FCF Exam Flashcards

1
Q

Under what flight conditions should a FCF be flown?

a. VMC only
b. Local flying area only
c. Daylight hours only
d. All the above

A

d. All the above

3710. 7T - 3.8.2

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2
Q

Who, if anyone, can authorize a FCF to be flown in combination with an operational flight?

a. Q.A.
b. Maintenance Officer
c. Commanding Officer
d. Operations Officer
e. “Check and go” flights are prohibited

A

c. Commanding Officer

COMNAVAIRFORINST 4790.2A – 5.1.1.4.3.2

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3
Q

Satisfactory completion of an item on a FCF checklist is denoted by

a. An “X”
b. A checkmark
c. Circling the item number
d. Anyone of the above methods is permissible

A

b. A checkmark

C-40A Checkflight Manual – pg 1.1

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4
Q

An unsatisfactory item that fails to meet published FCF criteria is denoted on the checklist by

a. An “X”
b. A checkmark
c. Circling the item number
d. Any one of the above methods is permissible

A

a. An “X”

C-40A Checkflight Manual – pg 1.1

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5
Q

If necessary to accomplish the assigned mission, a FCF may be flown at night with permission of the Commanding Officer.

A

True …………………………….. (3710.7T - 3.8.2)

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6
Q

The Commanding Officer may delegate authority to conduct FCFs under conditions other than daylight VMC.

A

False …………………………….. (3710.7T - 3.8.2)

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7
Q

Any NATOPS qualified aircraft commander may serve as pilot-in-command on a FCF without specific written designation.

A

False …………………………….. (3710.7T - 3.8.1)

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8
Q

Appropriate maintenance quality assurance and project specialist personnel required to accomplish the FCF may be utilized, provided they meet the minimum aviation physiology and water survival training requirements.

A

True …………………………….. (3710.7T - 3.8.1)

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9
Q

IAW the C-40A NATOPS Flight Manual, any NATOPS qualified pilot may occupy the left seat and conduct
the takeoff and landing on an FCF at the discretion of the assigned FCF aircraft commander.

A

False …………………………….. (C-40A NATOPS Flight Manual – pg 10-1)

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10
Q

In the interest of safety, FCF flights should be conducted with maximum crew allowed by NATOPS.

A

False …………………………….. (3710.7T - 3.8.1)

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11
Q

Passengers may be carried during “check and go” FCFs.

A

False …………………………….. (3710.7T - 3.8.1)

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12
Q

When an aircraft has not flown in 30 or more days a FCF is required.

A

True …………………………….. (COMNAVAIRFORINST 4790.2A – 5.1.1.4.2 (j))

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13
Q

IAW COMFLELOGSUPPWINGINST 4790.6P, FCFs performed for acceptance/transfer inspections may
have check items tailored provided the transferring and accepting commands are in concurrence.

A

False …………………………….. (COMFLELOGSUPPWINGINST 4790.6P – pg 7)

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14
Q

The desired Dutch Roll bank angle for yaw damper checks is _____ degrees maximum.

A

10 ……………………………. (C-40A Checkflight Manual – pg 1.58)

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15
Q

During Stall Warning check, if stick shaker has not actuated by _____ knots below chart value, or if _______
_______ occurs, discontinue test to prevent ____________.

A

5, stall buffet, stall ………….. (C-40A Checkflight Manual – pg 1.61)

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16
Q

Stick shaker speeds (Vss) listed in Figure 10 of the C-40 FCF checklist assumes _______ _______-_______
has been on for over ______ seconds.

A

wing anti-ice, 5 ……………… (C-40A Checkflight Manual – pg 1.65)

17
Q

List the recovery procedure for the C-40 Stall Warning Check Maneuver:
At buffet or stick shaker:
a. Apply __________________ thrust.
b. Smoothly decrease ___________ attitude to approximately ____ degrees ___________ the horizon.
c. ___________ wings.
d. Accelerate to ______________ speed for flap setting.
e. ___________ descent and return to ____________ ________________ .

A

a. maximum ……………… (C-40A Checkflight Manual – pg 1.64)
b. pitch, 5, above
c. Level
d. maneuvering
e. Stop, target altitude

18
Q

During the Rejected Takeoff check ensure the cabin door is ________ and ___________.

A

closed, locked ………….…… (C-40A Checkflight Manual – pg 1.79)

19
Q

During the Rejected Takeoff check, accelerate the airplane to greater than _____ knots ground speed prior to
rejecting takeoff.

A

90 …………………….………. (C-40A Checkflight Manual – pg 1.79)

20
Q

During the Fire Switch Shutdown check the Engine Start Lever should be placed to CUTOFF prior to ____%
N2 or after _____% N2 during engine spool down to prevent EEC faults.

A

20, 8 …………………………. (C-40A Checkflight Manual – pg 1.81)