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C-40A Clipper > Pilot Closed Book > Flashcards

Pilot Closed Book Flashcards

1
Q

Holding in icing conditions with flaps extended is acceptable..

A

False

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2
Q

Intentional selection of reverse thrust inflight is prohibited.

A

True

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3
Q

Backing up with reverse thrust is prohibited.

A

True

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4
Q

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or
yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA
(design maneuvering speed).

A

True

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5
Q

The use of Fuel System Icing Inhibitor changes the minimum fuel tank temperature limit.

A

False

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6
Q

Installation of handle covers on the over wing exits must be verified prior to departure whenever passengers
are carried.

A

True

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7
Q

With engine bleed air switches ON, do not operate the air conditioning packs in HIGH for takeoff, approach
or landing.

A

True

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8
Q

Do not apply brakes until after touchdown

A

True

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9
Q

Refueling with either engine turning (hot refueling) is prohibited.

A

True

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10
Q

Intentional running of a center tank fuel pump (low pressure light illuminated) is acceptable..

A

False

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11
Q

The maximum takeoff and landing tailwind component is _______ knots.

a. 5
b. 10
c. 15
d. 20

A

c. 15

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12
Q

Do not operate ________ during refueling operation.

a. Transponder test
b. Weather radar test
c. HF radios
d. GPWS test

A

c. HF radios

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13
Q

For single channel operation during approach, the autopilot shall not remain engaged below ______ feet AGL.

a. 1,000
b. 200
c. 100
d. 50

A

d. 50

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14
Q

Maximum allowable headwind when utilizing autoland is _______ knots.

a. 50
b. 30
c. 25
d. 15

A

c. 25

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15
Q

Maximum allowable crosswind when utilizing autoland is _______ knots.

a. 30
b. 25
c. 20
d. 15

A

c. 20

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16
Q

Maximum and minimum glideslope angles for autoland are _______ degrees respectively.

a. 3.5 and 2.5
b. 3.25 and 2.5
c. 3.25 and 2.0
d. 3.0 and 2.0

A

b. 3.25 and 2.5

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17
Q

Autoland capability may only be used to runways at or below _______ feet pressure altitude.

a. 10,400
b. 10,000
c. 8,500
d. 8,400

A

d. 8,400

18
Q

Engine ignition must be on for:

a. Takeoff
b. Landing
c. Operation in heavy rain
d. Anti-ice operation
e. All of the above

A

e. All of the above

19
Q

Severe turbulent air penetration airspeed is _______knots or _____ Mach; whichever is lower. Applicable to ______ and ______ only.

a. 300 / .77 / climb / cruise
b. 280 / .77 / climb / cruise
c. 250 / .76 / climb / descent
d. 280 / .76 / climb / descent

A

d. 280 / .76 / climb / descent

20
Q
  1. When utilizing the APU inflight the maximum altitude for bleed only is __feet.
    a. 15,000
    b. 16,000
    c. 17,000
    d. 20,000
A

c. 17,000

21
Q

When utilizing the APU inflight the maximum altitude for electrical load only is ________feet.

a. 15,000
b. 17,000
c. 38,000
d. 41,000

A

d. 41,000

22
Q

Maximum altitude for flap extension is _________ feet.

a. 30,000
b. 20,000
c. 10,000
d. 8,400

A

b. 20,000

23
Q

Do not deploy the speed brakes in flight at radio altitudes less than ______ feet.

a. 2,500
b. 2,000
c. 1,500
d. 1,000

A

d. 1,000

24
Q

Do not operate the weather radar in a hangar or within ____ feet of a fuel spill. This hangar restriction does
not apply to the weather radar test mode.
a. 50
b. 100
c. 150
d. 200

A

a. 50

25
Q

The maximum Landing Weight is ___________ pounds.

a. 136,000
b. 135,000
c. 134,000
d. 133,000

A

c. 134,000

26
Q

The maximum Zero Fuel Weight is __________ pounds.

a. 130,000
b. 126,000
c. 124,000
d. 121,500

A

b. 126,000

27
Q

Engine TAI must be on when icing conditions exist or are anticipated, except during climb and cruise below ______ degrees Celsius SAT.

a. 40
b. 10
c. -40
d. -10

A

c. -40

28
Q

Icing conditions exist when ___________.

a. TAT is 10 degrees C or below, and visible moisture is present
b. TAT is 10 degrees C or below and standing water, ice or snow is present on the ramps, taxiways, or runways
c. Both A and B
d. None of the Above

A

c. Both A and B

29
Q

Operation information listed in the FCOM Volume 1 limitations chapter that must be memorized (memory items) are marked with a _____ symbol.

a. *
b. %
c. @
d. #

A

d. #

30
Q

The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is _____ feet.

a. 50
b. 100
c. 200
d. 300

A

c. 200

31
Q

For RVSM operations, the maximum allowable on-the-ground altitude display differences between the Captain and First Officer from sea level to 5000 feet are and from 5001 to 10,000 feet are ______.

a. 50’ and 60’
b. 50’ and 50’
c. 50’ and 100’
d. 50’ and 75’

A

a. 50’ and 60’

32
Q

When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow ______ seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch.

a. 10
b. 15
c. 20
d. 30

A

b. 15

33
Q

When extending or retracting flaps with the ALTERNATE FLAPS position switch and after a complete extend/retract cycle, i.e. 0 to 15 and back to 0, allow ___ minutes cooling before attempting another extension.

a. 2
b. 3
c. 4
d. 5

A

d. 5

34
Q

Flight crews will not reset tripped ______________ circuit breakers.

a. fuel quantity indicator
b. fuel pump
c. fuel pump control
d. all of the above

A

d. all of the above

35
Q

Maximum fuel tank temperature is degrees C.

a. 40
b. 45
c. 47
d. 49

A

d. 49

36
Q

Operation with assumed temperature reduced takeoff thrust is not permitted with ________.

a. Anti-skid inoperative
b. Runways contaminated with standing water, ice, slush or snow
c. Wet runways
d. both a. and b.

A

d. both a. and b.

37
Q

Above 80 knots and prior to V1, the takeoff should be rejected for:

a. A fire or fire warning
b. An engine failure
c. A predictive windshear warning
d. An airplane that is unsafe or unable to fly
e. Any of the above

A

e. Any of the above

38
Q

If an engine fails during a go-around:

a. Perform normal go-around procedures
b. Verify maximum go-around thrust is set
c. Maintain flaps 15, VREF 30 or 40 + wind correction (5 knots maximum) speed and limit bank angle to 15 until initial maneuvering is complete and a safe altitude is reached
d. Accelerate to flap retraction speed by repositioning the command speed to the maneuvering speed for the desired flap setting and adjusting pitch.
e. All of the above

A

e. All of the above

39
Q

Takeoff with light coatings of frost, up to _____ inch _____mm in thickness on lower wing surfaces due to cold fuel is permissible

a. 1/16 , 1.5
b. 1/8, 3
c. 1/4, 6
d. 1/2, 12

A

b. 1/8, 3

40
Q

For the main deck cargo door, do not operate with winds in excess of knots.

a. 30
b. 35
c. 40
d. 45

A

c. 40

C-40A Clipper (9 decks)

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