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E175 > Memory Items > Flashcards

Memory Items Flashcards

1
Q

The runway cleared width for takeoff is _____ feet, and for landing, in the state of
Alaska only, is _____ feet.

A

100 ft
60 ft

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2
Q

The maximum landing weight for aircraft placarded 89,000 lbs. is _____.

A

75,177 lbs

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3
Q

True or False: In the event of a landing below -40 degrees C, the aircraft may not
takeoff without further maintenance analysis / inspection.

A

True

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4
Q

What is the minimum battery temperature?

A

-20 degrees Celsius

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5
Q

What is the maximum altitude for flap extension?

A

20,000 ft

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6
Q

What is VLO (landing gear operation speed) for retraction?

A

250 KIAS

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7
Q

What is VLO (landing gear operation speed) for extension?

A

250 KIAS

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8
Q

What is VLE (landing gear extended speed)?

A

250 KIAS

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9
Q

What is the maximum speed to open the direct vision window?

A

160 KIAS

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10
Q

What is the turbulent air penetration target speed maximum below 10,000 ft.?

A

250 KIAS

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11
Q

What is the turbulent air penetration target speed maximum at or above 10,000 ft.?

A

lesser of: 270 KIAS or .76 M

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12
Q

What is VFE (maximum flaps extended speed) for Flaps 1?

A

230 KIAS

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13
Q

What is VFE (maximum flaps extended speed) for Flaps 2?

A

215 KIAS

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14
Q

What is VFE (maximum flaps extended speed) for Flaps 3?

A

200 KIAS

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15
Q

What is VFE (maximum flaps extended speed) for Flaps 4 and Flaps 5?

A

180 KIAS

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16
Q

What is VFE (maximum flaps extended speed) for Flaps Full?

A

165 KIAS

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17
Q

What is the maximum tire ground speed?

A

195 KIAS

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18
Q

What is the maximum windshield wiper operating speed?

A

250 KIAS

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19
Q

What is the maximum takeoff and landing tailwind component?

A

15 Kts (except autoland)

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20
Q

The maximum crosswind limit for braking action “Good” and a RwyCC value of 6
(dry) is _____.

A

38 kts

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21
Q

What is the maximum N1 allowed with brakes applied and tailwinds greater than
10 kts.?

A

60%

22
Q

What is the maximum permitted imbalance between fuel tanks?

A

794 lbs

23
Q

What is the minimum fuel tank temperature?

A

-37 degrees Celsius

24
Q

True or False: The fuel crossfeed selector knob is NOT required to be set to OFF
during takeoff and landing.

A

False

25
Q

The maximum altitude allowed for starting the APU is _____ feet.

A

30,000 ft

26
Q

The maximum altitude allowed for operating the APU is _____ feet, including with
the generator in operation.

A

33,000 ft

27
Q

The maximum altitude allowed for operating the APU bleed air is _____ feet.

A

15,000 ft

28
Q

The maximum altitude allowed for APU air start assist is _____ feet.

A

21,000 ft

29
Q

The cooling periods after each APU start attempt are _____ for the first and
second attempts and _____ for the third attempt.

A

60 sec.
5 min.

30
Q

Due to the potential of drained batteries caused by an unexpected APU shutdown
and the lack of automatic fire protection, the APU shall not be left unattended for
longer than _____ minutes.

A

5 min.

31
Q

What is the minimum oil temperature for engine start?

A

-40 degrees Celsius

32
Q

Dry motoring duty cycle limits are _____ seconds for the first motoring and _____
seconds for the 2nd through 5th motorings.

A

90 sec.
30 sec.

33
Q

With regard to starting duty cycle limits (NOT dry motoring limits), the first and
second motorings are limited to _____ on the ground and _____ in flight, with a
_____ cooldown.

A

90 sec.
120 sec.
10 sec.

34
Q

With regard to starting duty cycle limits (NOT dry motoring limits), the third through
fifth motorings are limited to _____ on the ground and _____ in flight, with a _____
cooldown.

A

90 sec.
120 sec.
5 min.

35
Q

What is the maximum differential pressure?

A

8.4 psi

36
Q

What is the maximum differential overpressure?

A

8.8 psi

37
Q

What is the maximum differential negative pressure?

A

-.5 psi

38
Q

What is the maximum differential pressure for takeoff and landing?

A

.2 psi

39
Q

True or False: There is no temperature limitation for automatic operation of the
anti-icing system.

A

True

40
Q

On the ground, the TO DATASET MENU on the MCDU must be set to ENG when
OAT is between _____ degrees if there is a possibility of encountering visible
moisture up to 1,700 ft. AFE and when operating on ramps, taxiways, or runways
where surface snow, ice, standing water, or slush may be ingested by the engines,
or freeze on the engines, nacelles, or engine sensor probes.

A

5 to 10 degrees Celsius

41
Q

On the ground, the TO DATASET MENU on the MCDU must be set to ALL when
OAT is below _____ degrees if there is a possibility of encountering visible
moisture up to 1,700 ft. AFE and when operating on ramps, taxiways, or runways
where surface snow, ice, standing water, or slush may be ingested by the engines,
or freeze on the engines, nacelles, or engine sensor probes.

A

5 degrees Celsius

42
Q

With regard to operating in icing conditions, the engine and wing anti-ice systems
operate automatically when the ice protection mode selector is in the _____
position, and if either one or both ice detectors have failed, the crew must set the
mode selector to ON when icing conditions exist or are anticipated below _____
with visible moisture.

A

AUTO
10 degrees Celsius TAT

43
Q

The autopilot’s minimum engagement height is _____ feet and minimum use
height is _____ feet.

A

400 ft
50 ft

44
Q

Which of the following are limitations of the aircraft’s WiFi system?

A

A flight attendant shall be on board and part of the crew during operation of the wifi system.

45
Q

Which of the following are limitations of flightdeck power?

A

Use of flightdeck power is limited to Company-issued devices and personal cell phones only.

Flightdeck power shall not be used during critical phases of flight.

While charging Company iPads, do not position cord as to impede the movement of any flight control or restrict emergency egress paths.

46
Q

Which of the following is a correct statement regarding the use flightdeck power
and phase of flight?

A

Flightdeck power shall not be used during critical phases of flight.

47
Q

True or False: When using flightdeck power, do not position cord as to impede the
movement of any flight control or restrict emergency egress paths.

A

True

48
Q

Autoland operation shall be performed with flaps _____.

A

5

49
Q

Maximum wind component speeds for Autoland operations is _____ kts. headwind
and _____ kts. crosswind.

A

25 kts
15 kts

50
Q

The maximum tailwind component for Autoland operations is _____ kts.

A

10 kts

E175 (23 decks)

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