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Engines, APU EICAS Messages . . . . . . . . . . . . . . . . . . . . . . . . 7.40.1
787 Flight Crew Operations Manual
7.TOC.0.4 Boeing Proprietary
Engines, APU -
Table of Contents
Intentionally
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787 Flight Crew Operations Manual
Engines, APU Chapter 7
Controls and Indicators Section 10
Boeing Proprietary 7.10.1
7.10 Engines, APU-Controls and Indicators EICAS Display
Displayed full time on the EICAS display:
• TPR
• N1
• EGT.
1 Primary Engine Indications
DOWN
GEAR
F
LAP
S
15
1000
LBS X
SAT TEMP +13c
+10c FUEL
TOTAL FUEL
243.4
GROSSWT
640.0
102.4
TAT +14c TO1
TPR
102.4
EGT
N1
588 588
21.5
21.6
21.5
21.6
CAPTAIN’S / FIRST OFFICER’S INBD DISPLAY
1
787 Flight Crew Operations Manual
Engines, APU -
Controls and Indicators
7.10.2 Boeing Proprietary
Mode Indications
Displayed (white) – TAT (degrees C).
Displayed (green) – selected FMS thrust reference mode:
• TO – maximum rated takeoff thrust
• TO 1 – derate one takeoff thrust
• TO 2 – derate two takeoff thrust
• D–TO – assumed temperature derated takeoff thrust
• D–TO 1 – derate one assumed temperature derated takeoff thrust
• D–TO 2 – derate two assumed temperature derated takeoff thrust
• CLB – maximum rated climb thrust
• CLB 1 – derate one climb thrust
• CLB 2 – derate two climb thrust
• CON – maximum rated continuous thrust
• CRZ – maximum rated cruise thrust
• G/A – maximum go-around thrust.
Displayed (green) – selected assumed temperature (degrees C) for reduced thrust
takeoff.
Displayed REV (amber) – reverser in transit.
Displayed REV (green) – reverser fully deployed.
TPR Indications
Note: When reverse thrust is activated, the following indications are not
displayed:
1 Total Air Temperature (TAT)
2 Thrust Reference Mode
3 Assumed Temperature
4 Thrust Reverser Indication
• maximum TPR line
• commanded TPR
• reference/target TPR
indication
• reference TPR.
D-TO
REV
TAT +13c +30c
REV
EICAS DISPLAY (TOP)
1 2 3
4
787 Flight Crew Operations Manual
Engines, APU -
Controls and Indicators
Boeing Proprietary 7.10.3
Displayed (amber).
Displayed (green) – reference TPR limit.
Displayed (magenta) – target FMC commanded TPR when VNAV is engaged and:
• the autothrottle is engaged in THR or THR REF mode, or
• the autothrottle is not engaged.
Displayed (white).
Displayed:
• (white) – momentary difference between engine TPR and TPR
commanded by thrust lever position
• (amber filled) – difference between engine TPR and commanded TPR
exceeds normal operating parameters (TBD). EICAS alert message ENG
THRUST (L or R) is displayed.
Displayed (green).
Displayed (white).
Displayed (white).
1Maximum TPR Line
2 Reference/Target TPR indication
3 Commanded TPR
4 Commanded TPR Sector
5 Reference TPR
6 Actual TPR
7 Actual TPR indication
102.4
TPR
102.4
21.6 21.6
EICAS DISPLAY
5
2 6
1
7
3
4
787 Flight Crew Operations Manual
Engines, APU -
Controls and Indicators
7.10.4 Boeing Proprietary
TPR Indications (Alternate Mode)
Displayed (blank).
Displayed (blank).
N1 Indications
Displayed (red) – N1 RPM operating limit.
Digital N1 RPM (%), displayed:
• (white) – normal operating range
• displayed (red) – operating limit reached.
N1 RPM, displayed:
• (white) – normal operating range
• displayed (red) – operating limit reached.
1 TPR Indication
2 Actual TPR Indication
1 N1 Red Line
2 N1
3 N1 Indication
TPR
EICAS DISPLAY
2
1
N1
21.5 21.5
EICAS DISPLAY
3
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787 Flight Crew Operations Manual
Engines, APU -
Controls and Indicators
Boeing Proprietary 7.10.5
N1 Indications (Hard Alternate Mode)
Note: When reverse thrust is activated, the following indications are not
displayed:
• maximum N1 line
• commanded N1
• reference/target N1 indication
• reference N1.
Displayed (red).
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