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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

Runway cleared width for takeoff …….. 100’
Runway cleared width for landing (state of Alaska only) …….. 60’

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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 C

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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

Max 250 KIAS

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11
Q

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

A

Max 270 KIAS / .76 Mach whicever is lower

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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 (Horizon Limiation)

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19
Q

What is the maximum takeoff and landing tailwind component?

A

15 KTS

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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 C

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

26
Q

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

A

33,000

27
Q

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

A

15,000

28
Q

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

A

21,000

29
Q

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

A

60 seconds off
5 minutes off

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 minutes

31
Q

What is the minimum oil temperature for engine start?

A

-40 C

32
Q

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

A

90 seconds
30 seconds

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 seconds on the ground
120 seconds in flight
10 second cooldown

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 seconds on the ground
120 seconds in flight
10 second cooldown

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

-0.5 psi

38
Q

What is the maximum differential pressure for takeoff and landing?

A

0.2 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 C - 10 C

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 C

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 C TAT

43
Q

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

A

400 feet
50 feet

44
Q

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

A

A Flight Attendant shall be onboard and part of the crew during operation of the WiFi system.

45
Q

Which of the following are limitations of flightdeck power?

A

-Flightdeck power shall not be used during critical phases of flight.
-Use of flightdeck power is limited to Company-issued devices and personal cell phones only.
-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 headwind
15 KTS crosswind

50
Q

The maximum tailwind component for Autoland operations is _____ kts.

A

10 KTS tailwind

E175 (2 decks)

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