(Exhibit 10) What does IC mean on the TAKEOFF REPORT LAYOUT? What does the
N below it mean? Ans✓✓✓-Improved climb
Not used for this calculation
(AOM, Vol I, PERF)
(Exhibit 10) What is the highlighted area in used for? Ans✓✓✓-To transcribe data
from a live calculation run by the flight follower. (AOM, Vol I, PERF)
A hung start occurs after starter cutout, as indicated by the engine failing to
accelerate 90 seconds after fuel control switch placed to run. What recall item
should be accomplished? Ans✓✓✓-FUEL CONTROL switch (affected
engine)......CUTOFF (QRH 7)
According to GOM Ch. 6, what are some of the effects of operating at the high-
than-normal true airspeeds associated with high-altitude airport operations?
Ans✓✓✓-Greater turn radius
Higher landing and takeoff speeds
Potential for hot brakes
Missed approach climb capability problems
Aircraft may seem fast visually
,Higher rates of descent (near the GPWS "sink rate" warning activation)
Pressurization scheduling may differ from normal
(GOM 6)
After a fire test pass, what two systems are no longer being monitored by the AC?
Ans✓✓✓-Wheel Well
Leading Edge Duct
(AOM Vol II, 8)
After entering the Thrust Limit from Aerodata, there are dashed lines present on
the Takeoff Page. What do you do? Ans✓✓✓-The presence of dashes in place of
reference speeds in the CDU is an indication that the FMS cannot generate speeds
for the entered Thrust Limit, ZFW and Flap setting. All data entries should stop
and the crew reconfirm all performance data entries. (AOM, Vol I, PERF)
After receipt of a "Conditional Clearance" the PNF should? Ans✓✓✓-Print the
ATC UPLINK page and place the printout where both pilots can see it until the
clearance has been complied with.
Leave the ATC UPLINK page displayed until the clearance has been complied with.
(AOM Vol I, SP)
An engine has failed in flight. N1 rotation and oil pressure are indicated. The
EICAS message ENG 1 FAIL appears. What recall items should be accomplished?
Ans✓✓✓-None. There are no recall items associated with an engine failure. The
appropriate QRH should be called for by the PF. (QRH 7)
,Are the TAT probes heated? When? Ans✓✓✓-Yes, Inflight only. (AOM Vol II, 3)
At what tiller angle will the body gear begin to aid in turning the aircraft?
Ans✓✓✓-At 20° of tiller angle
(AOM Vol II, 14)
Autobrakes operate using which brake control system? Ans✓✓✓-Normal brake
system
(AOM Vol II, 14)
Before starting engines with the #1 APU generator inop, what must be done to
pressurize the #4 hydraulic system? Ans✓✓✓-Turn ON the #4 Demand pump.
(MEL 24) (AOM Vol II, 6) (AOM Vol II, 13)
Can a flight be released based on a METAR? Ans✓✓✓-Yes, when weather
conditions forecast in a TAF prevent the release of a
flight, but the METAR indicates current weather conditions are at or above
minimums, a flight may be released provided the METAR history shows a
reasonable trend of weather conditions at or above the minimums required. The
flight must be coordinated with flight following to ensure the takeoff, approach,
and landing can be accomplished prior to issuance of the next normally scheduled
METAR report. (GOM 5)
Can a flight be released to an airport without an available TAF? Ans✓✓✓-Yes.
The METAR must show that the weather is at or above minimums
and a reasonable trend shows that the weather will remain so. (GOM 5)
, Can Class ll Navigation be conducted with a dual FMC failure? Ans✓✓✓-Yes
(AOM Vol II, 11)
Can the APU provide bleed air in flight? If so, up to what altitude? Ans✓✓✓-Yes.
For one pack up to 15,000ft. (AOM Vol II, 2)
Can you reset a tripped fuel pump Circuit Breaker? Ans✓✓✓-Do not reset a
tripped fuel pump circuit breaker
(QRH 12)
Certain locations in the world have been identified by IATA as having less than
reliable air traffic control services. Is there any additional procedure required?
Ans✓✓✓-The IATA In Flight Broadcast Procedure should be followed at each
Mandatory reporting point. (GOM 6)
Describe the check required after passing a waypoint in Class II airspace. What is
being determined by this check? Ans✓✓✓-Approximately ten minutes after
passing each waypoint, the steering LRN unit position should be plotted, and all
LRN units checked against each other to ensure there are no significant
deviations.
Record the time (UTC)
Verify on-course tracking
The check is designed to ensure that the proper coordinates are inserted in the
'Next' position and that the aircraft is tracking to that position.