Systems Limitations Flashcards

1
Q

What is the maximum takeoff and landing tailwind?

A

10 knots

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2
Q

What is the maximum operating altitude?

A

41,000’

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3
Q

What is the maximum flap extension altitude?

A

20,000’

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4
Q

What is the maximum turbulent air penetration airspeed below 10,000 MSL?

A

250 KIAS

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5
Q

What is the maximum turbulent air penetration airspeed at or above 10,000 MSL?

A

270 KIAS / 0.76M, whichever is lower.

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6
Q

What is the maximum gear extension speed (V lo)?

A

250 KIAS

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7
Q

What is the maximum gear retraction speed (V lo)?

A

250 KIAS

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8
Q

What is the maximum gear extended speed (V le)?

A

250 KIAS

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9
Q

What is the maximum tire ground speed?

A

195 knots

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10
Q

What is the maximum Flaps 1 operating speed?

A

230 KIAS

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11
Q

What is the maximum Flaps 2 operating speed?

A

215 KIAS

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12
Q

What is the maximum Flaps 3 operating speed?

A

200 KIAS

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13
Q

What is the maximum Flaps 4 operating speed?

A

180 KIAS

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14
Q

What is the maximum Flaps 5 operating speed?

A

180 KIAS

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15
Q

What is the maximum Flaps Full operating speed?

A

165 KIAS

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16
Q

What is design maneuvering speed (V a)?

A

Below 240 KIAS

(Full application of rudder and aileron controls, as well as maneuvers that involve angles of attack near the stall, must be confined to speeds below 240 KIAS)

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17
Q

What is the definition of icing conditions?

A

A Static Air Temperature (SAT) on the ground or at takeoff OR a Total Air Temperature (TAT) in flight of 10ºC or below, AND visible moisture is present OR ramp, taxiway or runway surfaces are contaminated.

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18
Q

What is the definition of Visible Moisture?

A

The presence of Clouds, Fog, Visibility 1 SM or less, Mist, Rain, Snow, Sleet or Ice Crystals

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19
Q

What is the definition of a Contaminated Surface?

A

A Ramp, Taxiway and/or Runway with Snow, Ice, Standing Water or Slush on it.

20
Q

What must the MCDU DATASET MENU be set to when the SAT is 10ºC or below and icing conditions exist or are anticipated to be encountered below 1,700 AFE?

A

ALL

21
Q

What is the maximum windshield operating airspeed?

A

250 KIAS

22
Q

What is the maximum fuel imbalance between tanks?

A

790 lbs

23
Q

When must the XFEED Selector be set to OFF?

A

During takeoff and landing

24
Q

What is the maximum altitude for single pack operation?

A

31,000’

25
Q

When is the activation of Landing Gear Downlock Release Button prohibited?

A

During all takeoffs, unless obstacle clearance is required.

26
Q

En route use of flaps are __________

A

prohibited.

27
Q

True or False:

Do not hold in icing conditions with flaps extended.

A

True

28
Q

True or False:

Hold in icing conditions with flaps extended.

A

False

29
Q

True or False:

The use of Flaps 4 during approach and landing is prohibited.

A

True

30
Q

Thrust reversers must be stowed below what airspeed?

A

60 KIAS

31
Q

True or False:

LOC BC approaches using IESS are not authorized.

A

True

32
Q

What is the minimum engagement height for the autopilot?

A

400’ AGL

33
Q

What is the Minimum Use Height (ILS approach) for the autopilot?

A

50’ AGL

34
Q

What is the Minimum Use Height (Non-precision) for the autopilot?

A

MDA (DA)

35
Q

Before applying takeoff thrust, allow the engines to warm up for a minimum of how many minutes?

A

2 minutes

36
Q

How long must an engine cool down prior to shutting down?

A

2 minutes

37
Q

Single engine taxi is not authorized when:

A
  • Braking action is less than GOOD;

* RVR is less than 1,200’

38
Q

What are the EICAS Engine Limit Display Markings?

A

Red - Max and Min Limitations
Amber - Caution Range
Green - Normal Operating Range

39
Q

Reduced thrust takeoffs are prohibited when:

A
  • The runway is contaminated with standing water, slush, snow or ice;
  • Windshear is present or suspected;
  • Performance mandates no FLEX
40
Q

The use of reduced takeoff thrust procedures is not allowed on:

A
  • Runways contaminated with standing water, slush, snow or ice;
  • Wet runways UNLESS suitable performance accountability is made for the increased stopping distance on the wet runway surface.
41
Q

Does the “wet” runway analysis numbers take into account the increased stopping distance that occurs on wet runways?

A

Yes

42
Q

What is the maximum altitude for APU operation?

A

33,000’

43
Q

What is the maximum altitude for APU start?

A

30,000’

44
Q

Up to what altitude may the APU assist in engine start?

A

21,000’

45
Q

What is the maximum altitude for operation of the APU bleed?

A

15,000’