DOD-C-24529 Base Document:1976
|
CHARGERS, BATTERY, LIFT TRUCK AND PALLET TRANSPORTER BATTERY SERVICE (METRIC) |
MIL-HDBK-2165 Base Document:1995
|
TESTABILITY PROGRAM FOR SYSTEMS AND EQUIPMENTS |
MIL-T-5842 Revision B:1985
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
MIL-R-38370 Revision B:1972
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
MIL-I-18856 Revision B:1969
|
INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
MIL-A-38307 Revision A:1981
|
ACCELEROMETER, AIRCRAFT, MX-6663/AJB-7 |
MIL-T-38034 Revision E:1970
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
MIL-HDBK-1785 Base Document:1995
|
SYSTEM SECURITY ENGINEERING PROGRAM MANAGEMENT REQUIREMENTS |
MIL-F-24291 Revision C:1990
|
FLOWMETER, FLUID ELECTROMAGNETIC TYPE |
MIL-HDBK-59 Revision B:1994
|
COMPUTER AIDED ACQUISITION AND LOGISTIC SUPPORT (CALS) PROGRAM IMPLEMENTATION GUIDE |
MIL L 24554 : 0
|
LAMPS MK III INTERFACE SIGNAL SWITCHING SET |
MIL-STD-1629 Revision A:1980
|
PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
MIL-HDBK-2084 Base Document:1995
|
GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT |
JSGS-87231 Revision A:1995
|
ENGINES, AIRCRAFT, TURBINE |
MIL-T-83460 Base Document:1975
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
MIL-I-38121 Revision C:1989
|
INDICATOR, PRESSURE, EGU-9/A |
MIL-STD-188-322 Base Document:1978
|
SUBSYSTEM DESIGN ENGINEERING AND EQUIPMENT TECHNICAL DESIGN STANDARDS FOR LONG HAUL LINE OF SIGHT (LOS) DIGITAL MICROWAVE RADIO TRANSMISSION |
DOD M 24614 : NOTICE 1
|
METERING SYSTEM, STORAGE BATTERY CURRENT AND AMPERE HOUR, DIGITAL (METRIC) |
MIL-STD-756 Revision B:1981
|
RELIABILITY MODELING AND PREDICTION |
MIL P 24765 : 0
|
POWER SUPPLY, UNINTERRUPTIBLE, STATIC |
MIL-A-85055 Base Document:1979
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
MIL-HDBK-11991 Base Document:1996
|
DESIGN OF ELECTRICAL, ELECTRONIC, AND ELECTRO-MECHANICAL EQUIPMENT, GUIDED MISSILE AND ASSOCIATED WEAPONS SYSTEMS |
MIL-A-29420 Base Document:1985
|
AMPLIFIER-CONVERTER: AM-6879/URC |
MIL-I-29589 Base Document:1991
|
INTERROGATOR SET, AN/UPX-24(V) |
MIL-STD-2069 Base Document:1961
|
REQUIREMENTS FOR AIRCRAFT NONNUCLEAR SURVIVABILITY PROGRAM |
MIL-T-27305 Revision C:1987
|
TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
MIL-STD-2124 Revision A:1984
|
FLIGHT INCIDENT RECORDER/CRASH POSITION LOCATOR, MINIMUM PERFORMANCE STANDARDS FOR |
IEEE 1887-2017
|
IEEE Guide for Wayside Energy Storage Systems for DC Traction Applications |
MIL-HDBK-2069 Base Document:1997
|
AIRCRAFT SURVIVABILITY |
MIL P 15736/6 : A NOTICE 2
|
POWER SUPPLY, GUIDED MISSILE & GUIDED MISSILE FIRE CONTROL SYSTEM SUPPORT |
MIL-T-26922 Revision D:1977
|
TEST SET, ELECTRICAL POWER A/M24T-8() |
MIL-P-6457 Revision E:1974
|
POWER SUPPLY, METALLIC RECTIFIER TYPE, GENERAL SPECIFICATION FOR |
MIL STD 2080 : 0
|
MAINTENANCE ENGINEERING, PLANNING AND ANALYSIS FOR AERONAUTICAL SYSTEMS, SUBSYSTEMS, EQUIPMENT AND SUPPORT EQUIPMENT |
MIL-I-38338 Revision D:1991
|
INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-C-85521 Base Document:1983
|
CONCENTRATOR, OXYGEN, GGU-7/A |
MIL-R-81876 Revision B:1988
|
RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
MIL-C-28779 Revision B:1972
|
COMBINER, EXTENDED FREQUENCY RANGE CU-2OO7 (/SRR) |
MIL-STD-2097 Revision A:1989
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL-HDBK-2155 Base Document:1995
|
FAILURE REPORTING, ANALYSIS AND CORRECTIVE ACTION TAKEN |
MIL-R-85111 Revision A:1980
|
RECOVERY ASSIST SECURING AND TRAVERSING SYSTEM FOR LAMPS MK 111 HELICOPTER |
MIL-P-85710 Base Document:1986
|
PARACHUTES, PERSONNEL, EMERGENCY ESCAPE GENERAL DESIGN SPECIFICATION FOR |
MIL-HDBK-2067 Base Document:1999
|
AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR |
MIL-STD-188-125 Revision A:1994
|
HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C41 FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS - VOLUME 1 - FIXED FACILITIES (METRIC) |
MIL-R-38435 Revision B:1968
|
RECORDING SET, SIGNAL DATA A/A 24U-6 |
MIL-T-81541 Base Document:1967
|
TEST SET, ELECTRONIC CIRCUIT PLUG-IN UNIT AN/ASM-152 |
MIL T 38170 : F
|
TANK, MOBILE STORAGE, LIQUID OXYGEN TMU 27/M |
MIL-C-0024196 Revision B:1991
|
CLEANING SYSTEMS, ULTRASONIC |
MIL-C-24196 Revision A:1988
|
CLEANING SYSTEM, ULTRASONIC |
MIL-STD-471 Revision A:1973
|
MAINTAINABILITY DEMONSTRATION |
MIL-D-81358 Revision B:1970
|
DISPLAY GROUP, TACTICAL DATA AN/ASA-66 |
MIL-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-A-49273 Base Document:1988
|
AMPLIFIER, POWER SUPPLY AM-7152/GRC-213 & ADAPTER KIT, VEHICLE MK-2154/GRC-213 |
MIL-T-26017 Revision C:1972
|
TEST STAND, HYDRAULIC SYSTEM COMPONENTS, TYPE MK-3A (STAND, TEST, AIRCRAFT HYDRAULIC SYSTEM, ELECTRIC MOTOR DRIVEN, TYPE MK-3A) |
MIL-S-87233 Base Document:1985
|
SUPPORT EQUIPMENT SYSTEMS (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-A-27471 Revision C:1993
|
ADAPTER, PRESSURE-REDUCER, IN-LINE CRU-43A/A |
MIL-T-29402 Base Document:1982
|
TEST SET TS 3354/PRC 68 |
MIL-C-9082 Revision H:1986
|
CONVERTER, OXYGEN, AIRCRAFT, LIQUID TO GASEOUS, GENERAL SPECIFICATION FOR |
MIL-F-24713 Base Document:1989
|
FREQUENCY CHANGER, STATIC, AIR COOLED (NAVAL SHIPBOARD) |
MIL-HDBK-2097 Revision A:1997
|
ACQUISITION OF SUPPORT EQUIPMENT AND ASSOCIATED INTEGRATED LOGISTICS SUPPORT |
MIL C 38271 : B
|
CONNECTOR, OXYGEN MASK TO REGULATOR CRU-60/P |
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
MIL-HDBK-87244 Base Document:1995
|
AVIONICS/ELECTRONICS INTEGRITY |
MIL-S-83129 Revision A:1972
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
MIL-D-8685 Revision B:1967
|
DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
MIL-T-81540 Base Document:1967
|
TEST SET, COMPUTER, WEAPONS RELEASE AN/ASM-150 |
MIL-M-24614 Revision A:1993
|
METERING SYSTEM, STORAGE BATTERY CURRENT & AMPERE HOUR, DIGITAL (METRIC, NONMERCURY TYPE) |
MIL-E-87235 Base Document:1985
|
EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-G-18473 Revision B:1978
|
GENERATOR, MOTOR, AND AUXILIARY EQUIPMENT, DIRECT CURRENT, NAVAL SHIP PROPULSION |
MIL-F-24259 Revision A:1987
|
FLUID FLOWMETER, VOLUME VELOCITY TYPE |
MIL-W-81560 Base Document:1967
|
WEAPON, BIOLOGICAL AND CHEMICAL GENERAL DESIGN SPECIFICATION FOR |
MIL-C-85518 Base Document:1984
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
MIL-R-22307 Revision D:1972
|
RADIAC SET AN/PDR-43() |
MIL-P-87210 Base Document:1984
|
PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
MIL-M-29460 Base Document:1990
|
MODULE, WATER PUMP (SIXCON) |
MIL-A-83216 Revision B:1976
|
AIR CONDITIONER A/E32C-39 |
MIL-T-28764 Base Document:1971
|
TEST SET, RADAR, AN/UPM-136 |
MIL-S-87241 Base Document:1985
|
SIMULATOR, FLIGHT (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-I-87216 Base Document:1984
|
INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-A-22523 Revision E:1968
|
ANALYZER-INDICATOR, DEAD RECKONING (DRAI) (NAVAL SHIPBOARD) |
MIL A 87221 : 0
|
AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-A-28988 Revision B:1982
|
AMPLIFIER, RADIO FREQUENCY, AM-6545/GRC-193 |
MIL-HDBK-2124 Base Document:2000
|
FLIGHT DATA RECORDER FUNCTIONAL STANDARDS FOR |
MIL-D-8804 Revision B:1993
|
DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-C-85248 Revision A:1984
|
CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
MIL-P-24568 Revision A:1986
|
POWER SUPPLY, D.C., FOR OXYGEN GENERATOR |
DEFSTAN 00-41/3(1993) : 1993
|
RELIABILITY AND MAINTAINABILITY MOD GUIDE TO PRACTICES AND PROCEDURES |
MIL-E-24762 Base Document:1991
|
ENCLOSURES FOR ELECTRONIC EQUIPMENT, SURVIVABLE, NAVAL SHIPBOARD USE |
MIL-G-81665 Base Document:1971
|
GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
MIL-I-21735 Revision A:1969
|
INDICATOR, AIRSPEED AND MACH NUMBER, PITOT STATIC, 6O TO 65O KNOTS |
MIL O 38338 : C (1)
|
OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
MIL-P-15736-7 Revision B:1982
|
POWER SUPPLY, METALLIC RECTIFIER GUIDED MISSILE FIRE CONTROL, NAVAL SHIPBOARD |
DOD-HDBK-791 Base Document:1988
|
MAINTAINABILITY DESIGN TECHNIQUES |
MIL-G-83380 Base Document:1979
|
GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
MIL-L-87139 Base Document:1979
|
LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-STD-2067 Base Document:1978
|
AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR |
JSSG-2010-12 Base Document:1998
|
Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
MIL-M-19160 Revision C:1970
|
MOTOR GENERATOR, 60 HZ AC TO 400 HZ AC SHIPBOARD SERVICE |
MIL-S-38399 Revision A:1975
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
MIL-I-38391 Base Document:1965
|
INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE) |
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
MIL-P-85573 Base Document:1983
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
MIL F 38363 : B (3)
|
FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-STD-001591 Revision A:1978
|
COMMAND, CONTROL AND COMMUNICATIONS (C3) SYSTEM AND COMPONENT FAULT DIAGNOSIS, SUBSYSTEMS, ANALYSIS/SYNTHESIS OF |
MIL-S-29354 Revision B:1986
|
SWITCHBOARD, TELEPHONE SB 3614/TT AUTOMATIC |
MIL-STD-188-200 Base Document:1983
|
SYSTEM DESIGN AND ENGINEERING STANDARDS FOR TACTICAL COMMUNICATIONS |
MIL-A-81403 Base Document:1967
|
ALTIMETER-ENCODER, AAU-21/A |
MIL-E-18927 Revision E:1983
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
MIL-R-23098 Revision A:1970
|
REGULATORS, LINE VOLTAGE, SINGLE PHASE. |
MIL-W-81752 Revision A:1987
|
WINDSHIELDED SYSTEM, FIXED WING AIRCRAFT - GENERAL SPECIFICATION FOR |
MIL-STD-1367 Revision A:1989
|
PACKAGING, HANDLING, STORAGE, AND TRANSPORTABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
MIL M 87222 : 0
|
MECHANICAL SYSTEMS FOR AIRCRAFT DOORS AND CANOPIES |
MIL-STD-2072 Base Document:1977
|
SURVIVABILITY, AIRCRAFT, ESTABLISHMENT AND CONDUCT OF PROGRAMS FOR |
MIL-D-81357 Revision A:1970
|
DISPLAY GROUP, TACTICAL DATA AN ASA 70 |
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
MIL-S-85018 Revision A:1978
|
SECOND ORDER ATTITUDE REFERENCE SYSTEM (SOARS) AN/ASN-116 |
MIL-T-24309 Base Document:1967
|
TECHNICAL SUPPORT PLAN FOR ELECTRONIC EQUIPMENT |
MIL-M-29417 Base Document:1984
|
MODULE, FUEL PUMP [SIXCON] |
MIL-A-27670 Revision D:1994
|
AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
MIL-F-24701 Base Document:1988
|
FLOWMETER, LIQUID, ULTRASONIC, NON-INTRUSIVE |
MIL-F-87154 Base Document:1980
|
FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-T-17221 Revision B:1973
|
TRANSFORMER, POWER, DISTRIBUTION, SINGLE PHASE, 400 HERTZ, INSULATION SYSTEM CLASS 220 DEGREES C, DRY (AIR COOLER), NAVAL SHIPBOARD USE) |
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL-D-18300 Revision H:1993
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
MIL STD 2084 : 0
|
GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT |
MIL-C-87970 Base Document:1982
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
MIL-P-28739 Base Document:1970
|
PEDESTAL GROUP, ANTENNA, FOR IFF ANTENNAS AN/UPA-57 |
MIL-P-24587 Base Document:1979
|
POWER SUPPLY, UNINTERRUPTIBLE, SOLID STATE (NAVAL SHIPBOARD) |
MIL-A-38140 Revision B:1977
|
ALTIMETER, PRESSURE AAU-16/A |
MIL-STD-1606 Revision A:1983
|
TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS |
MIL-P-23141 Revision D:1968
|
PLOTTING TABLE, ANTI SUBMARINE AND DEAD RECKONING (NAVAL SHIPBOARD) |
MIL-T-81821 Base Document:1969
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
MIL-STD-2155 Base Document:1985
|
FAILURE REPORTING, ANALYSIS AND CORRECTIVE ACTION SYSTEM |
MIL-STD-1390 Revision D:1993
|
LEVEL OF REPAIR ANALYSIS (LORA) |
SAE ARP 4943 : 2008
|
GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR |
SAE AIR 4004 : 2015
|
GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |