MIL-PRF-49316 Revision A:1997
|
TEST SET, ELECTRONIC SYSTEMS, TS-3895A/UV |
MIL R 29583 : 0
|
RADIO SET |
MIL PRF 62542 : B
|
BALL SCREW LINEAR ACTUATOR (BSLA) |
MIL-PRF-32080 Revision G:2014
|
TRUCK, AIRCRAFT FUELING-DEFUELING, 6,000 GALLON, A/S32R-11 |
GEIA TA HB 0009 : 2013
|
RELIABILITY PROGRAM HANDBOOK |
DEFSTAN 00-035(PT3)/5(2017) : 2017
|
ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS |
MIL-DTL-49198 Revision B:2014
|
HEADSET-MICROPHONE KIT, MK-1564( )/AIC |
MIL I 25863 : D
|
INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL P 24765 : 0
|
POWER SUPPLY, UNINTERRUPTIBLE, STATIC |
MIL P 49146 : B
|
POWER SUPPLY 18 MILLIMETER, MICROCHANNEL WAFER |
MIL-DTL-27188 Revision C:2006
|
INDICATOR, PRESSURE EGU-2/A, OIL, 0-100 PSI |
MIL-DTL-19803 Revision G:2007
|
CONVERTER, LIQUID OXYGEN, 10-LITER, GCU-24A/A |
MIL STD 750-3 : 0
|
TRANSISTOR ELECTRICAL TEST METHODS FOR SEMICONDUCTOR DEVICES - PART 3: TEST METHODS 3000 THROUGH 3999 |
MIL T 83823 : 0
|
TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
MIL-PRF-83419 Revision F:2016
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
MIL DTL 25949 : F
|
ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED |
MIL STD 883 : K
|
TEST METHOD STANDARD - MICROCIRCUITS |
BS EN 50155:2017
|
Railway applications. Rolling stock. Electronic equipment |
16/30282633 DC : 0
|
BS EN 50155 - RAILWAY APPLICATIONS - ELECTRONIC EQUIPMENT USED ON ROLLING STOCK |
EN 61124:2012
|
RELIABILITY TESTING - COMPLIANCE TESTS FOR CONSTANT FAILURE RATE AND CONSTANT FAILURE INTENSITY (IEC 61124:2012) |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-24151 Revision B:2016
|
DOORS, ROLLER CURTAIN AND HINGED SLAT, AND ASSOCIATED OPERATING EQUIPMENT |
DEFSTAN 00-970(PT0)/17(2016) : 2016
|
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)/15(2015) : 2015
|
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)/11(2013) : 2013
|
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 |
MIL-DTL-5099 Revision C:2011
|
INDICATOR, CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1 |
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL DTL 6162 : C
|
GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
MIL P 49452 : 0
|
POWER SUPPLY 18 MM, MICROCHANNEL WAFER, GEN III, MX-10130()/UV |
MIL E 29581 : 0
|
EARCUP, UNIT ACTIVE NOISE REDUCTION SYSTEM |
MIL-DTL-25867 Revision D:2006
|
GAGE, PRESSURE, DIAL INDICATING, PNEUMATIC |
MIL-PRF-49404 Revision A:1997
|
BIAS VOLTAGE REGULATOR, CN-1559/UA |
MIL-DTL-24765 Revision B:2016
|
POWER SUPPLY, UNINTERRUPTIBLE, STATIC (NAVAL SHIPBOARD) |
MIL-PRF-49434 Revision A:1997
|
AIMING LIGHT, INFRARED, AN/PAQ-4C |
MIL-A-24233 Revision B:1989
|
ANTENNA, AS-1735( )/SRC |
IEEE 1332-2012
|
IEEE Standard Reliability Program for the Development and Production of Electronic Products |
MIL F 51536 : 0
|
FILTER UNIT, GAS-PARTICULATE, 200 CFM, 208V, 400 HZ, M56 |
MIL PRF 49177 : B
|
SCAN-INTERLACE, PL-1408/UA |
MIL-DTL-38195 Revision D:2000
|
GENERATOR SET, GAS TURBINE ENGINE, 60 KW 400 HZ, GENERAL PURPOSE |
MIL DTL 52872 : D
|
SENSOR GROUP, ULTRASONIC MOTION: TRANSCEIVER RT-1161/FSS-9(V) AND PROCESSOR MX-9444/FSS-9(V) |
MIL F 24713 : 0
|
FREQUENCY CHANGER, STATIC, AIR COOLED (NAVAL SHIPBOARD) |
DEFSTAN 00-42(PT7)/1(2014) : 2014
|
RELIABILITY AND MAINTAINABILITY - PART 7: RELIABILITY TESTING |
MIL DTL 25469 : J
|
VALVES, FILLER, LIQUID OXYGEN, AIRCRAFT TYPE |
SAE ARP 81490 : 2016
|
TRANSMISSION LINES, TRANSVERSE ELECTROMAGNETIC MODE |
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
I.S. EN 50155:2017-11
|
RAILWAY APPLICATIONS - ROLLING STOCK - ELECTRONIC EQUIPMENT |
MIL HDBK 115 : C
|
U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
MIL PRF 38230 : D
|
TRANSMITTER, PRESSURE, OIL, VARIABLE RELUCTANCE |
MIL-DTL-52876 Revision D:1997
|
CABINETS, MONITOR, CY-7359/FSS-9(V) CY-7360/FSS-9(V), AND CY-7361/FSS-9(V) |
MIL A 28865 : A
|
ANTENNA GROUP, OE-82()/WSC-1(V) |
MIL-PRF-26139 Revision E:2015
|
TESTER, PRESSURIZED CABIN LEAKAGE, AIRCRAFT, (AF/M24T-3 AND AF/M32T-1) |
IEEE 1633 : 2016
|
SOFTWARE RELIABILITY |
MIL HDBK 338 : B
|
ELECTRONIC RELIABILITY DESIGN HANDBOOK |
MIL-DTL-16392 Revision D:2015
|
BRAKE, ELECTRO-MECHANICAL, NAVAL SHIPBOARD |
MIL PRF 49293 : B
|
RADIAC SET, AN/PDR-75 |
MIL PRF 49168 : C
|
SCAN-INTERLACE, PL-1403/UA, PL-1403A/UA |
ABS 0272 : 2017
|
GUIDANCE NOTES ON QUALIFYING NEW TECHNOLOGIES |
DEFSTAN 00-41/3(1993) : 1993
|
RELIABILITY AND MAINTAINABILITY MOD GUIDE TO PRACTICES AND PROCEDURES |
MIL-DTL-25308 Revision C:2010
|
GAGE, PRESSURE, DIAL INDICATING, HYDRAULIC, TYPE ME-1 |
SAE AS 19692 : 2016
|
AEROSPACE - MILITARY TYPE VARIABLE DELIVERY, PRESSURE COMPENSATED HYDRAULIC PUMP |
SAE AIR 1277 : 2005
|
COOLING OF MILITARY AVIONIC EQUIPMENT |
IEC TR 62866:2014
|
Electrochemical migration in printed wiring boards and assemblies - Mechanisms and testing |
MIL-STD-750-1 Revision A:2015
|
ENVIRONMENTAL TEST METHODS FOR SEMICONDUCTOR DEVICES - PART 1: TEST METHODS 1000 THROUGH 1999 |
EN 50155:2017
|
Railway applications - Rolling stock - Electronic equipment |
MIL-HDBK-344 Revision A:1993
|
ENVIRONMENTAL STRESS SCREENING (ESS) OF ELECTRONIC EQUIPMENT |
MIL-DTL-38394 Revision E:2009
|
TRANSMITTER, PRESSURE TRU-81/A, OIL, 0-500 PSI |
MIL PRF 49163 : B
|
VIDEO PREAMPLIFIER, AM-6923/UA |
MIL HDBK 2164 : A
|
ENVIRONMENTAL STRESS SCREENING PROCESS FOR ELECTRONIC EQUIPMENT |
MIL-PRF-49318 Revision A:1997
|
TEST SET, ELECTRONIC SYSTEMS, TS-4348/UV |
UNE-EN 61124:2014
|
Reliability testing - Compliance tests for constant failure rate and constant failure intensity |
DEFSTAN 00-35(PT3)/4(2006) : 2006
|
ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS |
CEI EN 61124 : 2013
|
RELIABILITY TESTING - COMPLIANCE TESTS FOR CONSTANT FAILURE RATE AND CONSTANT FAILURE INTENSITY |
MIL-DTL-5882 Revision E:2013
|
TRANSMITTER, PRESSURE, MULTIPURPOSE, 0-50 PSI, MS28005-1 |
DEFSTAN 00-40(PT7)/1(2003) : 2003
|
RELIABILITY AND MAINTAINABILITY (R&M) - PART 7: (ARMP-7) NATO R&M TERMINOLOGY APPLICABLE TO ARMP'S |
MIL-DTL-5790 Revision H:2008
|
TRANSMITTER, PRESSURE, OIL, SYNCHRO, 0-200 PSI 320-DEGREE MOVEMENT, 26 V, SINGLE PHASE, 400 CYCLES |
MIL A 52879 : C
|
ALARM, AUDIBLE, BZ-204/FSS-9(V) |
MIL-DTL-7627 Revision G:2010
|
INDICATOR, TURN AND SLIP, 28 V DC |
MIL DTL 52869 : C
|
SENSOR GROUP, PASSIVE ULTRASONIC: RECEIVER R-1860/FSS-9(V) AND PROCESSOR MX-9443/FSS-9(V) |
ADS-63-SP : 2001
|
AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS |
MIL-PRF-49185 Revision B:1997
|
RADIO SET AN/GRC-103(V)3 |
RE.AERO 70306 : 2001
|
GUIDELINES FOR RELIABILITY GROWTH CONTROL |
MIL PRF 52955 : D
|
IMPROVED POSITION AND AZIMUTH DETERMINING SYSTEM (IPADS) |
MIL F 51544 : A
|
FILTER UNIT, GAS-PARTICULATE, 200 CFM, 208 VAC, M84 |
MIL A 0083216 : C
|
AIR CONDITIONER, HORIZONTAL, 54,000 BTUH, 208/230 V |
MIL-DTL-27189 Revision E:2008
|
INDICATOR, PRESSURE, OIL |
I.S. EN 61124:2012
|
RELIABILITY TESTING - COMPLIANCE TESTS FOR CONSTANT FAILURE RATE AND CONSTANT FAILURE INTENSITY |
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
PD IEC/TR 62866:2014
|
Electrochemical migration in printed wiring boards and assemblies. Mechanisms and testing |
IEC 61124:2012
|
Reliability testing - Compliance tests for constant failure rate and constant failure intensity |
MIL-DTL-9398 Revision D:2007
|
GENERATOR, TACHOMETER, TWO-POLE, HIGH TEMPERATURE, AIRCRAFT |
ARMP-7 : 2008
|
NATO R&M TERMINOLOGY APPLICABLE TO ARMPS |
AECTP-400 : 2006
|
MECHANICAL ENVIRONMENTAL TESTS |
10/30238858 DC : 0
|
BS EN 62506 - METHODS FOR PRODUCT ACCELERATED TESTING |
SAE ARP 6461 : 2013
|
GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
MIL A 53129 : 0
|
ALARM-MONITOR GROUP OA-9431/FSS-9(V) |
MIL-DTL-24347 Revision C:2015
|
MONITOR, AVAILABLE LOAD, 60 AND 400 HERTZ, A.C., 1 PHASE, ELECTRICAL POWER (NAVAL SHIPBOARD USE) |
MIL B 62542 : A
|
BALL SCREW LINEAR ACTUATOR |
MIL P 49090 : D
|
POWER SUPPLY 25 MILLIMETER, MICROCHANNEL INVERTER |
MIL L 85314 : A
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
MIL-O-52374 Revision E:2013
|
OSCILLATOR: HIGH VOLTAGE, GENERAL SPECIFICATION FOR |
MIL T 23752 : E
|
TRITIUM AIR MONITOR, PORTABLE OR FIXED |
ADS-65-HDBK : 2004
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
MIL A 29521 : 0
|
ANTENNA GROUP, AN/BRA-34(V), AN/BRA-34A(V), AN/BRA-34B(V) |
MIL C 85283 : B
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-9 |
MIL-DTL-27190 Revision C:2006
|
INDICATOR, PRESSURE AGU-3/A, HYDRAULIC, 0-4,000 PSI |
RE.AERO 70305 : A2000
|
GUIDE FOR RELIABILITY CONTROL |
MIL STD 781 : D
|
RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
MIL T 49318 : 1991-11-21
|
TEST SET, ELECTRONIC SYSTEMS |
MIL-PRF-49320 Revision A:1997
|
LASER INFRARED OBSERVATION SET, AN/PVS-6 |
BS EN 61124:2012
|
Reliability testing. Compliance tests for constant failure rate and constant failure intensity |