MIL-PRF-32080 Revision G:2014
|
TRUCK, AIRCRAFT FUELING-DEFUELING, 6,000 GALLON, A/S32R-11 |
GEIA TA HB 0009 : 2013
|
RELIABILITY PROGRAM HANDBOOK |
MIL-PRF-85676 Revision A:2006
|
LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
MIL-DTL-32529 Base Document:2015
|
POWER ELECTRONIC CONVERSION EQUIPMENT, NAVAL SHIPBOARD |
MIL-PRF-32272 Revision A:2016
|
INTEGRATED POWER MANAGEMENT CENTER (IPMC) |
MIL-PRF-83419 Revision F:2016
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
SAE ARP 5120 : 2016
|
AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-PRF-17773 Revision D:2015
|
SWITCH, BUS TRANSFER, ELECTRIC POWER, AUTOMATIC |
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)/7(2011) : 2011
|
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 |
MIL-DTL-32483 Base Document:2013
|
Switchgear, Power, Hard-Mounted, Medium Voltage, Naval Shipboard |
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)/11(2013) : 2013
|
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 |
MIL-DTL-22263 Revision C:2009
|
COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-16036 Revision M:2013
|
SWITCHGEAR, POWER, LOW VOLTAGE, NAVAL SHIPBOARD |
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-24299 Revision B:2017
|
HEATERS, LUBRICATING OIL AND FUEL, ELECTRIC, NAVAL SHIPBOARD |
AFGS-87219 Revision B:2012
|
ELECTRICAL POWER SYSTEMS, AIRCRAFT |
MIL-DTL-24765 Revision B:2016
|
POWER SUPPLY, UNINTERRUPTIBLE, STATIC (NAVAL SHIPBOARD) |
GEIA HEB 1 : 2005
|
HUMAN ENGINEERING - PRINCIPLES AND PRACTICES |
MIL-DTL-38195 Revision D:2000
|
GENERATOR SET, GAS TURBINE ENGINE, 60 KW 400 HZ, GENERAL PURPOSE |
MIL-DTL-32572 Base Document:2017
|
Anchor Windlass, Electro-Mechanical, Vertical, Two-Speedand Variable-Speed |
SAE JA 1010 : 2011
|
MAINTAINABILITY PROGRAM STANDARD |
MIL-DTL-85061 Revision C:2009
|
COUPLING, FUEL LINE, FLEXIBLE, 125 PSI |
MIL-HDBK-115 Revision C:2016
|
U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
MIL-HDBK-516 Revision C:2014
|
AIRWORTHINESS CERTIFICATION CRITERIA |
MIL-HDBK-502 Revision A:2013
|
Product Support Analysis |
MIL-PRF-26139 Revision E:2015
|
TESTER, PRESSURIZED CABIN LEAKAGE, AIRCRAFT, (AF/M24T-3 AND AF/M32T-1) |
MIL-DTL-18110 Revision G:2018
|
VALVES, GATE TYPE, STEEL SIZES 2[1/2] INCHES TO 16 INCHES |
MIL-HDBK-338 Revision B:1998
|
ELECTRONIC RELIABILITY DESIGN HANDBOOK |
SAE J 1776 : 2014
|
MARINE VEHICLES - HYDRAULIC SYSTEM PUMPS AND MOTORS - DESIGN AND SPECIFICATION GUIDE |
SAE AIR 5416 : 2016
|
MAINTENANCE LIFE CYCLE COST MODEL |
MIL-DTL-16392 Revision D:2015
|
BRAKE, ELECTRO-MECHANICAL, NAVAL SHIPBOARD |
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL-DTL-53078 Revision A:2011
|
MOUNTING KIT: M1 TANK CLEARED LANE MARKING SYSTEM (CLAMS) |
CSA N290.8 : 2015
|
TECHNICAL SPECIFICATION REQUIREMENTS FOR NUCLEAR POWER PLANT COMPONENTS |
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
JSSG-2010-12 Base Document:1998
|
Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
SAE AS 5356 : 2017
|
COUPLING, FUEL LINE, FLEXIBLE, 125 PSI GENERAL SPECIFICATION FOR |
MIL-DTL-24347 Revision C:2015
|
MONITOR, AVAILABLE LOAD, 60 AND 400 HERTZ, A.C., 1 PHASE, ELECTRICAL POWER (NAVAL SHIPBOARD USE) |