENERAL SPECIFICATION FOR |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| 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-A-5885 Revision D:1987 | ACCELEROMETER, AIRCRAFT |
| SAE ARP 1481 : 2004 | CORROSION CONTROL AND ELECTRICAL CONDUCTIVITY IN ENCLOSURE DESIGN |
| MIL D 83320 : 0 | DETECTOR, MAGNETIC AZIMUTH DSU-14/A |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-I-983 Revision E:1966 | INTERIOR COMMUNICATION EQUIPMENT, NAVAL SHIPBOARD, BASIC DESIGN REQUIREMENTS FOR |
| MIL-P-9388 Revision B:1986 | PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
| MIL-I-85071 Revision A:1992 | INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
| MIL-HDBK-11991 Base Document:1996 | DESIGN OF ELECTRICAL, ELECTRONIC, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPONS SYSTEMS |
| MIL-C-27298 Revision B:1980 | CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
| MIL-C-8605 Revision B:1990 | CAP, PRESSURE FUEL SERVICING |
| MIL-L-46159 Revision A:1976 | LACQUER, ACRYLIC, LOW REFLECTIVE, OLIVE DRAB |
| MIL-A-83377 Revision B:1978 | ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
| MIL-C-28794 Base Document:1973 | Cabinet, Electronic Equipment (Single Bay) (No S/S Document) |
| MIL-STD-193 Revision L:1991 | PAINTING PROCEDURES AND MARKING FOR VEHICLES, CONSTRUCTION EQUIPMENT, MATERIAL HANDLING EQUIPMENT, AND SPARE PARTS |
| MIL-G-25597 Revision D:1973 | Gyroscope, Displacement, Roll and Pitch, Type MD-1 |
| MIL-L-50794 Base Document:1973 | Linear Shaped Charge Assembly |
| MIL P 85582 : B | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL-I-29589 Base Document:1991 | INTERROGATOR SET, AN/UPX-24(V) |
| MIL-B-8568 Revision B:1967 | BINOCULAR, PRISMATIC, HAND-HELD [FOR AERONAUTICAL USE] 7 X 50 AND 6 X 42 WIDE FIELD [ASG] |
| MIL S 25879 : C | SWITCH, RADIO FREQUENCY TRANSMISSION LINE SA-521A/A |
| MIL-A-23595 Revision D:1995 | AMPLIFIER, AUDIO FREQUENCY |
| MIL-T-27305 Revision C:1987 | TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
| MIL S 9395 : F | SWITCHES, PRESSURE, [ABSOLUTE, GAGE AND DIFFERENTIAL] GENERAL SPECIFICATION FOR |
| MIL-T-85350 Revision B:1990 | TRANSMITTER, BEACON, LOCATOR T-1438/D |
| MIL P 53030 : A | PRIMER COATING, EPOXY, WATER REDUCIBLE, LEAD & CHROMATE FREE |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| MIL-I-81186 Base Document:1966 | INDICATOR, RATE OF FUEL FLOW SYNCHRO TYPE, M590360 |
| MIL-M-7255 Revision B:1969 | MANOMETER, PRESSURE, DIFFERENTIAL AND ABSOLUTE TYPE E 1 |
| MIL-F-22735 Revision C:1980 | FILM, ELASTOMERIC, FLUORESCENT, FOR WEAPONS SYSTEMS |
| MIL B 5806 : F | BOX, SHIPPING, AND STORAGE, HELICOPTER BLADE |
| MIL-I-21206 Revision B:1960 | Indicator, Rate of Flow, Fuel; EFU-7/A (300-5000-15000 PPH) |
| MIL-DTL-50872 Revision D Interim Revision:2004 | CARTRIDGE, 40 MM: HEDP, M433 |
| MIL-I-27709 Revision A:1962 | INDICATOR, ATTITUDE ARU-14/A, REMOTE |
| MIL-E-17341 Revision C:1970 | ENGINE, GAS TURBINE, PROPULSION & AUXILIARY NAVAL SHIPBOARD |
| MS27741 Revision A:2004 | CONNECTOR, ELECTRICAL, INDIVIDUAL SHIELD TERMINATION |
| MIL S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| MIL-S-12158 Revision D:1988 | SEALING COMPOUND, NONCURING, POLYBUTANE |
| MIL-S-85312 Base Document:1979 | SEALING COMPOUND, NONCURING, POLYSULFIDE, GROOVE INJECTION, FOR INTEGRAL FUEL TANKS |
| MIL-A-55503 Base Document:1966 | ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
| MIL-A-38267 Revision A:1971 | APPLICATION OF POLYURETHANE FUEL TANK COATINGS |
| MIL-I-27196 Revision C:1988 | INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED |
| MIL R 007885 : C SUPP 1 | RIVETS; BLIND, STRUCTURAL, LOCKED AND FRICTION RETAINED SPINDLE, GENERAL SPECIFICATION FOR |
| MIL-A-43671 Base Document:1969 | ADAPTOR, REVERSIBLE, QUICK-FIT, 1-3/4 INCH |
| MIL-L-81293 Revision A:1992 | LIGHTWEIGHT SANDWICH CONSTRUCTED PANEL (ASROC) LAUNCHER MK 112 |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
| MIL F 50869 : E | FUZE, PIBD M550 LESS SPITBACK ASSEMBLY METAL PARTS & LOADING ASSEMBLING AND PACKING |
| MIL-C-7438 Revision G:1985 | CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
| MIL-DTL-63092 Revision B Interim Revision:2004 | Cartridges, 40 Millimeter, Parachutes, Loading, Assembling, and Packing |
| MIL-C-23367 Base Document:1963 | Computer, Flight Director, Aircraft |
| MIL-DTL-25949 Revision F:1995 | ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED |
| PREN 6120 : 200P1 | AEROSPACE SERIES - PINS, CLOSE TOLERANCE, SWAGE LOCKING, PROTRUDING HEAD, SHEAR TYPE, IN ALUMINIUM ALLOY 7050, CHEMICAL FILM - INCH SERIES |
| PREN 6050 : 200P3 | AEROSPACE SERIES - PINS, CLOSE TOLERANCE, SWAGE LOCKING, 100 DEGREES COUNTERSUNK REDUCED HEAD, SHEAR TYPE, IN ALUMINIUM ALLOY 7050, CHEMICAL FILM - INCH SERIES |
| I.S. EN 6080:2016 | AEROSPACE SERIES - RIVET, 100 DEGREES NORMAL FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
| MIL-DTL-7885-16 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, UNIVERSAL PROTRUDING HEAD, NICKEL-COPPER ALLOY SLEEVE (ALUM COAT), MECHANICALLY LOCKED CRES SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 4) |
| MIL-P-23460 Revision E:1991 | PIN, QUICK-RELEASE, SELF-RETAINING POSITIVE-LOCKING |
| MIL-DTL-7885-12 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE |
| MIL-DTL-7885-14 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, UNIVERSAL PROTRUDING HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 1) |
| MIL-DTL-7885-11 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, UNIVERSAL PROTRUDING HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE (TYPE I, STYLE A, CLASS 1) |
| MS17988 Revision E:1994 | PIN QUICK RELEASE POSITIVE LOCKING DOUBLE ACTING T HANDLE |
| MIL-DTL-7885-28 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, FLANGED DOME HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED 8740 ALLOY STEEL SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 4) |
| MIL-DTL-7885-15 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG.FLUSH HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE, OVERSIZE DIAMETER (TYPE I, STYLE B, CLASS 2) |
| MS17987 Revision G:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, RING HANDLE |
| MIL-PRF-25134 Revision C:1996 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL-F-22978 Revision A:1963 | FASTENER, ROTARY, QUICK-OPERATING, HIGH STRENGTH (ASG) |
| MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
| MIL S 22885 : E | SWITCH, PUSH BUTTON, ILLUMINATED, GENERAL SPECIFICATION FOR |
| MIL-DTL-7885-27 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH SHEAR HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED 8740 ALLOY STEEL SPINDLE (TYPE I, STYLE A, CLASS 3) |
| MIL-T-53101 Base Document:1990 | TANKS, FABRIC, COLLAPSIBLE, 3000, 10,000 & 20,000 GALLON, PETROLEUM, LOW TEMPERATURE |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| MIL T 28800 : E | TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-DTL-7885-13 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH SHEAR HEAD, 5056 AL ALLOY SLEEVE, MECHANICALLY LOCKED CRES SPINDLE |
| MIL-C-5501 Revision G:1989 | CAP AND PLUG, PROTECTIVE, DUST AND MOISTURE SEAL |
| MIL-DTL-25027 Revision H:1997 | NUT, SELF-LOCKING, 250 DEG F, 450 DEG F, AND 850 DEG F |
| MIL-W-45595 Revision D:1985 | WASHER, RECESSED, SADDLE AND SHOULDERED METAL |
| MIL-N-8984 Base Document:1972 | NUT, SELF-LOCKING, STEEL, 260 KS1 FTU 450 DEGREES F |
| MS17984 Revision F:1994 | PIN QUICK RELEASE, SELF RETAINING POSITIVE LOCKING SINGLE ACTING BUTTON HANDLE |
| MS20604 Revision K:1995 | RIVET, BLIND, NONSTRUCTURAL, UNIVERSAL HEAD, CLASS 1 |
| MIL-N-8985 Base Document:1972 | NUT, SELF-LOCKING STEEL, 180 KS1 FTU 450 DEGREES F |
| MIL-G-81559 Revision C:1984 | Gyroscope Assemblies and Attitude and Directional Reference Instruments for Aircraft, Packaging of |
| MS17986 Revision G:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, "L" HANDLE |
| MIL-R-27384 Revision B:1970 | RIVET, BLIND, DRIVE TYPE |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MIL-E-20652 Revision F:1986 | EYELETS, METALLIC, AND EYELET WASHERS, METALLIC, GENERAL SPECIFICATION FOR |
| MIL-R-5674 Revision F:1994 | RIVETS, STRUCTURAL, ALUMINIUM ALLOY, TITANIUM COLUMBIUM ALLOY GENERAL SPECIFICATION FOR |
| MIL-D-23615 Revision C:1993 | DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
| MIL-DTL-6162 Revision C:2000 | GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL A 7291 : A | ANTENNA AT-191B/AP |
| MIL-S-8802 Revision F:1990 | SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION |
| MIL-S-26547 Revision C:1985 | STARTER-GENERATOR ENGINE STU-6A |
| MIL-M-9397 Revision E:1979 | FREQUENCY CONVERTER, MOBILE, TYPE MC-1A |
| MIL-C-48286 Revision A:1975 | CARTRIDGE, MINE EJECTION ASSEMBLY. M198 |
| DEFSTAN 00-77(PT1)/1(2005) : INTERIM | ASAAC STANDARDS - PART 1: PROPOSED STANDARDS FOR PACKAGING |
| MIL-G-19053 Revision C:1957 | GAGE - AIRCRAFT, CAPACITANCE, LIQUID OXYGEN CONVERTER, GENERAL SPECIFICATION FOR |
| MIL-R-85111 Revision A:1980 | RECOVERY ASSIST SECURING AND TRAVERSING SYSTEM FOR LAMPS MK 111 HELICOPTER |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| TT-E-527 Revision D:1988 | ENAMEL, ALKYD, LUSTERLESS, LOW VOC CONTENT |
| MIL-E-4158 Revision E:1973 | ELECTRONIC EQUIPMENT, GROUND GENERAL REQUIREMENTS FOR |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| MIL P 53022 : B | PRIMER, EPOXY COATING, CORROSION INHIBITING, LEAD & CHROMATE FREE |
| MIL A 28875 : 0 | AMPLIFIER, RADIO FREQUENCY AND MICROWAVE, SOLID STATE, GENERAL SPECIFICATION FOR |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-P-85658 Base Document:1986 | PAINT, WATER DISPLACING |
| MIL F 83870 : A | FILTER ELEMENT, FLUID PRESSURE, TRANSMISSION, AIRCRAFT DISPOSABLE, 20 MICRON ABSOLUTE |
| SAE AS 5604 : 2012 | COMPASS: MAGNETIC, PILOT'S STANDBY |
| MIL C 7907 : A | CLEANING COMPOUND, DECONTAMINATING [FOR SOILED AND RADIOACTIVE CONTAMINATED SURFACES] |
| MIL-E-52929 Base Document:1977 | ENAMEL, ALKYD, CAMOUFLAGE, FLASH DRY |
| MIL-HDBK-509 Base Document:1998 | CLEANING AND TREATMENT OF ALUMINUM PARTS PRIOR TO PAINTING |
| MIL-T-62032 Revision H:1991 | TRUCK, TANK, FUEL SERVICING, AND AIRCRAFT FUEL SERVICING, 1,000 - 4,000 GALLON, DIESEL & GASOLINE ENGINE DRIVEN, 16,000 GVW, 4X2, 4X4. 6 X 4 & 6X6 COMMERCIAL |
| MIL-DTL-62006 Revision C:1998 | COOLER, OIL: TRANSMISSION AND ENGINE |
| MIL-T-52983 Revision G:1994 | TANK, FABRIC, COLLAPSIBLE, 3,000 10,000 20,000 AND 50,000 GALLON, FUEL |
| MIL-C-83124 Base Document:1969 | CARTRIDGE ACTUATED DEVICES PROPELLANT ACTUATED DEVICES GENERAL DESIGN SPECIFICATION FOR |
| MIL-E-50796 Base Document:1973 | EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
| MIL-STD-1250 Revision A:1992 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL-S-7124 Revision B:1966 | SEALING COMPOUND, POLYSULFIDE, ACCELERATOR REQUIRED FOR AIRCRAFT STRUCTURES |
| MIL-A-24233 Revision B:1989 | ANTENNA, AS-1735( )/SRC |
| MIL-D-83029 Revision A:1968 | DRIVE ASSEMBLY, CONSTANT SPEED, GENERAL SPECIFICATION FOR |
| MIL R 83178 : A | REGULATOR, OXYGEN, DILUTER DEMAND, AUTOMATIC PRESSURE BREATHING, GENERAL SPECIFICATION FOR |
| MIL-P-5994 Revision D:1972 | PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
| MIL P 52995 : 0 | PRIMER COATING, SYNTHETIC, CORROSION INHIBITING, LACQUER RESISTING, LEAD AND CHROMATE FREE |
| MIL I 18997/2 : 0 | INDICATOR, PRESSURE, BOURDON TUBE CIRCULAR DIAL, OXYGEN SERVICE, BLEEDER TIP (3-1/2 AND 4-1/2 INCH SIZES) |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
| MIL-R-81553 Revision B:1992 | REGULATOR, CHEST MOUNTED, OXYGEN, POSITIVE PRESSURE, CRU-79/P |
| MIL L 3890 : A | LINE, RADIO FREQUENCY TRANSMISSION [COAXIAL AIR DIELECTRIC] |
| MIL-M-63508 Base Document:1982 | MINE, METAL PARTS FOR MINES: BLU-91/B AND BLU-92/B |
| MIL-C-82594 Base Document:1971 | CORROSION PREVENTIVE COMPOUND AND SURFACE SEALER FOR NONFERROUS METALS |
| MIL L 3976 : D | LIGHTS, MARKER, CLEARANCE (SERVICE & BLACKOUT) |
| MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
| MIL-DTL-39030-16 Revision B:2003 | DUMMY LOAD, ELECTRICAL, TYPE 14 (BIFURCATED CONTACT), STRIPLINE, LOW POWER |
| MIL-C-5604 Revision B:1962 | COMPASS, MAGNETIC, PILOTS STANDBY |
| MIL I 18997/1 : 0 | INDICATOR, PRESSURE, CIRCULAR DIAL (3-112 4-1/2 AND 8-1/2 INCH DIAL SIZES) |
| MIL-C-8603 Revision B:1984 | CLAMPS, LOOP TYPE, AND STRAPS, SUPPORT |
| MIL-H-87111 Revision A:1984 | HEAT SINKS, SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR |
| MIL-HDBK-1250 Revision A:1995 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL-STD-1516 Revision B:1990 | UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL |
| MIL-STD-2198 Base Document:1990 | DESIGN REQUIREMENTS FOR METAL ELECTRICAL BACKPLANE ASSEMBLIES |
| MIL-F-24666 Base Document:1986 | FILTER ELEMENT, SHIP FUEL SYSTEM PREFILTER, NONCLEANABLE, HIGH EFFICIENCY |
| MIL P 53084 : 0 | PRIMER, CATHODIC ELECTRODEPOSITION, CHEMICAL AGENT RESISTANT |
| TT-P-2756 Revision A:1996 | POLYURETHANE COATING - SELF-PRIMING TOPCOAT, LOW VOLATILE ORGANIC COMPOUND (VOC) CONTENT |
| TT-E-489 Revision J:1994 | ENAMEL, ALKYD, GLOSS, (FOR EXTERIOR AND INTERIOR SURFACES) |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL L 58085 : A | LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
| MIL-T-704 Revision K:1992 | Treatment and Painting of Material |
| MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
| PREN 6100 : 200P2 | AEROSPACE SERIES - PINS, CLOSE TOLERANCE, SWAGE LOCKING, 100 DEGREES COUNTERSUNK HEAD, SHEAR TYPE, IN ALUMINIUM ALLOY 7050, CHEMICAL FILM - INCH SERIES |
| MIL R 46963 : A | ROCKET MOTOR, M42A1, BOOSTER |
| MIL-C-83019 Base Document:1968 | COATING, POLYURETHANE, FOR PROTECTION OF INTEGRAL FUEL TANK SEALING COMPOUND |
| MIL-C-4150 Revision J:1989 | CASE, TRANSIT AND STORAGE, WATERPROOF AND WATER-VAPORPROOF |
| MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
| MIL-A-63576 Revision A:1985 | ALUMINUM OXIDE COATINGS, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-DTL-85110 Revision B:1997 | BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
| PREN 6051 : 200P3 | AEROSPACE SERIES - COLLARS, SWAGE LOCKING, SHEAR TYPE, IN ALUMINIUM ALLOY 3003, CHEMICAL FILM - INCH SERIES |
| PREN 6054 : 200P3 | AEROSPACE SERIES - COLLARS, SWAGE LOCKING, SHEAR TYPE, IN ALUMINIUM ALLOY 6061, CHEMICAL FILM - INCH SERIES |
| I.S. EN 4660-004:2011 | AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 004: PACKAGING |
| SAE AMS 3603 : 2002 | PROTECTIVE FILM, HIGH PERFORMANCE, POLYMERIC PRESSURE SENSITIVE ADHESIVE, FOR AIRCRAFT EXTERIOR APPLICATIONS |
| SAE AS 1297 : 2008(S2014) | REDUCERS, PNEUMATIC PRESSURE, MISSILE |
| MIL-G-18997 Revision E:1991 | GAUGE, PRESSURE, DIAL INDICATING |
| MIL-STD-186 Revision F:2002 | PROTECTIVE FINISHING SYSTEMS FOR ROCKETS, GUIDED MISSILES, SUPPORT EQUIPMENT AND RELATED MATERIALS |
| MIL-A-43820 Revision B:1981 | AIR LOCK, (MUST) |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-I-6447 Revision C:1974 | INDICATOR, TRUE AIRSPEED TYPE M 1A |
| MIL S 28827 : A | SWITCH, THERMOSTATIC, (VOLATILE LIQUID) HERMETICALLY SEALED GENERAL SPECIFICATION FOR |
| MIL-C-22751 Revision D:1971 | COATING SYSTEM, EPOXY-POLYAMIDE, CHEMICAL AND SOLVENT RESISTANT, PROCESS FOR APPLICATION OF |
| MIL-A-23622 Base Document:1963 | ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
| MIL-T-25193 Revision B:1961 | Transmitter, Remote Compass, Type C-2 (Unstabilized) |
| MIL-I-5418 Revision B:1963 | INDICATOR: AIRSPEED, PITOT STATIC, SENSITIVE, 50-650 KNOTS |
| SAE AIR 1664 : 2013 | AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS |
| MIL-C-27725 Revision B:1969 | COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS |
| MIL-M-7997 Revision C:1981 | Motor, Aircraft Hydraulic, Constant Displacement General Specification for |
| MIL-C-83873 Revision A:1993 | CLEANING COMPOUND, PRECOATING SURFACE, AIRCRAFT & AEROSPACE GROUND EQUIPMENT (AGE) |
| TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL-W-14993 Revision B:1975 | WARHEAD SECTION, GUIDED MISSILE, PRACTICE, M231 |
| MIL-T-60916 Revision C:1991 | TUBE, MOTOR, INTEGRAL BULKHEAD FOR ROCKET MOTOR 2.75 INCH, MARK 4 AND MARK 40 |
| MIL-L-3851 Revision E:1991 | LOOP, SLIDE [FOR EQUIPAGE] |
| SAE AMS 1377 : 2012 | REMOVER, PAINT, EPOXY AND POLYURETHANE PAINT SYSTEM, NON-CHLORINATED SOLVENT |
| MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MIL-I-83751 Base Document:1967 | INDICATOR, SAFETY LEVEL, RF |
| MIL-S-40626 Revision D:1994 | SIGN KIT, VEHICLE CLASS |
| NASM 23460 : 2004 | PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING |
| MIL-B-26793 Revision B:1958 | BLOWER, GASOLINE ENGINE DRIVEN, TYPE A-1 |
| MIL-A-26107 Revision D:1960 | AIR CONDITIONER, TRAILER-MOUNTED, FREON CYCLE, 11-1/2 TON REFRIGERATING CAPACITY, TYPE MA-3 |
| MIL-A-38331 Base Document:1964 | AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
| MIL-A-28865 Revision A:1987 | ANTENNA GROUP, OE-82()/WSC-1(V) |
| MIL-I-21203 Revision A:1962 | Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro |
| MIL-A-19940 Base Document:1957 | AMPLIFIER, CONTROL SINGLE CHANNEL, S-2 COMPASS |
| MIL-G-22169 Base Document:1959 | GYRO, VERTICAL AND MOUNT |
| MIL-C-18053 Revision A:1958 | CONTROL AMPLIFIER, ALTITUDE (P-1 AUTOMATIC PILOT RADAR SET, AN/APN-22) |
| MIL-A-62473 Revision B:1992 | ARMOR, ALUMINUM-ARAMID, LAMINATE COMPOSITE |
| MIL L 13629 : C NOTICE 1 | LACQUER, AIR DRYING FOR CRIMPED PARTS |
| MIL-H-9890 Revision E:1988 | HARDWARE, INDIVIDUAL LOAD CARRYING EQUIPMENT: AND HARDWARE, MISCELLANEOUS |
| MIL-R-19750 Revision A:1958 | REGULATOR; VOLTAGE, 28 V, 120 DEGREE C, FOR 30 V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
| MIL C 63092 : A | CARTRIDGES, 40MM, WHITE STAR, PARACHUTE, M583A1 GREEN STAR, PARACHUTE M661 RED STAR, PARACHUTE, M662 METAL PARTS AND LOADING ASSEMBLING AND PACKING |
| MIL-I-19028 Revision E:1971 | INVERTER (FOR TORPEDO MARK 37 MODS O, O)M(, 1, 2, AND 3) |
| MIL-A-43759 Revision A:1981 | ADAPTERS, AIR LOCK, MUST |
| MIL-L-28796 Base Document:1973 | LINE ASSEMBLIES, RADIO FREQUENCY TRANSMISSION GENERAL SPECIFICATION FOR |
| MIL-T-28735 Base Document:1970 | TEST SET RADAR AM UPM 137 |
| MIL-C-85528 Base Document:1983 | CONNECTOR, ELECTRICAL, MOUNTING DEVICE, FLANGE TYPE, GENERAL SPECIFICATION FOR |
| MIL-T-28764 Base Document:1971 | TEST SET, RADAR, AN/UPM-136 |
| MIL I 82356 : NOTICE 1 | INSTRUMENTS, SIMULATED, FOR AIRCRAFT TRAINING DEVICES; GENERAL SPECIFICATION FOR |
| MIL-C-18438 Revision B:1962 | Chargers, Battery, Generator Type |
| NASA KSC TM 584 : 1994 | CORROSION CONTROL AND TREATMENT MANUAL |
| MIL-T-85630 Base Document:1983 | Tube, Motor, for 2.75 Inch Rocket, Mark 66 |
| MIL-P-81985 Base Document:1974 | PEENING OF METALS |
| SAE AS 7997:1999 | MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR |
| MIL-A-81852 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL W 28839 : 0 | WAVEGUIDE, ELLIPTICAL GENERAL SPECIFICATION FOR |
| MIL-E-52835 Revision A:1977 | ENAMEL, MODIFIED ALKYD, CAMOUFLAGE, LUSTERLESS |
| MIL S 45310 : H NOTICE 1 | SEMITRAILER, TANK, GASOLINE AND FUEL OIL, COMMERCIAL |
| MIL-W-50930 Base Document:1971 | WARHEAD SECTION 762MM ROCKET TRAINING M42' |
| MIL-W-50932 Base Document:1971 | WARHEAD SECTION, 762MM ROCKET, TRAINING: M42, OGIVE FOR |
| MIL-STD-808 Revision A:1983 | FINISH, MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN SUPPORT EQUIPMENT |
| MIL L 52909 : NOTICE 1 | LACQUER, ACRYLIC, CAMOUFLAGE, LUSTERLESS |
| MIL-B-233 Revision D:1987 | BOXES, SUPPLY SUPPORT ITEMS, STOWAGE AND STORAGE |
| MIL-S-29413 Revision B:1988 | SHELTER, JOINING CORRIDOR FOR |
| MIL-W-14980 Revision A:1971 | WARHEAD, GUIDED MISSILE, HE, M224 PARTS FOR |
| MIL-T-21578 Revision A:1966 | TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
| TT-R-230 Revision B:1968 | REMOVER, PAINT (ALKALI TYPE FOR HOT APPLICATION) |
| MIL T 25439 : A (1) | TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
| MIL S 55041 : C | SWITCH, WAVEGUIDE GENERAL SPECIFICATION FOR |
| MIL-C-85642 Base Document:1985 | COMMUNICATIONS CENTRAL AN/ASC-26 |
| MIL-B-38401 Revision A:1973 | BEACON SET, RADIO AN/URT-33 |
| MIL I 6839 : C | INDICATOR, POSITION, LANDING GEAR |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| MIL T 83454 : 0 | TERMINAL, STUD, BLIND PLATE, FOR ELECTRICAL BONDING AND GROUNDING (NONINSULATED) |
| MIL-A-24319 Revision B:1981 | ANTENNA, WHIP, 10.67 METERS (35), AS-2537()/SR |
| MIL-T-27200 Revision C:1975 | TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
| MIL-E-85082 Revision A:1992 | ENCODERS, SHAFT ANGLE TO DIGITAL, GENERAL SPECIFICATION FOR |
| MIL-T-85601 Base Document:1983 | TEST SET, INDICATOR AN/APM-433 |
| MIL I 7304 : B | INDICATOR, PRESSURE TORQUE SENSITIVE TYPE A 9 |
| MIL-I-5482 Revision C:1960 | INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE |
| MIL-M-24144 Revision D:1988 | Monitors, Frost-Point/Dew-Point, Compressed Air, Semi-Portable (Future Acquisitions for this item may Refer to ST000-AG-IDX-010) |
| MIL A 29563 : 0 | ANTENNA SYSTEM, AIMS SHIPBOARD, ELECTRONICALLY STEERED OE-120/UPX |
| MIL-C-81790 Revision A:1990 | CONNECTORS, RECEPTACLE, EXTERNAL ELECTRIC POWER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AS 85376 : 2007 | STAND, SHIPBOARD, HELICOPTER MAINTENANCE |
| NFPA 69 : 2014 | EXPLOSION PREVENTION SYSTEMS |
| BS EN 4660-004:2011 | Aerospace series. Modular and open avionics architectures Packaging |
| STANAG 4626 : 2013 | MODULAR AND OPEN AVIONICS ARCHITECTURE |
| MIL-R-19309 Revision D:2003 | RELAY, SENSITIVE (FOR TORPEDO MARK 37 MOD 2) |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| NASA MSFC SPEC 250 : 1963 | PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-C-24105 Revision D:1995 | CONVERTERS, SYNCHRO SIGNAL (PANEL MOUNTED) GENERAL SPECIFICATION FOR |
| MIL-P-43155 Revision F:1984 | PRINTING PLANT, SPECIAL WARFARE, TRANSPORTABLE, (LIGHTWEIGHT) MODEL 800 |
| MIL-S-29410 Revision B:1988 | SHELTER ASSEMBLY, RIGID GENERAL PURPOSE |
| I.S. EN 6101:2016 | AEROSPACE SERIES - RIVET, 100 DEGREES MEDIUM FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| MIL I 5099 : B | INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
| MIL I 25725 : A | INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8 |
| MIL-I-18804 Revision B:1964 | INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH |
| MIL-C-11198 Revision K:1984 | CHEST, ICE STORAGE |
| MIL-B-543 Revision G:1990 | BUCKLE, TONGUELESS AND WEB STRAP |
| MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
| MIL-R-24358 Base Document:1968 | RESTORATION SHIPBOARD ELECTRONIC EQUIPMENT F, 1N AND 2N COGNIZANCE |
| MIL-I-21718 Base Document:1958 | Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots |
| MIL G 8360 : A | GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
| DSCC 85075 : B | SUPPORT, ELECTRICAL CARD HOLDER, MOUNTING BAR |
| MIL-S-29412 Revision C:1994 | SHELTER, COMPLEXING KIT FOR |
| MIL-A-23282 Revision B:1965 | ACTUATOR |
| MIL-S-83315 Base Document:1971 | SEALING COMPOUND, ALUMINUM STRUCTURE, PRESSURE AND WEATHER SEALING, LOW DENSITY |
| MIL-L-21652 Revision A:1964 | Light, Beacon, Anticollision, Aircraft, General Specification for |
| MIL L 46142 : 0 | LACQUER, LUSTRELESS, SOLAR HEAT REFLECTING |
| MIL L 52962 : 0 | LACQUER, CHLOROSULFONATED POLYETHYLENE, CAMOUFLAGE, LUSTERLESS |
| MIL-H-18911 Revision A:1974 | HEAD AND MOTOR, ROCKET, INERT PARTS, PAINTING AND MARKING |
| MIL T 6349 : C NOTICE 1 | TEST SET, SYNCHRO |
| MIL-I-26689 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
| MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
| MIL A 22641 : D | ADAPTOR, COAXIAL TO WAVEGUIDE, GENERAL SPECIFICATION FOR |
| MIL F 50907 : NOTICE 1 | FIRING DEVICE, ANTI PERSONNEL MINE, XM 123 PARTS & ASSEMBLY |
| MIL-N-3336 Revision A:1964 | Nut, Sheet Spring, Instrument Mounting |
| MIL-R-14821 Base Document:1968 | REMOVER, AIRCRAFT CANOPY. M9 REMANUFACTURED METAL PARTS ASSEMBLY |
| MIL L 3661 : B | LAMPHOLDER, INDICATOR LIGHTS, INDICATOR LIGHT HOUSINGS AND INDICATOR LIGHT LENSES GENERAL SPECIFICATION FOR |
| MIL-DTL-50869 Revision F Interim Revision:2004 | Fuze, Point Initiating, Base Detonating (PIBD) - M550, Less Spitback Assembly Loading, Assembling, and Packing |
| MIL M 7793 : F | METER, TIME TOTALIZING |
| MIL C 27889 : D | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
| MIL-A-25915 Revision A:1980 | ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
| MIL S 3928 : D | SWITCH, (COAXIAL) RADIO FREQUENCY TRANSMISSION LINE, GENERAL SPECIFICATION FOR |
| MIL-G-81168 Base Document:1964 | GYROSCOPE, RATE INTEGRATING |
| MIL-S-24317-9 Revision B:2006 | Switches, Multistation, Push Button, Matrix Arrangement Plug-In Module, 2 Amperes, Unsealed, Type SM09L1 |
| MIL-C-81991 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL-HDBK-83377 Base Document:1997 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for |
| MIL-DTL-44285 Revision A:2000 | DOORS, DOUBLE BUMP THROUGH |
| MIL-C-81740 Base Document:1969 | COATING, ALUMINUM AND ALUMINUM ALLOYS (METALLIC COMPOUND DECOMPOSITION) |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-C-26485 Revision D:1968 | CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
| MIL-R-23761 Revision B:1975 | Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL A 25088 : C | |
| MIL-I-25861 Revision D:1967 | INDICATOR, PRESSURE, HYDRAULIC, 0-4000 PSI INTEGRALLY LIGHTED |
| MIL-C-81946 Base Document:1973 | COATING SYSTEM, THERMAL INSULATION, INTUMESCENT |
| MIL-P-19692 Revision E:1994 | PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR |
| MIL C 22750 : F | COATING, EPOXY, VOC-COMPLIANT |
| MIL-S-70334 Base Document:1987 | SHIM, SOLID GENERAL SPECIFICATION FOR |
| MIL-G-7734 Revision C:1981 | GAGE, PRESSURE ENGINE AND UTILITY AIRCRAFT |
| MIL-C-172 Revision C:1958 | CASES: BASES, MOUNTING & MOUNTS, VIBRATION (FOR USE WITH ELECTRONIC EQUIPMENT) |
| MIL S 24251 : B | SHIELD, RETAINER (BASES), AND ADAPTERS, ELECTRON TUBE, HEAT DISSIPATING, GENERAL SPECIFICATION FOR |
| MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
| MIL-R-60897 Base Document:1968 | REMOVER, AIRCRAFT CANOPY, M8A1 METAL PARTS ASSEMBLY (CONVERSION) |
| MIL-G-23723 Base Document:1964 | Gyroscope, Rate Switching CN-495/AJB-3 |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| MIL G 23701 : 0 | MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52 |
| MIL-C-8412 Revision B:1969 | COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
| MIL-PRF-22885-112 Revision A:2013 | Switches, Pushbutton, White Light Emitting Diode (LED) Illuminated, Standard, Night Vision Imaging System (NVIS) and Sunlight Readable Displays, Dimmable, SPDT and DPDT, Low Level to 7 Amperes, Sealed and Unsealed, Solder and Common Termination System (CTS) Terminations |
| MIL I 7069 : A NOTICE 1 | INDICATORS, TACHOMETER, ELECTRIC, PERCENT SPEED TYPE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-S-63302 Base Document:1979 | SAFETY AND ARMING ASSEMBLIES FOR MINES: M74 AND M75 |
| MIL C 28754/21 : E | CONNECTOR, ELECTRICAL, MODULAR, FRAME, CASTING, TYPE 4, DOUBLE SPAN |
| MIL-S-63326 Base Document:1981 | SAFETY AND ARMING ASSEMBLIES FOR MINES: BLU-91/B AND BLU-92/B |
| DOD-E-8983 Revision C:1977 | ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
| MIL I 6424 : A NOTICE 1 | INDICATOR, INDUCTION COMPASS, TYPE V 8 |
| MIL-A-23088 Revision A:1963 | AMPLIFIER, RADIO FREQUENCY AM-3198 |
| MIL I 26359 : B | INDICATOR, ATTITUDE, REMOTE ARU-4/A |
| MIL-P-9389 Revision A:1987 | PUMP PRESSURE, OIL AND FREE AIR, TYPE MA AND 3 |
| MIL P 23971 : B | POWER DIVIDERS, POWER COMBINERS AND POWER DIVIDER/COMBINERS, GENERAL SPECIFICATION FOR |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL C 50509 : A | CARTRIDGE, 40MM, WHITE STAR, CLUSTER, M585A1 METAL PARTS FOR AND LOADING, ASSEMBLING AND PACKING |
| MIL-T-19646 Revision A:1990 | THERMOMETER, REMOTE READING, SELF-INDICATING DIAL, GAS ACTUATED |
| MIL-D-21625 Revision G:1993 | DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
| MIL-S-29411 Revision B:1988 | SHELTER ASSEMBLIES, 10 FOOT AND 20 FOOT ELECTROMAGNETIC INTERFERENCE |
| MIL-T-38306 Base Document:1964 | TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
| MIL-L-3890-3 Revision A:1970 | LINE, RADIO FREQUENCY TRANSMISSION [COAXIAL, AIR DIELECTRIC] 50 OHMS TYPE RG 382/U |
| MIL P 22636 : NOTICE 1 | PRIMER COATING; FOR RED FUMING NITRIC ACID RESISTANT PAINT |
| MIL C 28754 : D | CONNECTOR, ELECTRICAL, MODULAR AND COMPONENT PARTS, GENERAL SPECIFICATION FOR |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL C 28754/23 : F | CONNECTOR, ELECTRICAL, MODULAR, CONNECTOR ASSEMBLY, TYPE 4, SINGLE SPAN |
| MIL-H-9896 Revision C:1988 | HARDWARE, UNIVERSAL LOAD CARRYING SLING |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-S-52377 Revision D:1990 | SHOP EQUIPMENT, ELECTRONIC REPAIR, SEMI TRAILER MOUNTED |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| ARINC 404B-2:2015 | CONNECTORS, RACK AND PANEL, RECTANGULAR REAR RELEASE CRIMP CONTACTS |
| MIL STD 194 : A NOTICE 2 | SYSTEM FOR PAINTING AND FINISHING FIRE-CONTROL MATERIEL |
| L-P-1040 Revision B:1977 | PLASTIC SHEETS AND STRIPS (POLYVINYL FLUORIDE) |
| MIL-B-23072 Base Document:1961 | BLOWER, ANTI-EXPOSURE SUIT VENTILATION, GENERAL SPECIFICATION FOR |
| MIL-A-27198 Revision B:1987 | ALTIMETER, PRESSURE AAU-7/A |
| MIL-C-9075 Revision A:1968 | COMPUTER AND TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 150-900 KNOTS, TYPE MA 1 |
| MIL-R-7885 Revision D:1988 | RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED SPINDLE AND FRICTION LOCKED SPINDLE, GENERAL SPECIFICATION FOR |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-A-22165 Base Document:1959 | Amplifier, Compass, Servo (Type MF-1 Compass) |
| MIL I 7491 : B | INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
| MIL-I-21685 Base Document:1958 | INDICATOR, COMPASS REPEATER, ROTATING DIAL, TYPE MW-2 |
| SAE AMS 3146 : 2000 | COATING, INTERIOR AIRCRAFT CABIN LOW HEAT AND SMOKE RELEASE |
| MIL-A-81403 Base Document:1967 | ALTIMETER-ENCODER, AAU-21/A |
| MIL-A-27261 Revision A:1966 | Accelerometer, Aircraft |
| MIL P 43184 : 0 | PLATFORM COMPONENTS, AIR DELIVERY. MODULAR (DUAL RAIL SYSTEM), TYPE II |
| SAE AMS 3259 : 1997 | SEALING COMPOUND, POLYTHIOETHER - NONCHROMATED, CORROSION INHIBITING FOR INTERMITTENT USE TO 360 DEGREE F (182 DEGREE C) |
| SAE AMS P 81985 : 2001 | PEENING OF METALS |
| ARINC 654 : 1994 | ENVIRONMENTAL DESIGN GUIDELINES FOR INTEGRATED MODULAR AVIONICS PACKAGING AND INTERFACES |
| PREN 6101 : 200P2 | AEROSPACE SERIES - RIVET, 100 DEGREES MEDIUM FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| BS EN 6101:2016 | Aerospace series. Rivet, 100° medium flush head, close tolerance. Inch series |
| BS EN 6080:2016 | Aerospace series. Rivet, 100° normal flush head, close tolerance. Inch series |
| PREN 6069 : 200P3 | AEROSPACE SERIES - RIVET, 100 DEGREES REDUCED FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| BS EN 6081:2016 | Aerospace series. Rivet, universal head, close tolerance. Inch series |
| EN 6080:2016 | Aerospace series - Rivet, 100° normal flush head, close tolerance - Inch series |
| EN 6081:2016 | Aerospace series - Rivet, universal head, close tolerance - Inch series |
| EN 6101:2016 | Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch series |
| EN 4660-004:2011 | Aerospace series - Modular and Open Avionics Architectures - Part 004: Packaging |
| MIL-S-83318 Revision A:1991 | SEALING COMPOUND, LOW TEMPERATURE CURING, QUICK REPAIR, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
| MIL-B-36120 Base Document:1962 | BACK REST, LITTER, NONADJUSTABLE |
| MIL-PRF-81733 Revision D:1998 | SEALING AND COATING COMPOUND, CORROSION INHIBITIVE |
| MIL C 85285 : C | |
| MIL-C-81947 Revision A:1975 | COATING COMPOUND, THERMAL INSULATION, THREE-COMPONENT, INTUMESCENT |
| MIL F 50864 : B | FUZE, PIBD, M549, LESS SPITBACK METAL PARTS AND LOADING, ASSEMBLING AND PACKAGING |
| MIL-B-81934 Revision B:1991 | BEARING, SLEEVE, PLAIN AND FLANGED, SELF LUBRICATING |
| MIL-A-49079 Revision A:1986 | ALTIMETER SET, ELECTRONIC AN/APN-209(V) (UNITS OF) |
| MIL S 4510 : E | SPOTLIGHT, INCANDESCENT, ROOF MOUNTED, AUTOMOTIVE |
| MIL-F-8378 Revision B:1975 | FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
| MIL-T-27-233 Base Document:1978 | TRANSFORMERS AND INDUCTORS (AUDIO POWER AND HIGH POWER PULSE) INDUCTOR CHARGING TF5S37ZZ |
| MIL-A-25933 Revision B:1985 | ALTIMETER, PRESSURIZED COMPARTMENT, INTEGRALLY LIGHTED 0-50,000 FEET, 1-7/8 INCH DIAL |
| I.S. EN 6081:2016 | AEROSPACE SERIES - RIVET, UNIVERSAL HEAD, CLOSE TOLERANCE - INCH SERIES |
| MIL-A-26360 Revision B:1982 | AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
| MIL-A-27330 Revision B:1987 | ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
| MIL-S-21277 Revision A:1958 | SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
| MIL L 81352 : A | LACQUER, ACRYLIC (FOR NAVAL WEAPONS SYSTEMS) |
| MIL-T-81838 Base Document:1971 | Tank, Fuel, Aircraft, Auxiliary External 300 Gallon, Type AERO-1D |
| MIL T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
| MIL S 8932 : A | SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-M-83524 Base Document:1985 | MICROSCOPE, OPTICAL, MONOCULAR, HAND-HELD, PORTABLE, MILITARIZED, 200X MAGNIFICATION, FOR FIELD INSPECTION OF OPTICAL FIBERS |
| MIL PRF 62478 : A | COUPLER, OPTICAL |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| MIL-P-21415 Revision C:1973 | PROTECTIVE FINISH AND PAINTING FOR POLARIS FLEET BALLISTIC MISSILE |
| MIL-R-81903 Revision A:1977 | REMOVER, ACID ACTIVATED, FOR AMINE CURED EPOXY COATING SYSTEMS |
| MIL-W-87105 Base Document:1977 | WAVEGUIDE ASSEMBLIES, GENERAL SPECIFICATION FOR |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| SAE AS 85075 : 2000 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
| MIL-R-81835 Base Document:1971 | REMOVER, ORGANIC COATING, HOT TANK TYPE |
| MIL-R-25410 Revision G:1991 | REGULATORS, OXYGEN, DILUTER-DEMAND AUTOMATIC-PRESSURE BREATHING |
| DOD-HDBK-343 Base Document:1986 | DESIGN, CONSTRUCTION, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT |
| TT-E-529 Revision G:1988 | ENAMEL, ALKYD, SEMIGLOSS, LOW VOC CONTENT |
| MIL-HDBK-1568 Base Document:1996 | MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
| 15/30327754 DC : 0 | BS EN 4660-004 - AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 004: PACKAGING |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| MIL-I-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
| MIL-M-24605 Revision A:1988 | MONITOR, HEAT STRESS |
| MIL C 83488 : C | COATING, ALUMINUM, ION VAPOR DEPOSITED |
| MIL P 47115 : A | PAINT, EPOXY, ABRASION, HEAT AND CORROSION RESISTANT |
| MIL-S-43766 Revision A:1988 | SUPPORT ASSEMBLY, ARCH, INFLATABLE SHELTER SECTION (MUST) |
| MIL-V-18318 Revision B:1966 | VALVE, PRESSURE REGULATING, OXYGEN SYSTEM |
| MIL-T-26963 Revision D:1992 | TESTER, PRESSURE GAGE, HYDRAULIC, PORTABLE TYPE MP-1 |
| MIL-I-25941 Revision D:1986 | INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
| MIL-DTL-28754-67 Revision A:2016 | CONNECTORS, ELECTRICAL, MODULAR, CONNECTOR FRAME, TYPE 4, DOUBLE SPAN, CENTER |
| MIL T 18460 : 0 | TEST SET, INDICATOR, AN/APM-74 |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
| MIL-G-27693 Revision A:1962 | GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH |
| MIL-G-22077 Revision C:1993 | GENERATOR SETS, GAS TURBINE, DIRECT AND ALTERNATING CURRENT NAVAL SHIPBOARD USE |
| MIL-G-5678 Revision C:1964 | GAGE PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE |
| MIL-DTL-83488 Revision D:1999 | COATING, ALUMINUM, HIGH PURITY |
| MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL G 5413 : D NOTICE 1 | GENERATOR, TACHOMETER, FOUR POLE |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| MIL-G-25591 Revision E:1981 | Gyroscope, Rate, Switching, Type MC-1 |
| MIL T 25435 : B | TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
| MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
| MIL-DTL-32175 Base Document:2004 | FUZE, PIBD - M549A1, LESS SPITBACK ASSEMBLY |
| MIL M 62361 : C | MOTOR, DRIVE, DIRECT CURRENT 2 RPM/8RPM |
| NASA MSFC PROC 547 : 2014 | POLYURETHANE COATING, APPLICATION OF |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-C-23157 Revision D:1979 | CLIPBOARD, PILOTS, MXU-163/P AND MARK 2A |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL-T-58082 Revision A:1974 | TESTER, PYROMETER & THERMOCOUPLE, FIELD, TYPE N-3A |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL W 6496 : B NOTICE 1 | WINCH, DRUM, ENGINE OF TURRET HOIST, TYPE A-1 |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL I 27851 : B | INDICATOR, INDICATED AIRSPEED AVU-17/A |
| MIL-T-25307 Revision D:1985 | TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| MIL-I-25437 Revision B:1984 | INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-8974 Revision A:1981 | INDICATOR, EVENT COUNTING, GENERAL SPECIFICATION FOR |
| MIL M 62368 : A | MOTOR, GEARHEAD, 18-30 VOLTS, DIRECT CURRENT |
| MIL-A-43326 Revision A:1983 | ALTAR, PORTABLE |
| MIL L 25866 : B | LIGHT, EMERGENCY EXIT, AIRCRAFT LEU AND 1-A |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
| MIL C 15370 : F | COUPLERS, DIRECTIONAL GENERAL SPECIFICATION FOR |
| DOD-C-85050 Base Document:1982 | CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL G 9398 : C | GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT |
| MIL-P-24764 Base Document:1991 | POWER SUPPLIES, SHIPBOARD, ELECTRONIC, GENERAL SPECIFICATION FOR |
| MIL I 27190 : B | INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL-D-38134 Revision A:1971 | DETECTOR, MAGNETIC AZIMUTH DSU-4/A, HIGH TEMPERATURE |
| MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL C 38333 : 0 | CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
| MIL-W-50258 Revision A:1971 | WARHEAD SECTION, 762MM ROCKET, PRACTICE: M38 METAL PARTS FOR |
| MIL L 6484 : C | LIGHT, COCKPIT UTILITY, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-M-63394 Base Document:1980 | MINE, ANTI-TANK: HE, M75 METAL PARTS FOR |
| MIL-S-24317-12 Revision B:2006 | Switch, Multistation, Pushbutton, Illuminated Matrix Arrangement, Sunlight Readable, 4 Lamp, Plug-In Module, Style SM12L1 (No S/S Document) |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-B-8621 Revision A:1964 | Board, Chart, Mark 6A, Mark 6B and Mark 6C |
| NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| MIL-C-5191 Revision B:1953 | COMPUTER AND TRANSMITTER, TRUE AIRSPEED PITOT STATIC, TYPE A-2 |
| MIL-DTL-43695 Revision C:2000 | FRAME SECTIONS, TENT, FRAME TYPE, EXPANDABLE |
| MIL M 5388 : B | MACHMETER; PITOT STATIC OPERATED, RANGE 0.5 TO 1.5, TYPE A-2B |
| MIL-R-24243 Revision C:1987 | RIVET, BLIND, NON-STRUCTURAL, RETAINED MANDREL, GENERAL SPECIFICATION FOR |
| MIL-PRF-87937 Revision D:2001 | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
| MIL P 14458 : A NOTICE 1 | PAINT, RUBBER, RED FUMING NITRIC ACID RESISTANT |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-85049-94 Base Document:1993 | CONNECTOR ACCESSORIES, ELECTRICAL, MOUNTING DEVICE FLANGE TYPE, FULL MOUNTING PERIMETER DEVICE, TYPE I (HEAVY DUTY) |
| MIL F 14072 : D | FINISHES FOR GROUND BASED ELECTRONIC EQUIPMENT |
| MIL-B-50896 Base Document:1971 | BATTERY HOUSING, ASSEMBLY |
| MIL T 25627 : C | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
| MIL-C-53071 Base Document:1987 | COUPLING ASSEMBLIES, QUICK-DISCONNECT, SEXLESS TYPE |
| MIL-A-27391 Revision B:1963 | ALTIMETER, PRESSURE AAU-2A |
| MIL C 28754/22 : G | CONNECTOR, ELECTRICAL, MODULAR, FRAME, CASTING, TYPE 4, SINGLE SPAN |
| SAE AMS R 81835 : 2008 | REMOVER, ORGANIC COATING, HOT TANK TYPE |
| SAE AS 916 : 2016 | OXYGEN FLOW INDICATORS |
| SAE AS 5994A:2000(S2013) | PUMP UNITS, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY |
| PREN 6080 : 200P3 | AEROSPACE SERIES - RIVET, 100 DEGREES NORMAL FLUSH HEAD, CLOSE TOLERANCE - INCH SERIES |
| PREN 6081 : 200P2 | AEROSPACE SERIES - RIVET, UNIVERSAL HEAD, CLOSE TOLERANCE - INCH SERIES |
| PREN 6052 : 200P1 | AEROSPACE SERIES - RIVETS - COLLAR - SYSTEM IN ALUMINIUM ALLOY SHEAR TYPE INCH SERIES - TECHNICAL SPECIFICATION |
| MIL P 85582 : B | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| QQ-A-250-11 Revision F:1982 | ALUMINUM ALLOY 6061, PLATE AND SHEET |
| FED-STD-141 Revision D:2001 | PAINT, VARNISH, LACQUER AND RELATED MATERIALS, METHODS OF INSPECTION, SAMPLING AND TESTING |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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