MIL-STD-250 Revision D:1974
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
AIRCREW STATION CONTROLS AND DISPLAYS FOR ROTARY WING AIRCRAFT
05-12-1995
Important note : Users cannot be edited or removed once added to your Multi user PDF.Covers requirements applying to the design of aircrew stations in rotary wing aircraft procured by military departments. Described are the requirements for the arrangement, assignment, actuation and location of crew station controls, and related items of equipment; color and configuration of particular controls; the relative location of various displays which include the engine instrument and basic flight groups.
| DocumentType |
Standard
|
| Pages |
52
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
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| MIL-T-5842 Revision B:1985 | TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
| MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
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| DEFSTAN 00-970(PT0)/14(2014) : 2014 | 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)/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 |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-M-18012 Revision B:1964 | MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-HDBK-759 Revision C:1995 | HANDBOOK FOR HUMAN ENGINEERING DESIGN GUIDELINES |
| MIL-E-22285 Base Document:1959 | EXTINGUISHING SYSTEM, FIRE, AIRCRAFT, HIGH-RATE DISCHARGE TYPE, INSTALLATION AND TEST OF |
| MIL-D-23222 Revision A:1971 | DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
| NASA STD 3000 VOL 2 : 1995 | MAN-SYSTEMS INTEGRATION STANDARDS - VOLUME 2 |
| MIL-STD-1333 Revision B:1987 | AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT |
| MIL-C-81774 Revision A:1973 | CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| STANAG 3950 : 0 | HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
| MS33634 Revision A:1970 | INSTRUMENT, ENGINE, BASIC, STANDARD ARRANGEMENT OF |
| MIL-STD-1333 Revision B:1987 | AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT |
| MIL S 8805 : D | SWITCHES, AND SWITCH ASSEMBLIES, SENSITIVE AND PUSH, SNAP ACTION, GENERAL SPECIFICATION FOR |
| MIL-M-18012 Revision B:1964 | MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF |
| MIL-S-9487 Revision C:1985 | SWITCH, TRIGGER, SINGLE POLE, TWO STAGE, MOMENTARY |
| MIL-STD-802 Base Document:1970 | NUMBER, AIRCRAFT ENGINES AND ENGINE CYLINDERS, COMBUSTION CHAMBERS FLAME TUBES, INNER LINERS, AND SIMILAR ITEMS |
| MIL-STD-411 Revision F:1997 | AIRCREW STATION ALERTING SYSTEMS |
| MIL-L-18276 Revision C:1964 | LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
| MS26523 Base Document:1972 | HANDLE CONTROL, AIRCRAFT, FIRE EXTINGUISHER |
| MIL S 22885 : E | SWITCH, PUSH BUTTON, ILLUMINATED, GENERAL SPECIFICATION FOR |
| MIL-C-7188 Base Document:1951 | Compasses, Pilot\'s Standby, Installation of |
| MIL-STD-783 Revision D:1984 | LEGENDS FOR USE IN AIRCREW STATIONS AND ON AIRBORNE EQUIPMENT |
| MIL S 3950 : F | SWITCH, TOGGLE ENVIRONMENTALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-H-46855 Revision B:1979 | HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT & FACILITIES |
| MS26521 Revision A:1969 | HANDLE, CONTROL, AIRCRAFT LANDING GEAR |
| MS33785 Revision A:1970 | INSTRUMENT ARRANGEMENT, STANDARD, BASIC FOR FIXED AND ROTARY WING AIRCRAFT |
| MIL A 25165 : B NOTICE 1 | AIRCRAFT EMERGENCY ESCAPE SYSTEM, IDENTIFICATION OF |
| MIL-C-81774 Revision A:1973 | CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
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