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Indicators
SPOILERS
EICAS STATUS PAGE
EICAS FLIGHT CONTROLS SYNOPTIC PAGE
(SECONDARY DISPLAY)
Maximum Spoiler
Deployment Mark
Ground Spoiler
Position Indicators
Ground Spoiler
Outline
Respective hydraulic manifold and PSEU are
operative.
Respective hydraulic manifold and PSEU are
inoperative.
Invalid data
Ground Spoiler Outline
FLIGHT CONTROLS
For Training Purposes Only
May 03
10-29
P I LOT T R A I N I N G GU I D E
EICAS Flight Controls Indications (Flight Spoilers)
Figure 10-18
P604_10_020
FLIGHT CONTROLS
AIL AIL
FLAPS MOTOR OVERHEAT
FLAPS 30
Description Symbol Condition
Indicates relative position of respective spoiler
Note: Indicators are not displayed when respective
spoiler is retracted or input data is invalid
Flight Spoiler Position
Indicators
SPOILERS
EICAS STATUS PAGE
EICAS FLIGHT CONTROLS SYNOPTIC PAGE
(SECONDARY DISPLAY)
Maximum Spoiler
Deployment Mark
Mid Spoiler
Deployment
Mark
Flight Spoiler
Outline
Respective flight spoiler detent mechanism and
associated surface position are valid
Abnormal condition of flight spoiler detent mechanism
and associated surface position
Invalid data
Flight Spoiler Outline
Flight Spoiler
Position Indicator
FLIGHT CONTROLS
10-30 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
EICAS Flight Controls Indications (Flaps)
Figure 10-19
P604_10_021
FLIGHT CONTROLS
AIL AIL
FLAPS MOTOR OVERHEAT
FLAPS 30
Description Symbol Condition
Indicates in degrees, the position of the LH an RH
flaps
Notes: The flap information is removed from display
whenever the landing gear and flaps are fully
retracted
Flap Position Readout
EICAS PRIMARY PAGE EICAS FLIGHT CONTROLS SYNOPTIC PAGE
(SECONDARY DISPLAY)
Flap Position
Readout
Flaps are operating normally
Flaps are operating at half speed due to a single flap
motor overheat
Invalid data
Flap Outline
Flap Outline
DN DN DN
- GEAR - - FLAPS -
C ALT
STAB
RATE
- TRIM -
P
3200 200 -0.5
30
NU
ND
4.0
RUDDER
AIL
LWD RWD
NL NR
Flaps failed or both flap motors overheated
Invalid data
FLAPS 30
FLAPS _ _
FLIGHT CONTROLS
For Training Purposes Only
May 03
10-31
P I LOT T R A I N I N G GU I D E
EICAS Flight Controls Indications (Trim)
Figure 10-20
P604_10_022
Description Symbol Condition
Stabilizer position is within the takeoff trim range
(3° to 8°)
NU - Nose Up (Top tick mark - 9°)
ND - Nose Down (Bottom tick mark - 0°)
Stabilizer Trim Pointer and
Readout
Stabilizer position is outside of the takeoff trim range
Aileron Trim Pointer
Stabilizer Trim
Scale
Rudder Trim Pointer
Indicates aileron trim displacement
LWD - Left Wing Down
RWD - Right Wing Down
Indicates rudder trim displacement
NL - Nose Left
NR- Nose Right
STAB
NU
ND
4.0
STAB
NU
ND
4.0
AIL
LWD RWD
RUDDER
NL NR
Aileron Trim
Pointer
Rudder Trim
Pointer
EICAS PRIMARY PAGE
DN DN DN
- GEAR - - FLAPS -
C ALT
STAB
RATE
- TRIM -
P
3200 200 -0.5
20
NU
ND
4.0
RUDDER
AIL
LWD RWD
NL NR
Stabilizer Trim
Pointer and Readout
FLIGHT CONTROLS
10-32 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
EICAS Flight Controls Indications (Aileron, Elevator, Rudder)
Figure 10-21
FLIGHT CONTROLS
AIL
RUDDER
ELEV ELEV
AIL
FLAPS MOTOR OVERHEAT
FLAPS 30
P604_10_023
Description Symbol Condition
Indicates relative position of respective aileron
Top tick mark – 20.8°
Center tick mark – 0°
Bottom tick mark – -21.3°
Aileron Position Indicator
EICAS FLIGHT CONTROLS SYNOPTIC PAGE
(SECONDARY DISPLAY)
Aileron PCU Valve Jam Mechanical jam of PCU control valve is detected
Symbol
PCU Valve
Jam Symbol
Elevator Position Indicator
Aileron
Position
Indicator
Aileron
Outline
Elevator
Outline
Elevator
Position
Indicator
Rudder Position Indicator
AIL AIL
ELEV ELEV
RUDDER
Indicates relative position of respective aileron
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庞巴迪挑战者604机组操作手册 CL_604-FLIGHT_CONTROLS(11)
