Airplane general Flashcards

1
Q

What is approximately the minimum pavement width for a 180 turn?

a) 20 m.
b) 24 m.
c) 30 m.
d) 33 m.

A

24 m.

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2
Q

What is the maximum flight altitude?

a) 35.000 ft.
b) 37.000 ft.
c) 41.000 ft.
d) 44.000 ft.

A

41.000 ft.

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3
Q

What is the location of the logo Iights?

a) In the wing tips, just in front of the strobe lights.
b) On the top of each horizontal stabilizer.
c) In the inner flap track fairings.
d) In the outer flap track fairings.

A

On the top of each horizontal stabilizer.

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4
Q

What is approximately the wingspan of a Boeing 737-800 (with winglets)?

a) 35,8 m.
b) 28,9 m.
c) 36,2 m.
d) 29,8 m.

A

35,8 m.

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5
Q

What is the speed limit to extend the outboard landing lights?

a) 320 kt/ M.82
b) 280 kt/ M.70
c) 270 kt/ M.70
d) No limitations.

A

No limitations.

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6
Q

Select the correct statement regarding the taxi light.
a) The light extinguishes automatically when the gear retracts
b) It is recommended not to use the light for takeoff and landing because it does not
extinguish automatically.
c) The light shines forward in a fixed position.
d) It consists of two lights, both mounted on the nose wheel strut. Both controlled by
one switch.

A

The light extinguishes automatically when the gear retracts

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7
Q

What is the location of the runway turnoff lights?

a) On the nose gear.
b) In the lower airplane fuselage
c) In the wing tips, just in front of the strobe lights.
d) In the wing-root, adjacent to the fixed lights

A

In the wing-root, adjacent to the fixed lights

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8
Q

With the FASTEN BELT switch in AUTO the FASTEN BELT signs will illuminate?

a) When the landing gear lever is DOWN or TE FLAPS are NOT UP.
b) Only when the landing gear lever is in the DOWN position.
c) Only when the flaps are not in the UP position.
d) Both the landing gear and the flaps must be extended.

A

When the landing gear lever is DOWN or TE FLAPS are NOT UP.

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9
Q

What determines the correct eye reference position?

A

When looking over the glare shield a small amount of airplane nose structure must
be visible and your view of the instrument panel’s A/P-A/T-FMC lights and EHSI must
be unobstructed.

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10
Q

Which statement concerning circuit breaker panels P6 and P18 is true?

A

P6 is located behind the F/O’s seat and P18 behind the Capt’s seat.

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11
Q

When do the overwing emergency exits lock?
a) When three of the four Entry/Service doors are closed.
b) Either engine is running
c) The airplane air/ground logic indicates that the airplane is in the air or both thrust
levers are advanced.
d) All above conditions must be met.

A

All above conditions must be met.

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12
Q

The aircraft water system is supplied by:
a) One main water tank with separate tanks for the toilets.
b) A single water tank located behind the aft cargo compartment.
c) Two water tanks located either side of the aft cargo compartment.
d) One water tank in front of the forward cargo compartment for the forward galley and
toilet, one water tank behind the aft cargo compartment for the aft galley and toilets.

A

A single water tank located behind the aft cargo compartment.

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13
Q
.The passenger oxygen system is activated automatically when the cabin reaches
an altitude of:
a) 9,500 Feet.
b) 10,000 Feet.
c) 12,000 Feet.
d) 14,000 Feet.
A

14,000 Feet.

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14
Q
Each passenger oxygen generator when activated, will produce oxygen for
approximately:
a) 7 minutes.
b) 12 minutes.
c) 17 minutes.
d) 20 minutes.
A

12 minutes.

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15
Q

The system pressure of the flight crew oxygen system may be as high as:

a) 1500 P.S.I.
b) 1850 P.S.I.
c) 2000 P.S.I.
d) 2250 P.S.I.

A

1850 P.S.I.

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16
Q

A fire axe is located in:

a) The flight deck.
b) The forward galley.
c) The aft galley.
d) Both A and C are correct.

A

The flight deck.

17
Q

With how many escape straps/ropes is the Boeing 737-800 equipped?

a) 2, only in the cockpit.
b) 4, two in the cockpit and two in the cabin.
c) 6, two in the cockpit and four in the cabin.
d) 8, two in the cockpit and six in the cabin.

A

4, two in the cockpit and two in the cabin.

18
Q

Which statement is correct regarding EMERGENCY EXIT LIGHTS switch position?
a) OFF position prevents emergency light system operation if the airplane electrical
power fails or is turned off.
b) Armed position illuminates all emergency lights if AC bus 1 fails.
c) ON position illuminates only emergency lights in cabin.
d) ON position illuminates only flight deck emergency lights

A

OFF position prevents emergency light system operation if the airplane electrical
power fails or is turned off.

19
Q

Where on the flight deck is the flight crew oxygen pressure displayed?

a) At the oxygen cylinder
b) At the flight crew oxygen shutoff valve.
c) At the flight crew oxygen pressure indicator on the aft overhead panel
d) Behind the Captains seat on the P18 panel.

A

At the flight crew oxygen pressure indicator on the aft overhead panel

20
Q

The oxygen mask release levers when squeezed and pulled,

a) Release the mask from their stowage boxes.
b) Activate the oxygen and microphone when the stowage box door closes.
c) Inflate the mask harness when the left lever is squeezed.
d) Activate oxygen flow momentarily to test the regulator.

A

Release the mask from their stowage boxes.

21
Q

.Interior emergency exit lights are located:

a) On the lower inboard corner of the stowage bins.
b) Over the entry/service and overwing emergency hatches.
c) In the ceiling.
d) All of the above.

A

All of the above

22
Q

The EMERGENCY EXIT light switch in the ARMED position:
a) Activates the emergency light system with APU generator power only.
b) Illuminates all emergency lights all the time.
c) Illuminates all interior and exterior emergency lights if there is a loss of electrical
power on DC bus 1, or if AC power has been turned off.
d) Can be reset by switching from ON to ARMED.

A

Illuminates all interior and exterior emergency lights if there is a loss of electrical
power on DC bus 1, or if AC power has been turned off.

23
Q

The flight crew oxygen mask EMERGENCY/TEST selector when rotated to the
EMERGENCY position:
a) Supplies 100% oxygen under positive pressure at all cabin altitudes.
b) Test positive pressure supply to the regulator.
c) Provides a mixture of ambient air with oxygen on demand.
d) Supplies 100% oxygen only at high altitudes.

A

Supplies 100% oxygen under positive pressure at all cabin altitudes