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E175 SV (updated to v5.2) > Memory Items > Flashcards

Memory Items Flashcards

1
Q

Regarding runway width, the normal width for takeoff and landing is _____ feet, and narrow width(including plowed width) for takeoff and landing is ______ feet.

A

100 ft
60 ft (66ft for takeoff)

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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 tailwind limit for normal runway widths (100’ or greater) and all runway conditions?

A

15 Kts (except autoland)

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20
Q

The maximum crosswind limit for normal runway widths (100’ and greater) with a braking action “Good” / 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.?

22
Q

What is the maximum permitted imbalance between fuel tanks?

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.

25
The maximum altitude allowed for starting the APU is _____ feet.
30,000 ft
26
The maximum altitude allowed for operating the APU is _____ feet, including with the generator in operation.
33,000 ft
27
The maximum altitude allowed for operating the APU bleed air is _____ feet.
15,000 ft
28
The maximum altitude allowed for APU air start assist is _____ feet.
21,000 ft
29
The cooling periods after each APU start attempt are _____ for the first and second attempts and _____ for the third attempt.
60 sec. off 5 min. Off
30
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.
5 min.
31
What is the minimum oil temperature for engine start?
-40 degrees Celsius
32
Dry motoring duty cycle limits are _____ seconds for the first motoring and _____ seconds maximum time for the 2nd through 5th motorings, each with a 5 minute cooldown time.
90 sec. 30 sec.
33
With regard to starting duty cycle limits (NOT dry motoring limits), motoring numbers 1 and 2 are limited to _____ on the ground and _____ in flight, with a _____ cooldown.
90 sec. 120 sec. 10 sec.
34
With regard to starting duty cycle limits (NOT dry motoring limits), motoring numbers 3 through 5 are limited to _____ on the ground and _____ in flight, with a _____ cooldown.
90 sec. 120 sec. 5 min.
35
What is the maximum differential pressure?
8.4 psi
36
What is the maximum differential overpressure?
8.8 psi
37
What is the maximum differential negative pressure?
-.5 psi
38
What is the maximum differential pressure for takeoff and landing?
.2 psi
39
True or False: There is no temperature limitation for automatic operation of the anti-icing system.
True
40
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.
5 to 10 degrees Celsius
41
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.
5 degrees Celsius
42
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.
AUTO 10 degrees Celsius TAT
43
The autopilot’s minimum engagement height is _____ feet and minimum use height is _____ feet.
400 ft 50 ft
44
Which of the following are limitations of the aircraft’s WiFi system?
A flight attendant shall be on board and part of the crew during operation of the wifi system.
45
Which of the following are limitations of flight deck power?
Only company-issued devices and personal cell phones may be connected to flightdeck power. 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
Which of the following is a correct statement regarding the use flightdeck power and phase of flight?
Flightdeck power shall not be used during critical phases of flight.
47
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.
True
48
Autoland operation shall be performed with flaps _____.
5
49
Maximum wind component speeds for Autoland operations is _____ kts. headwind, _____ kts. crosswind, and _____ kts tailwind.
25 kts 15 kts 10kts
50
The maximum landing weight for aircraft without 89,000 lbs is _____.
74,957 lbs

E175 SV (updated to v5.2) (23 decks)

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