PRIMARY DISPLAY SYSTEM -INTRODUCTION
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FMA -flight mode annunciation
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FMCF -flight management computing function
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FMCS -flight management computing system
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F/O -first officer
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FPV -flight path vector
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FPA -flight path angle
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FSEU -flap slat electronics unit
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fwd -forward
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GPWS -ground proximity warning system
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GS -glide slope
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G/S -ground speed
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hdg -heading
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hPa -hectopascal
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hyd -hydraulic
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IDG -integrated drive generator
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ILS -instrument landing system
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IM -inner marker
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inbd -inboard
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IOM -input/output module
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isln -isolation
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ISSP -instrument source select panel
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lim -limit
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LNAV -lateral navigation
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lo -low
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loc -localizer
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LRU -line replaceable unit
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LRM -line replaceable module
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LSK -line select key
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mag -magnetic
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MAT -maintenance access terminal
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MCP -mode control panel
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MDA -minimum descent altitude
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MFD -multi-function display
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MINS -minimums
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MLW -maximum landing weight
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MM -middle marker
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MMEL -master minimum equipment list
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MMO -maximum operating mach number
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MTRS -meters
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nav -navigation
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NCD -no computed data
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ND -navigation display
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NVM -nonvolatile memory
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N1 -low pressure rotor speed
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N2 -high pressure compressor RPM
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OF -overfull
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OM -outer marker
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OPAS -overhead panel ARINC 629 system
* outbd -outboard
* ovht -overheat
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PDS -primary display system
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PFD -primary flight display
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pln -plan
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pos -position
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QFE -altimeter setting to indicate height above reference airfield
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QNH -altimeter setting to indicate height above mean sea level
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QRH -quick reference handbook
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RA -radio altitude
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RA -resolution advisory
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rcd -record
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rcl -recall
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ref -reference
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rev -reverser
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PRIMARY DISPLAY SYSTEM -INTRODUCTION
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RF -refill * WAI -wing anti-ice
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rjct -reject * WES -warning electronics system
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RLS -remote light sensor * wpt -waypoint
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RTO -rejected takeoff * WXR -weather radar
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SAI -system analysis item * X-BLD -cross bleed
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SATCOM -satellite communications
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SMT -scheduled maintenance task
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SPD -speed
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stat -status
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std -standard
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TA -traffic advisory
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TAI -thermal anti-ice
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TAS -true airspeed
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TCAS -traffic alert and collision avoidance system
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TCW -time critical warning
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temp -temperature
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tfc -traffic
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trk -track
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upr -upper
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UTC -universal time (coordinated)
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vert -vertical
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vib -vibration
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vlv -valve
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VMO -maximum operating limit speed
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VNAV -vertical navigation
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VR -rotation speed
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VREF -landing reference speed
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VSI -vertical speed indicator
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VS -stall speed
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VTK -vertical track
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VTO -volumetric topoff
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V1 -takeoff decision speed
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V2 -takeoff safety speed
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PRIMARY DISPLAY SYSTEM -INTRODUCTION
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PRIMARY DISPLAY SYSTEM -GENERAL DESCRIPTION
General
The AIMS PDS provides dynamic and static information to the flight and ground crews. The PDS also provides crew interface with other avionics systems. These are the major components of the AIMS PDS:
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Six display units (DUs)
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本文鏈接地址：777 AMM 飛機(jī)維護(hù)手冊(cè) 指示和記錄系統(tǒng) 2(12)
