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AIRPLANE SYSTEM CAUTION MESSAGES ADVISORY MESSAGES
AFCS
AP TRIM is NU (ND) (Ldg only)
AP TRIM LWD - RWD (Ldg only)
YD 1-2 FAIL
YD OFF
YD NOT CENTERED (TO only)
Air Conditioning Pressurization EMER DEPRESS
L-R PACK FAIL
Aural and Visual Warnings CHECK DU 1 (2) (3) (4) (5) (6)
SG 1 (2) (3) FAIL
Electrical Power BATT MASTER OFF BATT EMER PWR ON
RAT GEN ON (Ldg only)
Doors and Exits
CARGO DOOR
LARGE SERV DOORS
R EMER EXIT
PASSENGER DOOR
SMALL SERV DOORS
Flight Controls
ELEVATOR SPLIT
FLT SPLR DEPLOYED
FLT SPOILERS FAIL
GND LIFT DUMP
ROLL SELECT
ROLL SPOILERS FAIL
RUD AUTHORITY LOW
SLAT-FLAP FAIL
STAB TRIM
STALL PROTECT FAIL
FLT SPOILERS FAULT
GND LIFT DUMP
NO TAKEOFF (TO only)
RUD AUTHORITY SAFE
SHAKER 1 (2) FAIL
SLAT-FLAP BIT
SLAT-FLAP HALFSPD
STALL WARN ADVANCE
Hydraulic Power HYD 1 (2) (3) LO PRESS
HYD RAT PUMP FAIL (Ldg only)
Ice and Rain Protection ICE
Instruments ADC 1 (2) (3) MISCMP
ALL ADC MISCMP ADC 1 (2) (3) FAIL
For Training Purposes Only
Sept 04
7-25
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
Landing Gear
BRAKE 50% DEGRADED
CPLT BRAKE FAULT
GEAR DISAGREE
INBD BRK LO PRESS
L (R) INBD BRAKE FAIL
L (R) OUTBD BRAKE FAIL
NOSE STEER FAIL
OUTBD BRK LO PRESS
PARK/EMER BRAKE ON (Ldg only)
PLT BRAKE FAULT
UNCOMMANDED BRAKE
BRAKE TEMP (TO only)
GEAR SYS FAULT
NO TAKEOFF (TO only)
Lighting EMER LIGHTS OFF
Navigation ALL IRS MISCMP
Power Plant
A/T NOT IN HOLD (TO only)
L (R) FADEC N1 CTL
L (R) FUEL FILTER
L (R) REV LOCK FAIL
L (R) REVERSER FAIL (Ldg only)
A/T 1-2 FAIL
AIRPLANE SYSTEM CAUTION MESSAGES ADVISORY MESSAGES
7-26 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
TAKEOFF CONFIGURATION WARNINGS
Takeoff configuration warnings are armed when the airplane is on the ground and both
engines are accelerated towards takeoff thrust (throttle position ≥ 30°). A voice
warning, EICAS warning message, and both MASTER WARNING lights come on for
any of the following:
All configuration warning indications are canceled when the configuration error is
corrected, or the airplane is airborne, or either thrust lever is retarded. A NO
TAKEOFF CAS Advisory message will indicate a configuration error prior to the
throttles being advanced towards takeoff.
LANDING CONFIGURATION WARNING
The “GEAR” aural will sound if any gear is not down and locked and:
• The radio altitude is less than 1,000 feet AGL and the descent rate is more than 400
feet per minute; or
• The radio altitude is less than 500 feet AGL and either throttle is below 25º throttle
lever angle and the flap position is 30º
• The radio altitude is less than 500 AGL and both throttles are below 25º throttle
lever angle and the flap position is not at 30º
NOTE
The “GEAR” aural can not be muted during any of these
conditions.
The “Too Low Gear” (EGPWS) aural warning is heard if any landing gear is not down
and locked with the radio altitude less than 500 feet AGL and the indicated airspeed at
less than 190 knots.
CONDITION VOICE MESSAGE EICAS MESSAGE
Aileron trim outside of takeoff range “NO TAKEOFF” CONFIG AIL TRIM
Parking brake on during takeoff “NO TAKEOFF” PARK BRAKE ON
Rudder trim outside of takeoff range “NO TAKEOFF” CONFIG RUD TRIM
Flaps not in takeoff position “NO TAKEOFF” CONFIG SLATS/FLAPS
Spoilers not in takeoff position “NO TAKEOFF” CONFIG SPOILERS
Horizontal stabilizer outside of takeoff range (“green band”) ‘’NO TAKEOFF” CONFIG STAB TRIM
For Training Purposes Only
Sept 04
7-27
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
If neither radio altimeter is valid, the “GEAR” aural will sound if any gear is not down
and locked and the airplane is below 16,500 feet. The landing gear horn may be muted
by pressing the mute horn switch/light on the landing gear control panel. With both
thrust levers at IDLE, (less than three degrees throttle lever angle) the horn cannot be
muted.
STALL WARNING
Warning of an impending stall is provided by independent stall protection systems.
Both systems are energized in flight and deactivated on the ground through air/ground
logic. The flight displays indicate airplane approach to stall speed by low speed cues
　
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