-
The maximum start limit line (red) is displayed on the EICAS EGT indication after the fuel cutoff switch is placed to RUN, until:
the engine is stabilized at idle
-
The autostart system does NOT monitor ____ during engine start.
oil pressure or oil temperature
-
The EEC uses ____ for thrust control in the normal mode (200ER).
EPR
-
The auto-relight function of the EEC provides the pilot with ____
on the 777-200ER.
flameout protection during rain/hail ingestion
-
On a 777-200ER, which rotor drives the engine accessory gearbox?
N3
-
The EEC automatically selects approach idle when ____.
flaps are commanded Flaps 25 or greater
-
When the APU is operating in the attended mode, it will
immediately shut down for ____.
speed droop
-
Which of the following will cause approach idle to be
automatically selected in flight?
The opposite engine bleed valve is closed
-
With the engine in the hard alternate mode, reference and target
____ and maximum and commanded ____ values are displayed.
N1, N1
-
The autostart system will abort the start on the ground for ____.
starter shaft failure
-
Following a dual engine failure/stall procedure, airspeed should
be above ____ knots to ensure best windmill start capability.
(777-200ER)
250
-
On a 777-200ER, the minimum oil quantity prior to engine start is ____ quarts
16 QUARTS
-
A 300ER engine autostart will attempt to start the engines a
total of ___ times on the ground.
THREE
-
On a 777-300ER, if an engine is shutdown after selecting APU to
Pack operation, the engine cannot be started until:
APU to Pack takeoff mode has been deleted
-
T OR F.
On the -300ER, single engine taxi is not recommended.
TRUE
-
Following a dual engine failure/stall procedure, airspeed should
be above ____ knots to ensure best windmill start capability
(777-300ER).
270
-
What are the functions of the FUEL CONTROL Switch when selected to the RUN position during an Auto-Start?
- Opens the spar fuel valve
- arms the engine fuel valve
- arms the selected ignitor.
-
There is/are ____ fire extinguisher bottle available for APU
fires.
ONE
-
Bleed air is available from the APU through approximately ____
feet.
22000'
-
Concerning the APU supplying bleed air
and electrical power, which has priority?
Electrical power has priority over bleed air.
-
APU RPM is read on ____.
any of the 3 MFDs with status (STAT) selected
-
The main airplane battery provides power for the APU.....
- inlet door
- fuel valve
- APU fire detection system
-
If the APU start fails, the APU will _______automatically.
shut down automatically
-
T OR F
Do not start or shut down the APU if a fuel spill occurs
TRUE
-
The APU has 2 operating modes, attended and unattended. The APU will not shut down for high EGT, high oil temperature, or low oil pressure in ____ mode.
ATTENDED
-
The APU is in the unattended mode WHEN:
on the ground without either engine starting or running.
-
In the attended mode, the APU will continue to operate for which condition?
low oil pressure
-
In flight, if both AC transfer busses lose power, the RAT
deploys. What else happens?
The APU starts automatically
-
APU to Pack Operations (777-300ER) takeoffs are prohibited at
airports above ___ feet pressure altitude?
6900'
-
On -200ER aircraft, during Auto-Start, the EEC monitors EGT, N3 RPM, and other engine parameters UNTIL:
Until idle N3 is reached.
-
In the Normal mode, the EEC:
- Sets thrust by controlling EPR (RR) or N1 (GE ) based on thrust lever position.
- Maximum EPR (RR) or N1 (GE) represents the maximum rated thrust available from the engine.
- Maximum rated thrust is available in any phase of flight by moving the thrust levers to the full forward position.
-
T OR F
On -200ER aircraft, the Auto Relight system is activated when an engine is at or below idle with the FUEL CONTROL switch set to RUN.
TRUE
-
What is the required warm-up period prior to takeoff power application?
Three minutes
-
What are the indications of an engine failure during takeoff, with
airspeed at 100 knots?
- The Master Warning lights illuminate
- red ENG FAIL is displayed on the PFD,
- Voice annunciation "ENGINE FAIL".
-
The APU will not shut down for the following three conditions in ATTENDED mode:
- high EGT
- high oil temperature
- low oil pressure
-
When starting the APU, the APU Selector should be placed in the Start position for __ second.
ONE SECOND
-
The APU RUNNING memo message can be found on the _____ display.
EICAS Display
-
APU operating conditions (EGT, RPM, Oil Press, etc.) can be monitored on the ______ page.
Status Page (STAT)
-
In order to start the APU, the APU selector should be positioned how?
positioned to START for one second, then positioned to ON
-
After APU start during preflight, the APU is running in the unattended mode. It changes to the attended mode when:
when either engine is started or running
-
When operating the APU in the attended mode, these faults will result in the EICAS message APU LIMIT.
- high EGT
- high oil temperature
- low oil pressure
-
The EEC automatically selects approach idle when flaps are commanded to __________
flaps are commanded Flaps 25 or greater
-
When the APU is operating in the attended mode, it will immediately shut down for __ .
speed droop
-
On the 200ER the minimum oil quantity prior to engine start is __ quarts.
16 quarts
-
A red ENG FAIL on the PFD, accompanying voice annunciation, and Master Warning lights are displayed if an engine failure occurs at what speed range?
between 65 knots and 6 knots prior to V1
-
Engine flameout protection is provided by an auto-relight function in the EEC. This function is activated when:
- engine is at or below idle
- with the fuel control in RUN
- N3 above 35%
-
During the start, you will know the engines have stabilized at idle
when:
maximum start limit line (red) is no longer displayed on EGT
-
While monitoring oil temperature during engine start, you notice that it is in the amber range, you should not advance the throttles to takeoff power until oil temp is above:
50° C
-
Starting engines on a cold day, the crew positions the Start Selectors to START and the Fuel Control Switches to RUN. The EEC Auto start system commands starter cutout at about 50% N1 If the starter fails to cutout, the crew will know because the EICAS caution ______________ is displayed
ENG STARTER CUTOUT L,R
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