MQF SEP 2021 - 251-300 Flashcards
During a normal takeoff, initiate rotation to ______ degrees nose high at rotation speed.
A. 7-10
B. 10-12
C. 12-15
D. 7-15
Proctor Reference: T.O. 1T-6A-1
A. 7-10
N1 will automatically reduce from flight idle (67%) to ground idle (60-61%) approximately ______ seconds after touchdown:
A. 7
B. 8
C. 10
D. 4
Proctor Reference: T.O. 1T-6A-1
D. 4
In the auto start mode, if a hot start, hung start, or no start is detected, the PMU should terminate the start sequence. The pilot must then perform a ______ second motoring run.
A. 10
B. 15
C. 20
D. 30
Proctor Reference: T.O. 1T-6A-1
C. 20
During gusty wind conditions, increase landing threshold and touchdown speeds by 50% of the gust increment up to a maximum increase of ______ knots.
A. 5
B. 10
C. 8
D. Do not increase speeds
Proctor Reference: T.O. 1T-6A-1
B. 10
Airstart attempts are not recommended below ______ AGL, as primary attention should be to eject or safely recover the aircraft.
A. 6000
B. 5000
C. 2000
D. 3000
Proctor Reference: T.O. 1T-6A-1
C. 2000
If the standby attitude gyro off flag appears after the battery bus has failed, the indicator will continue to operate for at least ______ minutes.
A. 5
B. 9
C. 15
D. 30
Proctor Reference: T.O. 1T-6A-1
B. 9
If the battery fails, OBOGS will be inoperative. Emergency oxygen is required above 10,000 feet cockpit altitude.
True
False
Proctor Reference: T.O. 1T-6A-1
True
Maximum airspeed for flight with a shattered/damaged/unlocked canopy is
A. 200 KIAS
B. 185 KIAS
C. 150 KIAS
D. 120 KIAS
Proctor Reference: T.O. 1T-6A-1
C. 150 KIAS
If safe gear-down indications are obtained at any point during LANDING GEAR MALFUNCTION checklist:
A. discontinue the checklist and land as soon as practical
B. cycle the landing gear handle to verify safe gear down indications
C. pull the EMER LDG GR handle
D. none of the above
Proctor Reference: T.O. 1T-6A-1
A. discontinue the checklist and land as soon as practical
Illumination of the DUCT TEMP annunciator indicates that bleed air temperature in the
environmental systems duct (at anytime) or in the defog duct (defog on) has exceeded ______
deg F.
A. 200
B. 500
C. 300
D. 100
Proctor Reference: T.O. 1T-6A-1
C. 300
Whenever the trim interrupt button is being depressed, or when the trim disconnect switch is set to disconnect, all trim systems are disengaged and the TAD is disconnected.
True
False
Proctor Reference: T.O. 1T-6A-1
True
Recommended minimum altitudes for ejection are ______ feet AGL for controlled ejection, and ______ feet AGL for uncontrolled ejection.
A. 2,000; 10,000
B. 2,000; 6,000
C. 6,000; 10,000
D. None of the above
Proctor Reference: T.O. 1T-6A-1
B. 2,000; 6,000
For an engine failure, depending on airspeed, N1 will indicate 0% within approximately ______ seconds, even though the gas generator core may not have seized.
A. 2
B. 5
C. 10
D. 15
Proctor Reference: T.O. 1T-6A-1
B. 5
Full rudder deflection above ______ KIAS will exceed the limits for the rudder control system.
A. 150
B. 120
C. 180
D. 227
Proctor Reference: T.O. 1T-6A-1
A. 150
Holding a zero-G (+/- 0.25 G) loading for over ______ seconds can cause engine damage and possible engine failure, regardless of oil pressure indications.
A. 15
B. 5
C. 10
D. 30
Proctor Reference: T.O. 1T-6A-1
B. 5
Engine operation with high pressure pump suction feeding is limited to ______ hours.
A. 4
B. 6
C. 8
D. 10
Proctor Reference: T.O. 1T-6A-1
D. 10
You should attempt to manually balance a fuel load when the alternate engine data display is indicating FP FAIL.
True
False
Proctor Reference: T.O. 1T-6A-1
False
Which system operates independently from the primary hydraulic system:
A. Landing gear normal extension
B. Speed brake
C. Nose wheel steering
D. Wheel brakes
Proctor Reference: T.O. 1T-6A-1
D. Wheel brakes
Cabin pressurization will bleed out through the ______ when the inflow switch is set to OFF.
A. canopy seal
B. ram air valve
C. cabin pressurization outflow valves
D. inflow valve
Proctor Reference: T.O. 1T-6A-1
C. cabin pressurization outflow valves
The extra drag during an airstart attempt will cause a descent rate greater than 1350-1500
feet/min.
True
False
Proctor Reference: T.O. 1T-6A-1
True