|
MIL-I-83294 Base Document:1971
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR
|
|
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)/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 BULL 343 : A
|
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
|
|
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)/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
|
|
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)/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
|
|
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
|
|
MIL-HDBK-244 Revision A:1990
|
GUIDE TO AIRCRAFT - STORES COMPATIBILITY
|
|
SAE AS 681 : 2016
|
GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS
|
|
FAA AC 33.28-3 : 2014
|
GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS
|
|
MIL-STD-3050 Base Document:2015
|
AIRCRAFT CREW BREATHING SYSTEMS USING ON-BOARD OXYGEN GENERATING SYSTEM (OBOGS)
|
|
FAA AC 35.23-1 : 2011
|
GUIDANCE MATERIAL FOR 14 CFR SECTION 35.23, PROPELLER CONTROL SYSTEM
|
|
MIL-C-0024196 Revision B:1991
|
CLEANING SYSTEMS, ULTRASONIC
|
|
MIL-C-24196 Revision A:1988
|
CLEANING SYSTEM, ULTRASONIC
|
|
SAE AIR 5867 : 2017
|
ASSESSMENT OF THE INLET/ENGINE TOTAL TEMPERATURE DISTORTION PROBLEM
|
|
MIL-B-9972 Revision B:1994
|
BRAZING, NICKEL, ALLOY, GENERAL SPECIFICATION FOR
|
|
MIL T 25920 : C
|
TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION
|
|
API 11PGT : 1992
|
RECOMMENDED PRACTICE FOR PACKAGED COMBUSTION GAS TURBINES
|
|
SAE ARP 5638 : 2005
|
RMS TERMS AND DEFINITIONS
|
|
SAE ARP 5757 : 2016
|
GUIDELINES FOR ENGINE COMPONENT TESTS
|
|
SAE AIR 4246 : 2012
|
CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING
|
|
MIL-S-38399 Revision A:1975
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR
|
|
SAE MAP 749 : 2015
|
AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)
|
|
FAA AC 33-2 : 2013
|
GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES
|
|
SAE ARP 1827C : 2014
|
MEASURING AIRCRAFT GAS TURBINE ENGINE FINE FUEL FILTER ELEMENT PERFORMANCE
|
|
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES
|
|
API 616 REDLINE : 2011
|
GAS TURBINES FOR THE PETROLEUM, CHEMICAL, AND GAS INDUSTRY SERVICES
|
|
API 616 : 2011
|
GAS TURBINES FOR THE PETROLEUM, CHEMICAL, AND GAS INDUSTRY SERVICES
|
|
SAE AIR 4023 : 2016
|
AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS
|
Important note : All end users must be registered with an Account prior to user licenses being assigned.