1、MILSTD-203G1 MARCH 1991SUPERSEDINGMILSTD203F28 DECEMBER 1973MILITARY STANDARDAIRCREW STATION CONTROLSAND DISPLAYS: LOCATION, ARRANGEMENTAND ACTUATION OF, FOR FIXED WING AIRCRAFTAMSC N/A FSC 1510DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.Provided by IHSNot for Re
2、saleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-203GFOREWORD1. This military standard is approved for use by all Departments andAgencies of the Department of Defense.2. Beneficial comments (recommendations, additions, deletions) and anypertinent data shich may be of
3、use in improving this document should beaddressed to: Systems Engineering and Standardization Department (Code 53),Naval Air Engineering Center, Lakehurst, NJ 08733-5100, by using theself-addressed Standardization Document Improvement Proposal (DD Form 1426)appearing at the end of this document or b
4、y letter.3. At their 98th Meeting in July 1984 the Aircrew Station StandardizationPanel (ASSP) formed an ad-hoc to revise MIL-STD-203F to incorporate newtechnology requirements. Some major changes include revising the scope ofMIL-STD-203 to include the location, arrangement, and actuation of control
5、s anddisplays- rather than the assignment of controls and displays in fixed wingaircraft. The requirements for the specific location and arrangement oftransilluminated dedicated signal displays were incorporated in MIL-STD-203after deletion from MIL-STD-411RE, Aircrew Station Systems.Definitions wer
6、e revised to coincide with associated documents such asMIL-STD-1333 Aircrew Station Geometry for Military Aircraft among others.Detailed figures of specific type cockpit arrangements were added for guidance.iiProvided by IHSNot for ResaleNo reproduction or networking permitted without license from I
7、HS-,-,-MIL-STD-203GCONTENTSPARAGRAPH1.1.11.22.2.12.1.12.23.3.13.23.2.13.2.23.2.33.2.43.33.3.13.43.4.13.4.23.4.33.4.43.4.53.53.5.13.5.1.13.5.23.5.33.5.43.5.53.63.73.7.13.7.23.7.33.83.93.9.13.9.24.4.4.24.34.3.14.3.2SCOPE Scope Applicability APPLICABLE DOCUMENTS Government documents Specifications, sta
8、ndards and handbooks .Order of precedence .DEFINITIONS Fixed wing aircraft Types of aircrew stations Single pilot .Dual pilot .Multiple Non-standard flight crew stations .Geometry and clearanceClearance Controls Primary controls .Alternate controls Emergency controls .Primary flight controls .Power
9、plant controls Display Signal .Visual displayed information Generated graphics Primary displays Primary flight displays Power plant displays .Attention getting device Control and switch actuation .Position related Performance related .Single action Military power.Interior vision Cone of vision Desig
10、n eye position GENERAL REQUIREMENTS General Arrangement of controls and displays .Location of controls and displays Flight critical controls Flight essential controls PAGE11111122222233333333333334444444444555666666iiiProvided by IHSNot for ResaleNo reproduction or networking permitted without licen
11、se from IHS-,-,-MIL-STD-203GPARAGRAPH4.3.34.3.44.3.54.44.54.64.74.84.94.9.14.9.24.104.10.14.10.24.10.2.14.10.2.24.10.34.10.44.10.54.114.125.5.15.1.15.1.25.1.35.1.45.1.55.1.65.1.75.1.85.1.9CONTENTSMission critical controls .Mission essential controls Other controls Location .Assignment of controls to
12、 crew members .Actuation of controls .Other aircrew stations .Interior vision Displayed information .Integrally illuminated control and informationpanels and switches Instructional panels, legends, emergency markings,signals Control knobs, handles, and switches .Emergency control markings Control mo
13、nitoring Remote and indirect control monitoring .Direct control monitoring .Control guards MarkingControl coding.Ground maintenance controls and displays .Cockpit equipment arrangement .5.1.9.15.1.9.25.1.105.1.115.1.125.1.135.1.145.1.14.15.1.14.25.1.14.3DETAILED REQUIREMENTS Flight and ground contro
14、ls .Foot actuated rudder control Rudder pedal adjustment control .Roll control Pitch control .Surface augmentation control Flight control lock .Automatic flight controls (auto-pilot) Trim controls (yaw, pitch, roll) .Landing gear control .Emergency retraction control Alternate landing gear extension
15、 control .Landing gear position indicator(s) .Landing flap control .Landing flap position indicator Speed brake control Arresting hook control.Normal system operation Emergency system operation Emergency arresting hook control PAGE66667777777889999999910 10 10 10 10 10 10 10 10 11 12 12 12 12 12 12
16、13 13 13 13 13 ivProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-PARAGRAPH5.1.155.1.165.1.175.1.185.1.18.15.1.18.25.1.18.35.1.18.45.1.195.1.205.1.215.1.225.1.235.1.245.25.2.15.2.1.15.2.1.25.2.1.35.2.25.2.2.15.2.2.25.2.35.2.45.2.55.2.65.2.75.2.7.15.2.
17、7.25.2.7.35.2.7.45.2.85.2.95.2.105.2.115.2.11.15.2.11.25.2.125.2.135.2.13.15.2.13.25.2.145.2.14.15.2.14.25.2.14.3MIL-STD-203GCONTENTSPAGEWing folding controlWing locking controlWing sweep control Brake controlWheel brake controlParking brake controlEmergency brakeAnti-SkidCanopy control (sliding or
18、hinged)Canopy jettison controlNose wheel steering controlDrag chute controlCatapult (hand grip)/strut stiff controlLaunch bar controlPower plant controlsPower controlsReciprocating enginesTurboprop enginesTurbojet, enginesReverse thrust controlShaft power enginesTurbojet and turbo fan enginesFluid i
19、njection system controlsAfterburner system controlContrail suppression controlSupercharger(s) or turbo-supercharger controlsAssisted takeoff controlFiring controlJettison controlCombined firing and jettison controlCircuit test (push to test)Cooling controls (cowl flaps, intercoolers, oilcoolers, etc
20、.)Air Induction system air controls (carburetor heatair filter, alternate air and turbo-by-pass system)Air induction system anti-icing controlIgnition control switch(es)Reciprocating enginesTurboprop or turbojet/turbofan engineAir start control(s)Propeller feathering controlsManual propeller feather
21、ing controlsAutomatic propeller feathering controlsVector thrust-mechanical controlsNozzle selector controlNozzle selector stop controlNozzle angle indicator.1313131415.141414141515151515161616.1617171717181818181818.18181919191919191919.20202020202020vProvided by IHSNot for ResaleNo reproduction or
22、 networking permitted without license from IHS-,-,-MIL-STD-203GPARAGRAPH5.35.3.15.3.25.3.35.3.45.3.4.15.3.4.1.15.3.4.1.25.3.4.1.35.3.4.25.45.4.15.4.25.55.5.15.5.1.15.5.25.5.35.5.3.15.5.42222222222235.5.4.15.5.55.5.65.5.75.65.5.15.6.25.6.2.15.6.2.25.6.2.2.15.6.2.35.6.2.3.15.6.2.3.25.6.35.6.3.15.6.3.2
23、5.6.3.35.75.7.15.7.25.7.35.85.8.15.8.25.8.35.8.3.15.8.4CONTENTSPAGEFuel system controls Engine fuel feed controls .Fuel transfer controls Fuel dump control .Inflight refueling Boom and receptacle system Inflight refueling switches selector, reset, andmanual override Disconnect switch .Indicator ligh
24、ts Probe and drogue system .Fire fighting controls .Engine emergency shutdown controls .Fire extinguisher and agent discharge control .Electrical engine start COMM/NAV/IDENT and .lighting controls .Electrical system controls Circuit protective devices (breakers) .Engine start, primer, oil dilution c
25、ontrols Lighting controls (interior/exterior) Landing/taxi light and searchlight switches .Primary voice communications (VHF, UHF)control(s) Channel/frequency indication .Intercommunication (ICS) controls NAV/AUTONAV/FLT MGMT controls .Radar beacon (IFF, SIF) controls Armament controls Armament cont
26、rols - General .Weapon release controls .Missile/gun firing switch .Bomb, rocket, torpedo, and external stores controlsNormal release switch Emergency release of stores Master electrical jettisoning control Mechanical release of external stores .Weapon aiming controls .Sight manual range controls Ra
27、dar boresight/caging control Target designator control .Displays .Displays - General Basic flight parameter(s) group .Engine parameters .Location and arrangement of signals Light signals .Arrangement scheme Warning signals Master warning signals .Caution signals .202020212121212121212121222323232424
28、2424242425252525252525252525252526262626262727viProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-203GPARAGRAPH5.8.4.15.8.55.8.65.8.75.95.9.127282828285.9.25.9.35.9.45.9.55.9.65.9.75.9.85.9.95.9.9.12828282828292929295.9.10CONTENTSPAGEMaster cau
29、tion signals Advisory signals Mechanical visual signals Radar altimeter .Miscellaneous controls and equipment Oxygen system controls and displays (Includingoxygen “ON“ “OFF” valve, oxygen regulator withintegral pressure gauge and flow indicator,liquid oxygen quantity) Anti-G suit control Environment
30、al control systems and displays .Shoulder harness lock .Seat adjustment controls Flap stowage De-icing, anti-icing, and pilot heat controls Bail-out alarm switch .Emergency power system controls Ram air turbine control/emergency power unit/auxiliary power unit Checkoff lists 29296.6.16.26.36.46.5NOT
31、ESIntended use Issures of DODISS International intrest .Subject term (key word) Changes from previous issue .303030303030FIGURES1. Cockpit arrangement: Fithter/Attack-SingleEjection Seat 2. Cockpit arrangement: Attack/Bomber/ASW-Side-by-Side-Ejection Seats 3. Cockpit arrangement: Patrol/Cargo/Transp
32、ort/AEW/Side-by-Shle Multi-flight crew/Non-Ejection Seats 4. Instrument Panel variations: Fighter/Attack-SingleEjection Seat 31323334viiProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-203G1. SCOPE1.1 Scope. This document establishes the requi
33、rements for the uniformlocation, arrangement, and actuation of controls and displays used in thefunctional crew stations of military fixed wing aircraft.1.2 Applicability. The requirements contained herein apply to the designof aircrew stations in fixed wing aircraft procured by the militarydepartme
34、nts. The contents describe requirements location, for the location,arrangement, and actuation of crew station controls and related items ofequipment, and the relative location of electromechanical and electronicdisplays, including the basic flight and engine instrument groups.2. APPLICABLE DOCUMENTS
35、2.1 Government documents.2.1.1 Specifications, standards and handbooks. The followingspecifications, standards and handbooks form a part of this document to theextent specified herein. Unless otherwise specified, the issues of thesedocuments are those listed in the issue of the Department of Defense
36、 Index ofSpecifications and Standards (DODISS) and supplement thereto, cited in thesolicitation (see 6.2).SPECIFICATIONSMILITARYMIL-S-3950MIL-L-6503MIL-C-6781MIL-P-7788MIL-S-8805MIL-H-8810MIL-M-18012MIL-L-18276MIL-F-18372MIL-S-22885MIL-H-46855MIL-C-81774MIL-L-85762MIL-E-87235Switch, Toggle, Environm
37、entally Sealed, GeneralSpecification forLighting Equipment, Aircraft, General Specification forInstallation ofControl Panel, Aircraft Equipment, Rack or Console MountedPanel, Information Integrally IlluminatedSwitches and Switch Assemblies, Sensitive and Push, SnapAction, General Specification forHa
38、ndles, Control, AircraftMarkings for Aircrew Station Displays, Design andConfiguration ofLighting, Aircraft Interior, Installation ofFlight Control Systems: Design, Installation and Test of,Aircraft (General Specification for)Switch, Push Button, Illuminated, General Specification forHuman Engineeri
39、ng Requirements for Military Systems,Equipment and FacilitiesControl Panel, Aircraft, General Specification forLighting, Aircraft, Interior, Night Vision ImagingSystem (NVIS) CompatibleEmergency Escape, Aircraft1Provided by IHSNot for ResaleNo reproduction or networking permitted without license fro
40、m IHS-,-,-STANDARDSMILITARYMIL-STD-411MIL-STD-783MIL-STD-1333MIL-STD-1472MS26518MS26521MS26523MS33634MS33785MIL-STD-203GAircrew Station SignalsLegends for Use in Aircrew Stations and on AirborneEquipmentAircrew Station Geometry for Military AircraftHuman Engineering Design Criteria for MilitarySyste
41、ms, Equipment and FacilitiesHandle, Control Aircraft RPM LargeHandle, Control, Aircraft Landing GearHandles, Control, Aircraft Fire ExtinguisherInstrument Arrangement, Engine, Standard, Basic, ForFixed and Rotary Wing AircraftInstrument Arrangement, Flight Standard, Basic forFixed and Rotary Wing Ai
42、rcraft(Unless otherwise Indicated, copies of federal and military specifications,standards, and handbooks are available from the Standardization DocumentsOrder Desk, Bldg 4D, 700 Robbins Ave., Philadelphia, PA 19111-5094)2.2 Order of precedence. In the event of a conflict between the text ofthis sta
43、ndard and the references cited herein, the text of this standard takesprecendence. Nothing in this document, however, supersedes applicable laws andregulations unless a specific exemption has been obtained.3. DEFINITIONS3.1 Fixed wing aircraft. All aircraft where the wings remain relativelyfixed wit
44、h respect to the aircraft fuselage. For the purposes of thisstandard, fixed wing aircraft shall include swing wing, tilt wing, and anyother type of aircraft other than rotary wing aircraft.3.2 Types of aircrew stations. (see Figures 1 thru 4)3.2.1 Dual pilot. An aircrew station with a single aircrew
45、 member.3.2.2 Dual pilot. An aircrew station requiring two aircrew members tocontrol the aircraft or complete the mission. The second aircrew member maynot be required for controlling flight but must be provided with the controlsand displays necessary for aircraft control and be capable of performin
46、g pilotduties as a backup. In an emergency, either pilot shall be able to safelycontrol the aircraft throughout all mission phases.(a) Tandem dual. The aircrew members are seated fore and aft withrespect to aircraft fuselage.3Provided by IHSNot for ResaleNo reproduction or networking permitted witho
47、ut license from IHS-,-,-MIL-STD-203G(b) Side-by-side dual. The aircrew members are seated laterally withrespect to aircraft fuselage.3.2.3 Multiple. An aircrew station with multiple aircrew membersconfigurations defined by the acquiring activity. Dual and multiple types mayinclude Configurations not
48、 requiring a co-pilot, flight controls or displaysnecessary for aircraft control capability, when defined by the acquiringactivity.3.2.4 Non-standard aircrew stations. Aircrew stations other than thegeneric types described by Figures 1 thru 4 may involve arrangements for whichthis standard will have
49、 limited application. The application of this standardwithin a non-standard aircrew station shall be directed by the acquiringactivity.3.3 Geometry and clearance. The arrangement of controls and displayswithin the aircrew station to accommodate the user population while the useris clad in full complement of clothing and equipment.3.3.1 Clearance. The distance by which one object clears an
