CAFB T-1 MQF (2025)
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Terms in this set (300)
1. An operating C. Caution
procedure or
technique which
is considered
essential to
emphasize is a ?
(T.O. 1T-1A-1)
,2. If either B. False
electronic fuel
control fails, the
synchronization
system is still
operative. (T.O.
1T-1A-1)
3. Once TCAS A. expeditiously return to the
announces "clear applicable ATC clearance unless
of conflict," the otherwise directed by ATC.
pilot should: (T.O.
1T-1A-1)
4. Failure to A. nuisance warnings from the GPWS.
properly set the
decision height
could result in .
(T.O. 1T-1A-1)
5. If the ARC A. True
format is selected
on the DSP, the
EHSI will present
an expanded 70°
(approximate)
compass
segment. (T.O. 1T-
1A-1)
,6. The weather D. wet precipitation, ±60°
radar system
detects __ along
the flight path
ahead of the
aircraft. The radar
antenna sweeps
to paint a full
screen radar
picture of the
precipitation
pattern along the
flight path. (T.O.
1T-1A-1)
7. Due to weather C. do not rely on the system as the
radar system only means to avoid or
limitations, . (T.O. circumnavigate adverse weather.
1T-1A-1)
, 8. If the left A. True
engine fails while
the
synchronization
system is on,
there will be a
maximum of 1.5%
rpm spool down
of the right
engine. For this
reason, the
engine
synchronization
system should be
off during takeoff
and landing. (T.O.
1T-1A-1)
9. Avoid fingerlift A. True
actuation to
preclude
inadvertent
engine shutdown
when retarding
throttle toward
IDLE. (T.O. 1T-1A-1)
|Comprehensive Questions And
Verified Answers |100% Accurate
Answers | Already Graded A+
Save
Terms in this set (300)
1. An operating C. Caution
procedure or
technique which
is considered
essential to
emphasize is a ?
(T.O. 1T-1A-1)
,2. If either B. False
electronic fuel
control fails, the
synchronization
system is still
operative. (T.O.
1T-1A-1)
3. Once TCAS A. expeditiously return to the
announces "clear applicable ATC clearance unless
of conflict," the otherwise directed by ATC.
pilot should: (T.O.
1T-1A-1)
4. Failure to A. nuisance warnings from the GPWS.
properly set the
decision height
could result in .
(T.O. 1T-1A-1)
5. If the ARC A. True
format is selected
on the DSP, the
EHSI will present
an expanded 70°
(approximate)
compass
segment. (T.O. 1T-
1A-1)
,6. The weather D. wet precipitation, ±60°
radar system
detects __ along
the flight path
ahead of the
aircraft. The radar
antenna sweeps
to paint a full
screen radar
picture of the
precipitation
pattern along the
flight path. (T.O.
1T-1A-1)
7. Due to weather C. do not rely on the system as the
radar system only means to avoid or
limitations, . (T.O. circumnavigate adverse weather.
1T-1A-1)
, 8. If the left A. True
engine fails while
the
synchronization
system is on,
there will be a
maximum of 1.5%
rpm spool down
of the right
engine. For this
reason, the
engine
synchronization
system should be
off during takeoff
and landing. (T.O.
1T-1A-1)
9. Avoid fingerlift A. True
actuation to
preclude
inadvertent
engine shutdown
when retarding
throttle toward
IDLE. (T.O. 1T-1A-1)
