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E175 > 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 _____

A

100; less than 100 feet to 66 feet (narrow takeoff), less than 100 feet to 60 feet (narrow landing).

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2
Q

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

A

75,177

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3
Q

The maximum landing weight for aircraft without 89,000-lb placard is ___.

A

74,957

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4
Q

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

A

True

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5
Q

What is the minimum battery temperature?

A

-20°C

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6
Q

What is the maximum altitude for flap extension?

A

20,000 feet

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7
Q

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

A

250 KIAS

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8
Q

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

A

250 KIAS

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9
Q

What is VLE (landing gear extended speed)?

A

250 KIAS

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10
Q

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

A

160 KIAS

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11
Q

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

A

250 KIAS

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12
Q

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

A

270 KIAS / 0.76 M,  whichever is lower.

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13
Q

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

A

230 KIAS

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14
Q

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

A

215 KIAS

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15
Q

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

A

200 KIAS

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16
Q

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

A

180 KIAS

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17
Q

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

A

165 KIAS

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18
Q

What is the maximum tire ground speed?

A

195 KIAS

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19
Q

What is the maximum windshield wiper operating speed?

A

250 KIAS

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20
Q

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

A

15 knots

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21
Q

The maximum crosswind limit for normal runway widths (100’ and greater) with a breaking action “Good”/RwyCC value of 6 (dry) is ___.

22
Q

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

23
Q

What is the maximum permitted imbalance between fuel tanks?

24
Q

What is the minimum fuel tank temperature?

25
True or False: the fuel crossfeed selector knob is NOT required to be set to OFF during takeoff and landing.
False
26
The maximum altitude allowed for starting the APU is___ feet.
30,000
27
The maximum altitude allowed for operating the APU is ___ feet, including with the generator in operation.
33,000
28
The maximum altitude allowed for operating the APU bleed air is ___ feet.
15,000
29
The maximum altitude allowed for APU air start assist is ___ feet.
21,000
30
The cooling periods after each APU start attempt are___ for the first and second attempts and ___for the third attempt.
60 seconds OFF; 5 minutes OFF
31
Due to the potential of drained batteries caused by an unexpected APU shut down and the lack of automatic fire protection, the APU shall not be left unattended for longer than ___ minutes.
5
32
What is the minimum oil temperature for engine start?
-40°C
33
Dry motoring duty cycle limits are ___ seconds maximum time for the first motoring and ___ seconds maximum time for the 2nd through 5th motoring, each with the 5 minute cool-down time.
90; 30
34
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 ___ cool down.
90  seconds; 120 seconds; 10 second
35
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 ___ cool down.
90 seconds; 120 seconds; 5 minute
36
What is the maximum differential pressure?
8.4 PSI
37
What is the maximum differential overpressure?
8.8 PSI
38
What is the maximum negative differential pressure?
-0.5 PSI
39
What is the maximum differential pressure for takeoff and landing? 
0.2 PSI
40
True or False: there is no temperature limitation for automatic operation of the anti-icing system.
True
41
On the ground, the TO DATASET MENU on the MCDU must be set to ENG when OAT is between ___ if there is a possibility of encountering visible moisture to 1,700 feet 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°C and 10°C
42
On the ground, the TO DATASET MENU on the MCDU must be set to ALL when OAT is below ___ if there is a possibility of encountering visible moisture to 1,700 feet 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°C
43
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°C TAT
44
The autopilot’s minimum engagement height is ___ feet and minimum use height is ___ feet.
400; 50
45
Which of the following are limitations of the aircraft’s Wi-Fi system?
A FA shall be onboard and part of the crew during operation of the Wi-Fi system
46
Which of the following are limitations of flightdeck power?
Shall not be used during critical phases of flight. Use is limited to company-issued devices and personal cell phones only. While charging company iPad’s, do not position cord as to impede movement of any flight controls or restrict emergency egress paths.
47
Which of the following is a correct statement regarding the use of flight deck power and phase of flight?
Shall not be used during critical phases of flight
48
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
49
Autoland operation shall be performed with flaps ___.
5
50
Maximum wind component speeds for autoland operations is ___ kts. headwind, ___ kts. crosswind, and ___ kts tailwind.
25; 15; 10

E175 (1 decks)

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