Limitations 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

38
Q

AUTOLAND
Maximum allowable wind speeds when landing weather minima are predicated on autoland operations?

FOM 3.2.3

A

Headwind 25 knots;
Tailwind 10 knots;
Maximum crosswind 20 knots; and
Autoland capability may only be used with flaps 30 or 40 and both engines
operative.
Not authorized for overweight landings.
The maximum and minimum glideslope angles are 3.25 and 2.5 degrees, respectively.

39
Q

Engine Warm Up Requirement

FOM 4.5.1

A

(B737NG) Verify an increase in engine oil temperature before takeoff

(B737MAX) Verify engine oil temperature is at or above 31°C before takeoff

Run the engine, for at least 2 minutes (B737NG) or 3 minutes (B737MAX), using a
thrust setting normally used for taxi operations before applying takeoff thrust