SAE AS 94900 : 2007
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
Superseded date
19-10-2019
Superseded by
Published date
01-01-2007
Publisher
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1. SCOPE
2. REFERENCES
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
Establishes general performance, design, test, development and quality assurance requirements for the Flight Control Systems of military piloted aircraft. Flight Control Systems (FCS) include all components used to transmit flight control commands from the pilot or other sources to appropriate force and moment producers.
| Committee |
A-6A3
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| DocumentType |
Standard
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| SAE ARP 94910 : 2012 | AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
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| SAE ARP 5812 : 2017 | ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
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| SAE ARP 5764 : 2013(R2018) | AEROSPACE ACTIVE INCEPTOR SYSTEMS FOR AIRCRAFT FLIGHT AND ENGINE CONTROLS |
| ASTM B 438/B438M : 2005 | Specification for Bronze Powder Metallurgy (P/M) Bearing (Oil-Impregnated) |
| MIL-A-8865 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
| MIL-DTL-18375H: 2005 | WIRE ROPE, FLEXIBLE, CORROSION-RESISTING, NONMAGNETIC, FOR AIRCRAFT CONTROL |
| MIL-PRF-7958 Revision D:2013 | PUSH-PULL CONTROLS, FLEXIBLE AND RIGID |
| MIL-I-8500 Revision D:1980 | INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| SAE AS 8976 : 2012 | BEARINGS, PLAIN, SELF-ALIGNING, ALL METAL, GENERAL SPECIFICATION FOR |
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| MS33736 Revision D:2002 | TURNBUCKLE ASSEMBLIES, CLIP LOCKING OF |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| SAE AS 81820 : 2014 | BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LOW SPEED OSCILLATION |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| IEEE 12207.1-1997 | IEEE/EIA Guide - Industry Implementation of International Standard ISO/IEC 12207 : 1995 (ISO/IEC 12207) - Software Life Cycle Processes - Life Cycle Data |
| MIL-DTL-781 Revision J:2014 | TERMINAL, WIRE ROPE SWAGING, GENERAL SPECIFICATION FOR |
| NASM33588:2010 | NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| SAE AS 7949 : 2004 | BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD |
| MIL-DTL-83420 Revision P:2017 | WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL-A-87229 Base Document:1985 | AUXILIARY POWER SYSTEMS, AIRBORNE |
| SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| MIL-DTL-6193 Revision E:2017 | JOINTS, UNIVERSAL, PLAIN, LIGHT AND HEAVY DUTY, GENERAL SPECIFICATION FOR |
| ISO 22072:2011 | Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications |
| MIL-A-8870 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE |
| SAE AMS A 22771 : 2012 | ALUMINUM ALLOY FORGINGS, HEAT TREATED |
| MIL-HDBK-781 Revision A:1996 | RELIABILITY TEST METHODS, PLANS, AND ENVIRONMENTS FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
| MIL-M-38510 Revision J:1991 | MICROCIRCUITS, SPECIFICATION FOR |
| SAE AS 5440 : 2011 | HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| SAE AS 6038 : 2011 | BEARINGS, BALL, BELLCRANK, ANTIFRICTION, AIRFRAME |
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| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| SAE AS 56761 : 1999 | SPLICING; CABLE TERMINAL, PROCESS FOR, AIRCRAFT |
| NASM33540:2003 | SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR |
| SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| MIL-DTL-6117 Revision L:2008 | WIRE ROPE ASSEMBLIES, AVIATION, SWAGED TYPE |
| SAE AMS STD 2175 : 1998 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| SAE AS 7997:1999 | MOTORS, AIRCRAFT HYDRAULIC, CONSTANT DISPLACEMENT - GENERAL SPECIFICATION FOR |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| MIL-STD-882 Revision E:2012 | System Safety |
| SAE AS 6039 : 2009 | BEARINGS, BALL, ROD END, DOUBLE ROW, SELF-ALIGNING |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| NASM33602:2011 | BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR |
| MIL-STD-203 Revision G:1991 | AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT |
| IEEE 12207.0-1996 | IEEE/EIA Standard - Industry Implementation of International Standard ISO/IEC 12207:1995 (ISO/IEC 12207) Standard for Information Technology -- Software Life Cycle Processes |
| MIL-STD-1773 Base Document:1988 | FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
| MIL-DTL-8878 Revision L:2014 | TURNBUCKLES, POSITIVE SAFETYING, GENERAL SPECIFICATION FOR |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-DTL-7034 Revision F:2005 | PULLEYS, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| FAA AC 120-29 : 0 | CRITERIA FOR APPROVAL OF CATEGORY 1 AND CATEGORY 2 WEATHER MINIMA FOR APPROACH |
| SAE ARP 4895 : 2006 | FLIGHT CONTROL ACTUATORS - DYNAMIC SEALS, COLLECTION OF DUTY CYCLE DATA |
| SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
| SAE AS 35411 : 2010 | FITTINGS, LUBRICATION |
| SAE ARP 988 : 2016 | ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
| MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
| SAE AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| NASM24665:2016 | PIN, COTTER (SPLIT) |
| SAE AMS F 7190 : 2016 | FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
| MIL-HDBK-838 Base Document:1997 | LUBRICATION OF MILITARY EQUIPMENT |
| SAE ARP 4386 : 2010 | TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
| ARINC 429 : 2001 | ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS |
| MIL-HDBK-470 Revision A:1997 | Designing and Developing Maintainable Products and Systems, Volume I |
| MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
| SAE ARP 4058 : 2007 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| NASM15981:2010 | FASTENERS, EXTERNALLY THREADED, SELF-LOCKING DESIGN AND USAGE LIMITATIONS FOR |
| SAE ARP 490 : 2008 | ELECTROHYDRAULIC SERVOVALVES |
| NAS 516:2015 | FITTING, LUBRICATION, .1250 INCH DRIVE, FLUSH TYPE |
| IEEE 12207.2-1997 | IEEE/EIA Guide - Industry Implementation of International Standard ISO/IEC 12207 : 1995 (ISO/IEC 12207) Standard for Information Technology- Software Life Cycle Processes - Implementation considerations |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| SAE AIR 1083 : 2012 | AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT |
| SAE AS 5643 : 2016 | IEEE-1394B INTERFACE REQUIREMENTS FOR MILITARY AND AEROSPACE VEHICLE APPLICATIONS |
| MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
| MIL-C-81774 Revision A:1973 | CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
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