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􀀙 Continued on next page 􀀙
􀀙FUEL QTY LOW continued􀀙
Notes:Use flaps 20 and VREF 20 for landing.
Increased speed provides improved elevator
control for landing flare in the event of a dual
engine flameout.
Avoid high nose up attitude and excessive
acceleration or deceleration. This prevents
forward pumps from uncovering.
Deferred Items
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC 12.29
12.29
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing Checklist
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . DOWN
Landing gear . . . . . . . . . . . . . . . . . . . . . . DOWN
Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20
􀂠􀂠􀂠􀂠
1 Increase airspeed, change altitude or deviate to a
warmer air mass to achieve a TAT equal to or
higher than the fuel temperature limit (3 degrees C
above the fuel freeze point).
2 TAT increases approximately 0.5 to 0.7 degrees C
for each .01 Mach increase in airspeed. In extreme
conditions it may be necessary to descend as low
as FL250.
􀂠􀂠􀂠􀂠
􀀙FUEL QTY LOW continued􀀙
[] FUEL TEMP LOW
Condition: Fuel temperature is near the minimum.
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC
12.30
12.30
1 Do not start the APU. This prevents a potential fire
hazard.
2 Do not accomplish the following checklist:
APU SHUTDOWN
􀂠􀂠􀂠􀂠
[] FUEL VALVE APU
Condition: The APU fuel valve is not in the commanded
position.
Note: The APU is not available for the rest of the
flight.
December 10, 2007
777 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Hydraulics Section 13
Table of Contents
Copyright © The Boeing Company. See title page for details.
D632W001-TBC 13.TOC.1
HYD AUTO CONTROL C ...................................13.1
HYD AUTO CONTROL L, R................................13.1
HYD OVERHEAT DEM C1, C2, L, R.....................13.1
HYD OVERHEAT PRI C1, C2 .............................13.2
HYD OVERHEAT PRI L, R .................................13.2
HYD PRESS DEM C1, C2, L, R...........................13.3
HYD PRESS PRI C1, C2 ...................................13.3
HYD PRESS PRI L, R .......................................13.3
HYD PRESS SYS C ..........................................13.4
HYD PRESS SYS L ..........................................13.8
HYD PRESS SYS L+C .................................... 13.10
HYD PRESS SYS L+C+R ................................ 13.14
HYD PRESS SYS L+R .................................... 13.15
HYD PRESS SYS R ........................................ 13.18
HYD PRESS SYS R+C.................................... 13.20
HYD QTY LOW C........................................... 13.25
HYD QTY LOW L, R ....................................... 13.25
HYD QTY LOW L+C....................................... 13.25
HYD QTY LOW L+C+R................................... 13.26
HYD QTY LOW L+R....................................... 13.26
HYD QTY LOW R+C ...................................... 13.27
RAT UNLOCKED ........................................... 13.28
December 10, 2007
NNC.13-Hydraulics
Table Of Contents
777 Flight Crew Operations Manual
Non-Normal Checklists -
Hydraulics
Table of Contents
Copyright © The Boeing Company. See title page for details.
13.TOC.2 D632W001-TBC
Intentionally
Blank
December 10, 2007
777 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D632W001-TBC 13.1
13.1
NNC.13 Non-Normal Checklists-Hydraulics
1 C1 AIR DEMAND pump selector . . . . . . . . . . .ON
􀂠􀂠􀂠􀂠
1 ELEC DEMAND pump selector
(affected system) . . . . . . . . . . . . . . . . . . . . .ON
􀂠􀂠􀂠􀂠
1 DEMAND pump selector . . . . . . . . . . . . . . . OFF
2 Do not accomplish the following checklist:
HYD PRESS DEM
􀂠􀂠􀂠􀂠
[] HYD AUTO CONTROL C
Condition: Both of the following occur:
•Automatic control of both center demand
pumps fails
•System indications fail
　
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