MQF Flashcards

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1
Q
  1. Pilots shall not exchange seats during flight if only two pilots are aboard the airplane.

A. True

B. False

A
  1. Pilots shall not exchange seats during flight if only two pilots are aboard the airplane.

Answer is A. True

Ref: T.O. 1C-135(K)R(II)-1, Page 4-2, Warning

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2
Q
  1. Verbal coordination between applicable crewmembers will be required when:

A. Control of the airplane is transferred between pilot and copilot or when an autopilot mode or axis is engaged or disengaged.

B. Repositioning fuel panel valves and switches or when an electrical source is changed.

C. A crewmember leaves position or leaves interphone or goes on or off oxygen.

D. Any of the above.

A
  1. Verbal coordination between applicable crewmembers will be required when:

A. Control of the airplane is transferred between pilot and copilot or when an autopilot mode or axis is engaged or disengaged.

B. Repositioning fuel panel valves and switches or when an electrical source is changed.

C. A crewmember leaves position or leaves interphone or goes on or off oxygen.

D. Any of the above.

Ref: T.O. 1C-135(K)R(II)-1, Page 4-2

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3
Q
  1. Normal hydraulic pressure range is to psi.

A. 1000; 3000

B. 2400; 3050

C. 1500; 2800

D. 1971; 2469

A
  1. Normal hydraulic pressure range is to psi.

A. 1000; 3000

B. 2400; 3050

C. 1500; 2800

D. 1971; 2469

Ref: T.O. 1C-135(K)R(II)-1, Page 5-7

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4
Q
  1. Based on ______________, the aircraft commander may elect single pilot preflight operations where one pilot proceeds to the aircraft with the boom operator to perform the exterior safety check and begin the interior preflight checks, while the other pilot accomplishes additional duties (obtaining weather brief, etc.).

A. Operational Need

B. Mission Requirements

C. Personal Preference

D. A or B

A
  1. Based on ______________, the aircraft commander may elect single pilot preflight operations where one pilot proceeds to the aircraft with the boom operator to perform the exterior safety check and begin the interior preflight checks, while the other pilot accomplishes additional duties (obtaining weather brief, etc.).

A. Operational Need

B. Mission Requirements

C. Personal Preference

D. A or B

Ref: T.O. 1C-135(K)R(II)-1, Page 2-2

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5
Q
  1. The copilot ANN DIM switch on the Copilot Overhead Light Panel must be out of the DIM (full ccw) position for the _________ to operate. Ensure that the copilot ANN DIM switch is out of the DIM (full ccw) position prior to closing the crew entry/cargo door. Once the crew entry/cargo doors are closed the DIM switch can be adjusted as required.

A. Co-Pilot’s Annunciator Panel

B. Side Panel Lighting

C. Engine Fire Lights

D. FDR

A
  1. The copilot ANN DIM switch on the Copilot Overhead Light Panel must be out of the DIM (full ccw) position for the _________ to operate. Ensure that the copilot ANN DIM switch is out of the DIM (full ccw) position prior to closing the crew entry/cargo door. Once the crew entry/cargo doors are closed the DIM switch can be adjusted as required.

A. Co-Pilot’s Annunciator Panel

B. Side Panel Lighting

C. Engine Fire Lights

D. FDR

Ref: T.O. 1C-135(K)R(II)-1, Page 2-16, Note

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6
Q
  1. Speed Brake Warning horn sounds when lever is pulled back more than ____ degrees out of the full forward position.

A. 5

B. 6

C. 2

D. 4

A
  1. Speed Brake Warning horn sounds when lever is pulled back more than ____ degrees out of the full forward position.

A. 5

B. 6

C. 2

D. 4

Ref: T.O. 1C-135(K)R(II)-1, Page 2-31

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7
Q
  1. If an APU with an operable generator is not available, and external power is not used, the start can be made on battery power only. During this procedure, all engine _________ gages are inoperative until a generator is on the line and 28V AC power is available.

A. Oil Pressure and Fuel Flow

B. N1 and N2

C. Oil Low Pressure Lights and EGT

D. Instrument

A
  1. If an APU with an operable generator is not available, and external power is not used, the start can be made on battery power only. During this procedure, all engine _________ gages are inoperative until a generator is on the line and 28V AC power is available.

A. Oil Pressure and Fuel Flow

B. N1 and N2

C. Oil Low Pressure Lights and EGT

D. Instrument

Ref: T.O. 1C-135(K)R(II)-1, Page 2-62, Notes

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8
Q
  1. For temperatures __________ , failure to set the engine start switch to IGNITION may result in engine flameout when the throttles are retarded during taxi operations.

A. Colder than normal

B. At and below 10C (50F)

C. At and below 4C (40F)

D. At and below 0C (32F)

Ans: D

Ref: T.O. 1C-135(K)R(II)-1, Page 2-64, Note

A
  1. For temperatures __________ , failure to set the engine start switch to IGNITION may result in engine flameout when the throttles are retarded during taxi operations.

A. Colder than normal

B. At and below 10C (50F)

C. At and below 4C (40F)

D. At and below 0C (32F)

Ref: T.O. 1C-135(K)R(II)-1, Page 2-64, Note

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9
Q
  1. Do not taxi or tow an aircraft within ____ feet of obstructions without wing walkers monitoring the clearance between the aircraft and the obstruction. Do not taxi aircraft closer than ____ feet to any obstruction.

A. 10, 25

B. 25, 10

C. 10, 10

D. 25, 25

Ans: B

Ref: AFI 11-218 AMC SUP, Paragraphs 1.22.2., 1.22.3

A
  1. Do not taxi or tow an aircraft within ____ feet of obstructions without wing walkers monitoring the clearance between the aircraft and the obstruction. Do not taxi aircraft closer than ____ feet to any obstruction.

A. 10, 25

B. 25, 10

C. 10, 10

D. 25, 25

Ref: AFI 11-218 AMC SUP, Paragraphs 1.22.2., 1.22.3

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10
Q
  1. When taxi clearance is doubtful, use ______ wing walkers.

A. One or more

B. Two or more

C. Three or more

D. Four or more

A
  1. When taxi clearance is doubtful, use ______ wing walkers.

A. One or more

B. Two or more

C. Three or more

D. Four or more

Ref: AFI 11-2KC-135 Vol 3, Paragraph 5.19.2

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11
Q
  1. What is the minimum taxi spacing during formation:

A. Safe interval

B. 150 feet

C. 75 feet

D. 50 feet

A
  1. What is the minimum taxi spacing during formation:

A. Safe interval

B. 150 feet

C. 75 feet

D. 50 feet

Ref: AFI 11-2KC-135 Vol 3, Paragraph 18.6.3

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12
Q
  1. In those situations where runway/taxi conditions or performance considerations are such that safety could be compromised,

A. A static takeoff should be made.

B. A rolling or static/rolling takeoff should be made

C. Extreme care should be given to calculating takeoff data

D. B and C

A
  1. In those situations where runway/taxi conditions or performance considerations are such that safety could be compromised,

A. A static takeoff should be made.

B. A rolling or static/rolling takeoff should be made

C. Extreme care should be given to calculating takeoff data

D. B and C

Ref: T.O. 1C-135(K)R(II)-1, Page 2-74, Caution

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13
Q
  1. If stabilizer trim has moved from setting selected during the TAXI checklist, ________.

A. Abort the mission

B. Reset to original setting

C. Call maintenance

D. Immediately place the stabilizer trim switch to the CUT-OFF position and manually trim throughout departure.

A
  1. If stabilizer trim has moved from setting selected during the TAXI checklist, ________.

A. Abort the mission

B. Reset to original setting

C. Call maintenance

D. Immediately place the stabilizer trim switch to the CUT-OFF position and manually trim throughout departure.

Ref: T.O. 1C-135(K)R(II)-1, Page 2-74, Step 2

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14
Q
  1. When experiencing a loss shear on takeoff, anticipate a loss in indicated airspeed and altitude. This situation is potentially dangerous if the airplane is close to the ground. If this loss is expected to be _____ knots or more, the takeoff shall be delayed, if possible, until more favorable conditions exist.

A. 10

B. 15

C. 20

D. 25

A
  1. When experiencing a loss shear on takeoff, anticipate a loss in indicated airspeed and altitude. This situation is potentially dangerous if the airplane is close to the ground. If this loss is expected to be _____ knots or more, the takeoff shall be delayed, if possible, until more favorable conditions exist.

A. 10

B. 15

C. 20

D. 25

Ref: T.O. 1C-135(K)R(II)-1, Page 7-7

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15
Q
  1. Maneuvering at speeds below three engine climbout speed plus ____ knots is not recommended. A bank angle of 30 degrees at climbout speed with flaps down could reduce climb capability by as much as____fpm.

A. 10, 200

B. 25, 300

C. 35, 300

D. 50, 400

Ans: D

Ref: T.O. 1C-135(K)R(II)-1, Page 2-84, Warning

A
  1. Maneuvering at speeds below three engine climbout speed plus ____ knots is not recommended. A bank angle of 30 degrees at climbout speed with flaps down could reduce climb capability by as much as____fpm.

A. 10, 200

B. 25, 300

C. 35, 300

D. 50, 400

Ref: T.O. 1C-135(K)R(II)-1, Page 2-84, Warning

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16
Q
  1. A departure alternate is required if weather is below landing minimums for the lowest suitable approach (at departure aerodrome). To qualify as a departure alternate, the airfield must be:

A. Within 30 minutes flying time, the existing weather is equal to or better than the published approach minimums and forecast to remain so until 1 hour after takeoff.

B. Within one hour flying time, better than published mins for the lowest suitable approach (to include a circling approach) for until end AAR time.

C. Within two hours flying time, the existing weather is at least 500-1 above the lowest compatible published approach minimums, but not less than 600-2 (precision) or 800-2 (non-precision) and forecast to remain so for 1 hour after ETA at the alternate.

D. A or C

A
  1. A departure alternate is required if weather is below landing minimums for the lowest suitable approach (at departure aerodrome). To qualify as a departure alternate, the airfield must be:

A. Within 30 minutes flying time, the existing weather is equal to or better than the published approach minimums and forecast to remain so until 1 hour after takeoff.

B. Within one hour flying time, better than published mins for the lowest suitable approach (to include a circling approach) for until end AAR time.

C. Within two hours flying time, the existing weather is at least 500-1 above the lowest compatible published approach minimums, but not less than 600-2 (precision) or 800-2 (non-precision) and forecast to remain so for 1 hour after ETA at the alternate.

D. A or C

Ref: AFI 11-2KC-135 Vol 3, para 6.19.2.1 and 6.19.2.2

17
Q
  1. If airplane is to remain in closed traffic after takeoff, thrust will be adjusted to climb out at the same speed to be used on the downwind leg, and a rate of climb of approximately ____ feet per minute.

A. 500

B. 1000

C. 1500

D. 2500

A
  1. If airplane is to remain in closed traffic after takeoff, thrust will be adjusted to climb out at the same speed to be used on the downwind leg, and a rate of climb of approximately ____ feet per minute.

A. 500

B. 1000

C. 1500

D. 2500

Ref: T.O. 1C-135(K)R(II)-1, Page 2-84

18
Q
  1. Possible causes of a ____ are engaging the pilot’s interphone (on the yoke or the tiller), pressing the pilot’s FD ANN TEST button, a cold hydraulic system, the low- flow capability of the auxiliary hydraulic pump, and/or the use of other hydraulically- actuated systems during the EFAS test; in this case, the EFAS self-test is ____ indicating a system failure.

A. Failed EFAS test; correctly

B. Failed EFAS test; incorrectly

C. Failed SYD test; not applicable and

D. Failed SYD test; correctly

A
  1. Possible causes of a ____ are engaging the pilot’s interphone (on the yoke or the tiller), pressing the pilot’s FD ANN TEST button, a cold hydraulic system, the low- flow capability of the auxiliary hydraulic pump, and/or the use of other hydraulically- actuated systems during the EFAS test; in this case, the EFAS self-test is ____ indicating a system failure.

A. Failed EFAS test; correctly

B. Failed EFAS test; incorrectly

C. Failed SYD test; not applicable and

D. Failed SYD test; correctly

Ref: T.O. 1C-135(K)R(II)-1, Page 2-22, Note

19
Q
  1. When a receiver is in or near the contact position, the pilot _____________ first indication of autopilot malfunction, including an inadvertent disconnect, if accompanied by out-of-trim control forces.

A. will switch the autopilot attitude source from VG to INU-2

B. should initiate a breakaway

C. should start a gentle climb

D. will initiate a breakaway

A
  1. When a receiver is in or near the contact position, the pilot _____________ first indication of autopilot malfunction, including an inadvertent disconnect, if accompanied by out-of-trim control forces.

A. will switch the autopilot attitude source from VG to INU-2

B. should initiate a breakaway

C. should start a gentle climb

D. will initiate a breakaway

Ref: T.O. 1C-135(K)R(II)-1, Page 2-90F, Warning

20
Q
  1. Unless dictated otherwise by ATP-56 (Part 5, Annex ZE) or by mission requirements, tankers will establish the applicable contact air refueling airspeed before the receiver reaches ____ . If the tanker is off airspeed by more than ____ knots, the receiver pilot will be informed prior to tanker airspeed changes.

A. 1NM, 5

B. 1NM, 10

C. Astern, 5

D. Astern, 10

A
  1. Unless dictated otherwise by ATP-56 (Part 5, Annex ZE) or by mission requirements, tankers will establish the applicable contact air refueling airspeed before the receiver reaches ____ . If the tanker is off airspeed by more than ____ knots, the receiver pilot will be informed prior to tanker airspeed changes.

A. 1NM, 5

B. 1NM, 10

C. Astern, 5

D. Astern, 10

Ref: T.O. 1C-135(K)R(II)-1, Page 2-90D, Warning

21
Q
  1. The position approximately 50 ft behind and slightly below the tanker boom nozzle where the receiver stabilizes with zero rate of closure before being cleared to the contact

position is called:

A. Astern

B. Pre-Contact

C. Stabilized

D. Either A or B

A
  1. The position approximately 50 ft behind and slightly below the tanker boom nozzle where the receiver stabilizes with zero rate of closure before being cleared to the contact

position is called:

A. Astern

B. Pre-Contact

C. Stabilized

D. Either A or B

Ref: ATP-56 Part 5, page ZE-4-2

22
Q
  1. When planning to conduct a Rendezvous G, a common track length equivalent to ____ min flying time should be planned to allow for tanker descent to RV FL/altitude/height, visual acquisition and timing corrections.

A. 5

B. 10

C. 15

D. 20

A
  1. When planning to conduct a Rendezvous G, a common track length equivalent to ____ min flying time should be planned to allow for tanker descent to RV FL/altitude/height, visual acquisition and timing corrections.

A. 5

B. 10

C. 15

D. 20

Ref: ATP-56 Part 2, Annex 1G, para 102G(b), page 1 G-1

23
Q
  1. After obtaining and reading back the clearance, the pilot should monitor the forward estimate for oceanic entry, and if this changes by ____ minutes or more, the pilot must pass a revised estimate to ATC.

A. 1

B. 2

C. 3

D. 5

A
  1. After obtaining and reading back the clearance, the pilot should monitor the forward estimate for oceanic entry, and if this changes by ____ minutes or more, the pilot must pass a revised estimate to ATC.

A. 1

B. 2

C. 3

D. 5

Ref: North Atlantic MNPSA Operations Manual, Para 5.1.7

24
Q
  1. Approximately ____ minutes after exiting CPDLC and/or ADS-C service areas, the flight crew should ensure there are no active CPDLC or ADS-C connections.

A. 15

B. 30

C. 40

D. 45

A
  1. Approximately ____ minutes after exiting CPDLC and/or ADS-C service areas, the flight crew should ensure there are no active CPDLC or ADS-C connections.

A. 15

B. 30

C. 40

D. 45

Ref: GOLD Manual, Para 5.2.5.2

25
Q
  1. A speed brake lever position of less than ____ degrees is not recommended, due to a tendency to over-control at these settings.

A. 20

B. 30

C. 40

D. 50

A
  1. A speed brake lever position of less than ____ degrees is not recommended, due to a tendency to over-control at these settings.

A. 20

B. 30

C. 40

D. 50

Ref: T.O. 1C-135(K)R(II)-1, Page 2-91, Note

26
Q
  1. Prior to initiating turns, visually check for other traffic. The first turn should not be initiated until _____________.

A. Reaching minimum traffic pattern (maneuver) speed

B. A safe altitude

C. Passing the end of the runway

D. All of the above

A
  1. Prior to initiating turns, visually check for other traffic. The first turn should not be initiated until _____________.

A. Reaching minimum traffic pattern (maneuver) speed

B. A safe altitude

C. Passing the end of the runway

D. All of the above

Ref: T.O. 1C-135(K)R(II)-1, Page 2-100, Warning

27
Q
  1. N1 settings, pattern, approach, and reference speeds will be recomputed when:
    (1) Gross weight changes >/= ____ pounds
    (2) Temperature changes >/= ____ (5F)
    (3) Pressure altitude changes >/= ____ feet
    (4) Airplane configuration changes
    (5) Changes in wind conditions require an adjustment to the charted speeds

A. 5,000; 5C; 500 feet

B. 10,000; 3C; 250 feet

C. 10,000; 3C; 500 feet

D. 5,000; 2C; 500 feet

A
  1. N1 settings, pattern, approach, and reference speeds will be recomputed when:
    (1) Gross weight changes >/= ____ pounds
    (2) Temperature changes >/= ____ (5F)
    (3) Pressure altitude changes >/= ____ feet
    (4) Airplane configuration changes
    (5) Changes in wind conditions require an adjustment to the charted speeds

A. 5,000; 5C; 500 feet

B. 10,000; 3C; 250 feet

C. 10,000; 3C; 500 feet

D. 5,000; 2C; 500 feet

Ref: T.O. 1C-135(K)R(II)-1, Page 2-104, Note