777 AMM 飞机维护手册 指示和记录系统 2(11)

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Takeoff Configuration Warning Test
The takeoff configuration warning test verifies the operation of the takeoff configuration warning function. This test simulates takeoff thrust and looks for proper takeoff configuration warning function response.
When you do a takeoff configuration warning test, you also do a stabilizer green band test. You will see the green band lamps on the stabilizer trim indicators come on.
Training Information Point
The takeoff configuration warning test will supply a takeoff configuration warning only if the airplane is not in the proper configuration for takeoff.
WES System Test
The WES system test verifies the status of each one of the WES channels. The test also verifies the operation of these:
*
Master warning lights

*
Aural warning speakers

*
Stick shaker actuators.

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WES -GROUND TESTS -1

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WES -GROUND TESTS -2

General
You do the stall warning test from the MAT.
Training Information Point
The WES is in ATA chapter 31. However, you must select ATA System 27 Stall Warning Management to do a stall warning test.
Stall Warning Test
The stall warning test verifies the operation of the stall warning function. This test will activate the stick shaker actuators momentarily. You will also see some speed tape parameters on the PFD.
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WES -GROUND TESTS -2

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BOEING PROPRIETARY -Copyright # -Unpublished Work -See title page for details.

PRIMARY DISPLAY SYSTEM -INTRODUCTION

General
The primary display system (PDS) is part of the airplane information management system (AIMS). The PDS shows information in many different formats on six display units (DUs) in the flight deck. The information includes:
*
Airplane status

*
Navigation data

*
Flight plan data

*
Engine indicating and crew alerting data

*
Communication data

*
Checklists

*
Maintenance data.

Abbreviations and Acronyms
*
ACARS -aircraft communications addressing and reporting system

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ACE -actuator control electronics

*
acpt -accept

*
ADIRS -air data inertial reference system

*
ADIRU -air data inertial reference unit

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AFDS -autopilot flight director system

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ail -aileron

*
AIMS -airplane information management system

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ALDB -airline loadable database

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alt -altitude

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altn -alternate

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app -approach

*
ARINC -Aeronautical Radio, Inc.

*
arpt -airport

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att -attitude

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baro -barometric

*
BLS -bezel light sensor

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brks -brakes

*
canc -cancel

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capt -captain

*
CAS -calibrated airspeed

*
CCD -cursor control device

*
CDU -control display unit

*
chkl -checklist

*
CMCF -central maintenance computing function

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comm -communication

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CPM/GG -core processor module/graphics generator

*
crz -cruise

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DH -decision height

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DSP -display select panel

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dspl -display

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DU -display unit

*
EFIS CP -electronic flight instrument system control panel

*
EGT -exhaust gas temperature

*
EICAS -engine indication and crew alerting system

*
elev -elevator

*
eng -engine

*
EPCS -electronic propulsion control system

*
EPR -engine pressure ratio

*
ESI -engine start inhibit

*
excd -exceedance

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ext -external

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fctl -flight control

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F/D -flight director

*
FDCF -flight deck communication function

*
FF -fuel flow

*
flprn -flaperon

*
flt -flight

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