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OIL PRESS
FAN VIB
4890 4890
16770
1.2
82
3500
2120
- FUEL QTY - TOTAL
3500
82
115 OIL TEMP 115
1.2
4870
Oil Pressure
Digital Readout
Oil Temperature
Digital Readout
FAN VIB
Digital Readout
3500 FF 3500
Invalid data or fuel flow exceeds 5000 lbs/hr
Fuel Flow Digital Readout
(On aircraft 5301-5499 and
aircraft pre SB 604-34-031) 3500 FF 3500
3500 FF(PPH) 3500
1590 FF(KGH) 1590
Indicates fuel flow in pounds per hour (PPH) or
kilograms per hour (KGH)
FF(PPH)
FF(KGH)
Invalid data or fuel flow exceeds 5000 lbs/hr or
2222 kg/hr
Oil Pressure Digital
Readout
82 OIL PRESS 82
Oil pressure greater than 25 psi and less than or
equal to 115 psi
Oil pressure greater than 116 psi and less than or
equal to 155 psi
Oil pressure is less than or equal to 25 psi
Invalid data
120 OIL PRESS 120
10 OIL PRESS 10
10 OIL PRESS 10
1.2 FAN VIB 1.2
3.0 FAN VIB 3.0
–.– FAN VIB –.–
115 OIL TEMP 115
158 OIL TEMP 158
169 OIL TEMP 169
115 OIL TEMP 115
FAN VIB Digital Readout
Oil temperature greater than -40°C and less than or
equal to 154°C
Oil temperature greater than 155°C and less than or
equal to 162°C
Oil temperature is greater than 163°C
Invalid data
Fan vibration is 0 to less than or equal to 2.6 MILS
Fan vibration is equal or greater than 2.7 MILS
Invalid data
Symbol
POWER PLANT
18-34 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
EICAS Messages
MESSAGE MEANING AURAL WARNING
(IF ANY)
ENGINE
Left or right engine N1 or N2 or ITT above exceedance
level.
TRIPLE ATTENSON
L ENG OIL PRESS
Oil pressure in the respective engine is less than 25 psi. “ENGINE OIL”
R ENG OIL PRESS
L ENG START SOV The respective start shutoff valve is not closed with that
engine running.
TRIPLE ATTENSON
R ENG START SOV
APR INOP
Either the APR has failed or it is not armed (APR to arm and N1 > 79% and both
eng speed switches on).
APR CMD SET APR has been inadvertently activated on both engines.
L ENG MISCOMP The engine comparator has sensed a discrepancy in the respective engine
R ENG MISCOMP parameters (N1, ITT or N2).
L FUEL FILTER
Respective fuel filter is in impending bypass mode.
R FUEL FILTER
L FUEL LO PRESS
Insufficient pressure at the respective engine pump inlet.
R FUEL LO PRESS
L REV UNLOCKED
Reverser moved away from fully stowed position without a deploy command.
R REV UNLOCKED
L REV UNSAFE
Unarmed thrust reverser received a deploy command.
R REV UNSAFE
APR ARM Aircraft in takeoff configuration, dynamic test OK.
APR TEST 1 OK
APR TEST 2 OK The respective APR circuit has passed the self-test.
APR TEST 3 OK
L ENG SOV CLSD Fuel shutoff valve is closed after activation of the respective ENG FIRE PUSH
R ENG SOV CLSD switch/light.
IGNITION A ‘A’ igniters are activated, ‘B’ igniters off.
IGNITION A/B Both ‘A’ and ‘B’ igniters are activated.
IGNITION B ‘B’ igniters are activated, ‘A’ igniters off.
L REV ARMED
The respective thrust reverser is armed.
R REV ARMED
DCU 1 APR FAIL
DCU 2 APR FAIL The respective DCU has failed its APR test.
DCU 3 APR FAIL
L ENG ECU FAIL
The respective engine ECU failed to respond to an APR test.
R ENG ECU FAIL
EICAS Messages
Table 18-2
For Training Purposes Only
Sept 04
5-i
P I LOT T R A I N I N G GU I D E
COMMUNICATIONS
Chapter 5: Communications TABLE OF CONTENTS
Page
Introduction .........................................................................................................................5-1
Description ..........................................................................................................................5-1
Interphone Communication...........................................................................................5-1
Flight Compartment Speakers ................................................................................5-1
Flight Crew Intercom...............................................................................................5-2
Service Intercom Panels .........................................................................................5-3
Control Wheel Radio Key........................................................................................5-5
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