|
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
|
RTCA DO 178 : C2011
|
SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
|
SAE AMS QQ P 416 : 2016
|
PLATING, CADMIUM (ELECTRODEPOSITED) |
|
MIL STD 704 : F
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
|
ARINC 600 : 1977 SUPP 20
|
AIR TRANSPORT AVIONICS EQUIPMENT INTERFACES |
|
MIL STD 130 : N
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
|
IEEE 12207.1 : 1997
|
INDUSTRY IMPLEMENTATION OF INTERNATIONAL STANDARD ISO/IEC 12207:1995 (ISO/IEC 12207) STANDARD FOR INFORMATION TECHNOLOGY - SOFTWARE LIFE CYCLE PROCESSES - LIFE CYCLE DATA |
|
MIL STD 810 : G
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
SAE ARP 4955 A: 2012(R2018)
|
RECOMMENDED PRACTICE FOR MEASUREMENT OF STATIC AND DYNAMIC CHARACTERISTIC PROPERTIES OF AIRCRAFT TIRES |
|
SAE ARP 4754 : 2010
|
GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
|
NAS 1638 : 0
|
CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS |
|
SAE AIR 1739 : 2016
|
INFORMATION ON ANTISKID SYSTEMS |
|
ARINC 629 : 90 SUPP 5
|
MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION |
|
RTCA DO 254 : 2000
|
DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
|
FAA AC 20-152 : 2005
|
RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
|
MIL HDBK 454 : B
|
GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
|
ARINC 604 : 1985 SUPP 1
|
GUIDANCE FOR DESIGN AND USE OF BUILT-IN TEST EQUIPMENT (BITE) |
|
FAA AC 23-8 : 2011
|
FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
|
SAE ARP 4761 : 1996
|
GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
|
SAE AS 22759 : 2014
|
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY |
|
(INACTIVE RECORD)RTCA DO 160 : G2010 CHG 1 2014
|
ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT |
|
MIL PRF 81322 : G
|
GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395 |
|
MIL STD 1568 : D
|
MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
|
MIL HDBK 5400 : 0
|
ELECTRONIC EQUIPMENT, AIRBORNE GENERAL GUIDELINES FOR |
|
MIL HDBK 217 : F
|
RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
|
MIL STD 882 : E
|
STANDARD PRACTICE FOR SYSTEM SAFETY |
|
MIL STD 461 : G
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
|
IEEE 12207.0 : 1996
|
INTERNATIONAL STANDARD ISO/IEC 12207:1995 (ISO/IEC 12207) STANDARD FOR INFORMATION TECHNOLOGY - SOFTWARE LIFE CYCLE PROCESSES |
|
RTCA DO 248 : C2011
|
SUPPORTING INFORMATION FOR DO-178C AND DO-278A |
|
ASME Y14.100 : 2017
|
ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
|
SAE AS 8775 : 1998
|
HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
|
SAE ARP 598 : 2016
|
AEROSPACE MICROSCOPIC SIZING AND COUNTING OF PARTICULATE CONTAMINATION FOR FLUID POWER SYSTEMS |
|
MIL DTL 26500 : G
|
CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING OR HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
FAA AC 25-7 : 2012
|
FLIGHT TEST GUIDE FOR CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES |
|
SAE ARP 490 : 2008
|
ELECTROHYDRAULIC SERVOVALVES |
|
MIL P 8564 : D
|
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
|
IEEE 12207.2 : 1997
|
|
|
MIL W 5088 : L
|
WIRING, AEROSPACE VEHICLE |
|
FAA AC 121.195-1 : 0
|
OPERATIONAL LANDING DISTANCES FOR WET RUNWAYS; TRANSPORT CATEGORY AIRPLANES |
|
ASME Y14.24 : 2012
|
TYPES AND APPLICATIONS OF ENGINEERING DRAWINGS - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |