Limitstions Flashcards

1
Q

Maximum Operating Altitude

3.1.1.2

A

41,000 feet

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2
Q

Maximum Flight Operation Latitude

3.1.1.3

A

82° North and 82° South

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3
Q

Maximum Runway Slope

3.1.1.6.

A

+/- 2%

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4
Q

Take off & landing tail wind - Maximum

3.1.1.7

A

10 knots

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5
Q

Takeoff crosswind - Maximum

3.1.1.7

A

-700/-800 33 knots, -8 35 knots

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6
Q

Landing crosswind - Maximum

3.1.1.7

A

-700/-800 33 knots, -8 32 knots

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7
Q

Land Crosswind limit - BAR - Dry Runway

3.1.1.7

A

-700/-800 33 knots, -8 32 knots

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8
Q

Land Crosswind limit - BAR - Good

3.1.1.7

A

-700/-800 33 knots. -8 32 knots

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9
Q

Land Crosswind limit - BAR - Good to Medium

3.1.1.7

A

All 25 Knots

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10
Q

Land Crosswind limit - BAR - Medium

3.1.1.7

A

All 20 knots

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11
Q

Land Crosswind limit - BAR - Medium to Poor

3.1.1.7

A

All 15 knots

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12
Q

Land Crosswind limit - BAR - Poor

3.1.1.7

A

All 10 knots

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13
Q

Maximum Speeds

3.1.1.10

A

Observe Gear and flap placards

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14
Q

Escape Slide Retention Bar On revenue passenger flights during taxi , takeoff, and landing

3.1.1.11

A

Installed

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15
Q

Autopilot Engaged - Minimum Altitude - Takeoff

3.2.2

A

400 feet AGL

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16
Q

Autopilot Engaged - Minimum Altitude - Single channel operation during approach

3.2.2

A

50 feet AGL

17
Q

Engine Limitations and Display Markings - Maximum and Minimum Limits

3.4.1

A

Red

18
Q

Engine Limitations and Display Markings - Caution Limits

3.4.1

A

Amber

19
Q

Engine Ignition - On

3.4.2

A

Takeoff, Landing, Operation in Heavy Rain & Ant-ice operation

20
Q

Starter Duty Cycle - NG

3.4.3

A

2 Minutes On - 10 seconds between start attempts

21
Q

Starter Duty Cycle - MAX

3.4.3

A

3 Minutes On - 10 seconds between start attempts

22
Q

Reverse Thrust Intentional selection in flights

3.4.4

A

Prohibited

23
Q

APU - Bleed and Electrical Load - Maximum altitude

3.4.5

A

10,000 feet

24
Q

APU - Bleed Only - Maximum altitude

3.4.5

A

17,000 feet

25
Q

APU - Electrical load only - Maximum altitude

3.4.5

A

41,000 feet

26
Q

What must be avoided with a Dual Bleed light illuminated?

A

Thrust must be limited to idle

27
Q

Wide Cut Fuels JP-4 or Jet B

3.5.1

A

Prohibitied

28
Q

Maximum fuel tank temperature

3.5.2

A

49°C

29
Q

Minimum fuel tank temperautre

A

-43° C or 3°C above the freezing point of fuel being used. Whichever is higher.

30
Q

Fuel Imbalance - Allowable lateral imbalance between main and tanks 1 and 2

3.5.3

A

Must be scheduled to be zero

31
Q

Random fuel imbalance for taxi, takeoff, flight or landing

3.5.3

A

Must not exceed 1,000 lbs

32
Q

Maximum flap extension altitude

3.6.1

A

20,000 feet

33
Q

Holding in icing conditions with flaps extended

3.6.1

A

Prohibited

34
Q

Under what conditions must engine anti-ice be selected on?

A

When icing conditions exist or are anticipated, except during climb and cruise below -40°C SAT. Icing conditions are defined as, the ambient temperature is +10°C or below and any of the following conditions exist; Visible moisture such as clouds or fog with visibility less than 1nm, rain, snow, sleet, or ice crystals; Standing water, ice, snow, is present on ramps, taxiways, or runways.

35
Q

Speedbrakes - Minimum radio altitudes for deployment in flight

3.6.2

A

1,000 feet

36
Q

Under what conditions are reduced thrust takeoffs not permitted?

A

Slippery or contaminated runways, anti skid inop, when special departure procedures specify max Thrust for T/O, wind shear is present, or EEC in alternate mode

37
Q

Maximum Differential

3.9.1

A

9.1 PSI