SAE ARP 755 : 2014
|
AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION AND NOMENCLATURE
|
MS33540 Revision J:1986
|
SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
|
MS33787 Revision D:1984
|
WRENCHING ELEMENT, EXTERNAL SPLINE, DIMENSIONS FOR
|
MIL-E-5607 Revision F:1983
|
ENGINE, GAS TURBINE, PREPARATION FOR STORAGE AND SHIPMENT OF, PROCESS FOR
|
SAE ARP 1179 : 2011
|
AIRCRAFT GAS TURBINE ENGINE EXHAUST SMOKE MEASUREMENT
|
VV-F-800 Revision E:1987
|
FUEL OIL, DIESEL
|
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS
|
MIL-STD-130 Revision N:2007
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
|
MIL STD 2084 : 0
|
GENERAL REQUIREMENTS FOR MAINTAINABILITY OF AVIONIC AND ELECTRONIC SYSTEMS AND EQUIPMENT
|
MIL H 27267 : B
|
HOSE TETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE
|
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
|
MIL H 25579 : E
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
|
MIL C 85704 : B
|
CLEANING COMPOUND, TURBINE ENGINE GAS PATH
|
TIA 455-21 : A1988(R2012)
|
FOTP-21 MATING DURABILITY FOR FIBER OPTIC INTERCONNECTING DEVICES
|
MIL-E-6051 Revision D:1967
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
|
MS9006 Revision C:1963
|
RECESSES-CROSS, LOW TORQUE DRIVE, DIMENSIONS AND GAGE DIMENSIONS FOR
|
SAE AMS 2432 : 2013
|
SHOT PEENING, COMPUTER MONITORED
|
MIL-M-38510 Revision J:1991
|
MICROCIRCUITS, SPECIFICATION FOR
|
SAE AS 568 : 2014
|
AEROSPACE SIZE STANDARD FOR O-RINGS
|
SAE ARP 1256 : 2011
|
PROCEDURE FOR THE CONTINUOUS SAMPLING AND MEASUREMENT OF GASEOUS EMISSIONS FROM AIRCRAFT TURBINE ENGINES
|
MIL STD 470 : B
|
MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
|
MIL-STD-889 Revision C:2016
|
DISSIMILAR METALS
|
MIL E 5400 : T
|
ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
|
MIL-STD-1529 Base Document:1955
|
VENDOR SUBSTANTABLE FOR AEROSPACE PROPULSION SYSTEM ITEMS
|
MIL-STD-1815 Revision A:1983
|
|
MIL C 7024 : D
|
CALIBRATING FLUID, AIRCRAFT FUEL SYSTEM COMPONENTS
|
SAE AMS 2432 : 2013
|
SHOT PEENING, COMPUTER MONITORED
|
SAE AS 870 : 2015
|
WRENCHING CONFIGURATION, BI-HEXAGONAL (12 POINT) DRIVE, DESIGN STANDARD FOR
|
MIL C 38999 : J
|
CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS
|
MS33588 Revision E:1984
|
NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
|
TT-S-735 Revision A:1988
|
STANDARD TEST FLUIDS, HYDROCARBON
|
TIA 455-20 : B2004(R2013)
|
OPTICAL FIBRES - PART 1-46: MEASUREMENT METHODS AND TEST PROCEDURES - MONITORING OF CHANGES IN OPTICAL TRANSMITTANCE
|
MIL-F-17874 Revision B:1965
|
FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
|
MS33537 Revision E:1974
|
INSERT, SCREW THREAD, HELICAL COIL, COARSE AND FINE THREAD, STANDARD DIMENSIONS FOR
|
MIL-STD-1818 Revision A:1993
|
ELECTROMAGNETIC EFFECTS REQUIREMENTS FOR SYSTEMS
|
MIL-C-24621 Revision B:1991
|
COUPLER, PASSIVE, FIBER OPTIC, GENERAL SPECIFICATION FOR (METRIC)
|
MIL STD 1800 : A NOTICE 1
|
HUMAN ENGINEERING PERFORMANCE REQUIREMENTS FOR SYSTEMS
|
MIL-STD-882 Revision E:2012
|
System Safety
|
MIL-S-8879 Revision C:1991
|
SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
|
MIL-STD-471 Revision A:1973
|
MAINTAINABILITY DEMONSTRATION
|
MIL S 19500 : J
|
SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR
|
MIL-STD-100 Revision G:1997
|
ENGINEERING DRAWINGS
|
MIL-STD-1472 Revision G:2012
|
HUMAN ENGINEERING
|
SAE ARP 1420 : 2002
|
GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
|
MIL F 16884 : J
|
FUEL, NAVAL DISTILLATE
|
MIL-H-46855 Revision B:1979
|
HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT & FACILITIES
|
MIL C 85045 : E
|
CABLES, FIBER OPTICS, (METRIC), GENERAL SPECIFICATION FOR
|
SAE AS 681 : 2016
|
GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS
|
MIL-STD-721 Revision C:1981
|
DEFINITIONS OF EFFECTIVENESS TERMS FOR RELIABILITY MAINTAINABILITY, HUMAN FACTORS, AND SAFETY
|
MIL-STD-2173 Base Document:1986
|
RELIABILITY-CENTERED MAINTENANCE REQUIREMENTS FOR NAVAL AIRCRAFT, WEAPONS SYSTEMS AND SUPPORT EQUIPMENT
|
MIL-T-5544 Revision C:1991
|
THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM
|
MIL-STD-785 Revision B:1980
|
RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
|
MS33602 Base Document:1967
|
BOLT, SELF RETAINING AIRCRAFT RELIABILITY AND MAINTAINABILITY DESIGN AND USAGE REQUIREMENTS FOR
|