MIL-STD-202-211 Base Document:2015
|
METHOD 211, TERMINAL STRENGTH |
SAE AMS 1424 : 2016
|
FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1 |
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
MIL-STD-202-302 Base Document:2015
|
METHOD 302, INSULATION RESISTANCE |
MIL-DTL-5624 Revision W:2016
|
TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
MIL-STD-883 Revision K:2016
|
TEST METHOD STANDARD - MICROCIRCUITS |
MIL-STD-202-109 Base Document:2015
|
METHOD 109, EXPLOSION |
MIL-PRF-7808 Revision L:1997
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
ANSI/NCSL Z540 3 : 2006(R2013)
|
REQUIREMENTS FOR THE CALIBRATION OF MEASURING AND TEST EQUIPMENT |
MIL-PRF-5606 Revision H:2002
|
HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
MIL-PRF-19500 Revision P:2010
|
SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR |
MIL-PRF-87937 Revision D:2001
|
CLEANING COMPOUND, AEROSPACE EQUIPMENT |
MIL-STD-202-101 Base Document:2015
|
METHOD 101, SALT ATMOSPHERE (CORROSION) |
MIL-STD-202-107 Base Document:2015
|
METHOD 107, THERMAL SHOCK |
MIL-HDBK-454 Revision B:2007
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
MIL-STD-202-106 Base Document:2015
|
METHOD 106, MOISTURE RESISTANCE |
MIL-STD-202-301 Base Document:2015
|
METHOD 301, DIELECTRIC WITHSTANDING VOLTAGE |
MIL-STD-202-215 Base Document:2015
|
METHOD 215, RESISTANCE TO SOLVENTS |
MIL-PRF-23699 Revision G:2014
|
Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167 |
SAE AS 81714 : 2014
|
TERMINAL JUNCTION SYSTEM (TJS), ENVIRONMENT RESISTANT, GENERAL SPECIFICATION FOR |
MIL-STD-461 Revision G:2015
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
MIL-PRF-83383-4 Revision G:2017
|
CIRCUIT BREAKERS, REMOTE CONTROL, AC-DC, THERMAL, TRIP-FREE, SERIES TRIP, TRIPLE POLE, AUXILIARY CONTACTS (5 TO 100 AMPERES) |
MIL-PRF-83383-1 Revision G:2016
|
CIRCUIT BREAKERS, REMOTE CONTROL, AC-DC, THERMAL, TRIP-FREE, SERIES TRIP, SINGLE POLE, (5 TO 100 AMPERES) |
SAE AS 39029/1 : 2014
|
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR AS81714 TERMINAL JUNCTION SYSTEM) |
SAE AS 1241 : 2016
|
FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
MIL-PRF-83282 Revision D:1997
|
HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
MIL-STD-202-310 Base Document:2015
|
METHOD 310, CONTACT-CHATTER MONITORING |
MIL-STD-202-110 Base Document:2015
|
METHOD 110, SAND AND DUST |
MIL-PRF-38535 Revision K:2013
|
Integrated Circuits (Microcircuits) Manufacturing, General Specification for |
MIL-STD-202 Revision H:2015
|
ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
MIL-STD-1285 Revision D:2004
|
MARKING OF ELECTRICAL AND ELECTRONIC PARTS |
FED-STD-H28 Revision A:1994
|
Screw-Thread Standards for Federal Services |
ISO 10012-1:1992
|
Quality assurance requirements for measuring equipment Part 1: Metrological confirmation system for measuring equipment |
MIL-STD-202-204 Base Document:2015
|
METHOD 204, VIBRATION, HIGH FREQUENCY |
MIL-PRF-83383-2 Revision G:2016
|
CIRCUIT BREAKERS, REMOTE CONTROL, AC-DC, THERMAL, TRIP-FREE, SERIES TRIP, SINGLE POLE, AUXILIARY CONTACTS (5 TO 100 AMPERES) |
MIL-STD-202-213 Base Document:2015
|
METHOD 213, SHOCK (SPECIFIED PULSE) |