SCA 737 Limitations Flashcards

Learn Sun Country 737 Limitations

1
Q

Max Runway Slope

A

+/-2%

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2
Q

Max Takeoff Tailwind Component

A

10 Knots

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3
Q

Max Landing Tailwind Component

A

10 Knots

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4
Q

Max Autoland Headwind Component

A

25 Knots

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5
Q

Max T/O and LDG X-Wind Component

A

34 Knots w/ Winglets 36 knots w/o Winglets

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6
Q

Max Autoland X-Wind Component

A

15 Knots

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7
Q

Max Operating Altitude

A

41,000’

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8
Q

Max T/O and LDG Altitude

A

8,400’ Pressure Alt.

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9
Q

Max In Flight Difference for RVSM

A

200’ Captain and FO

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10
Q

Max Ground Difference for RVSM

A

50’ Captain and FO

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11
Q

Max Difference Field Elevation

A

75’ Captain or FO

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12
Q

Flaps Up Max Load Factor

A

+2.5G to -1.0G

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13
Q

Flaps Down Max Load Factor

A

+2.0G to 0.0G

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14
Q

Max Taxi Weight

A

174,700 lbs

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15
Q

Max T/O Weight

A

174,200 lbs

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16
Q

Max Landing Weight

A

146,300 lbs

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17
Q

Max Zero Fuel Weight

A

138,300 lbs

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18
Q

Max Flap Ext Speed 1

A

250 knots

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19
Q

Max Flap Ext Speed 2

A

250 knots

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20
Q

Max Flap Ext Speed 5

A

250 knots

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21
Q

Max Flap Ext Speed 10

A

210 knots

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22
Q

Max Flap Ext Speed 15

A

200 knots

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23
Q

Max Flap Ext Speed 25

A

190 knots

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24
Q

Max Flap Ext Speed 30

A

175 knots

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25
Q

Max Flap Ext Speed 40

A

162 knots

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26
Q

Max Flap Ext Altitude

A

20,000’

27
Q

Holding with Flaps Extended

A

Prohibited

28
Q

Flaps Cat II/III

A

40

29
Q

VLO (Ret)

A

235 knots

30
Q

VLE (Ext)

A

270/.82

31
Q

VLE

A

320/.82

32
Q

Oxygen 2 Crew

A

735 psi

33
Q

Oxygen 3 crew

A

1,055 psi

34
Q

WX Limits for T/O

A

Prohibited in

Moderate or Heavy Freezing Rain

Heavy Ice Pellets

Hail

35
Q

Autopilot Min Alt for T/O

A

1,000’ AGL

36
Q

Autopilot Min Alt Enroute

A

1,000’ AGL

37
Q

Autopilot Min Alt ILS Coupled Approach

A

50’ AGL

38
Q

Autopilot Min Altitude ILS-Autoland

A

After Touchdown

39
Q

Autopilot Min Altitude Non-Precision Approach

A

50’ below MDA, VNAV DA

40
Q

Aileron Trim with A/P Engage

A

Prohibited

41
Q

Arming VNAV on the ground

A

Prohibited

42
Q

Headsets

A

Req’d below 18,000’, except as permitted by MEL

43
Q

Engine Limits

A

Max and Min Limits in Red

Caution in Amber

Normal in White Arc

44
Q

Engine EGT Limit for T/O

A

950C for 5 Minutes

45
Q

Engine EGT Max Cont

A

925C

46
Q

Engine EGT Starting

A

725C

47
Q

Engine Oil Quantity for Dispatch

A

12 quarts prior to start

48
Q

Engine Oil in Amber

A

Operation limited to 45 minutes.

If in Amber with T/O Thrust, do not take off.

49
Q

Engine Ignition

A

Must be on for:

Takeoff Landing

Operation in Heavy Rain

Anti-Ice Operation

Severe Turbulence

50
Q

Reverse Thrust

A

Prohibited in Flight

51
Q

Alternate Mode EEC

A

Reduced or Derated Thrust is not allowed when EEC is in the Alternate Mode.

Reduced Thrust is not allowed when:

Antiskid is inoperative or off.

Runways are contaminated with standing water, ice, slush or snow.

52
Q

APU Bleed and Electrical Load, Flight

A

Max Altitude 10,000’

53
Q

APU Bleed and Electrical Load, Ground

A

Max Altitude 15,000’

54
Q

APU Bleed

A

Max Altitude 17,000’

55
Q

APU Electrical Load

A

Max Altitude 41,000’

56
Q

APU Bleed Valve Closed When

A
  1. Ground Air Connected and isolation valve open.
  2. Engine #1 Bleed Valve Open.
  3. Isolation and Engine #2 Bleed Valves Open.
57
Q

APU

A

APU Bleed may be open during start, but avoid engine power above idle.

After 3 aborted start attempts, a 15 minute cooling period is required.

58
Q

Speed Brakes

A
  1. Do not deploy below 1,000’ RA.
  2. Do not extend past Flight Detent in flight
59
Q

Flight Controls

A

Avoid rapid and large alternating control inputs.

May cause structural failure at any speed.

60
Q

Fuel Tank Temps

A

Maximum: 49C

Minimum: -43C

Jet B prohibited

61
Q

Fuel Balance

A

Lateral imbalance between tanks 1 and 2 must be scheduled to be zero.

Random imbalance must not exceed 1,000 lbs for taxi, takeoff, flight or landing.

62
Q

Fuel Loading

A

Main Tanks 1 & 2 must be full if center tank contains more than 1,000 lbs.

63
Q

Center Fuel Tank Switches

A

Must be OFF:

  1. for ground ops, unless center tank > 1,000 lbs, except when defueling or x-ferring fuel.
  2. for ground and flight ops when first center tank fuel pump low press light comes on, if center tank is empty.
64
Q

Center Tank Fuel Pump

A

Dry Running is Prohibited.