SCA 737 Limitations Flashcards

Learn Sun Country 737 Limitations (64 cards)

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
Max Flap Ext Speed 40
162 knots
26
Max Flap Ext Altitude
20,000'
27
Holding with Flaps Extended
Prohibited
28
Flaps Cat II/III
40
29
VLO (Ret)
235 knots
30
VLE (Ext)
270/.82
31
VLE
320/.82
32
Oxygen 2 Crew
735 psi
33
Oxygen 3 crew
1,055 psi
34
WX Limits for T/O
Prohibited in Moderate or Heavy Freezing Rain Heavy Ice Pellets Hail
35
Autopilot Min Alt for T/O
1,000' AGL
36
Autopilot Min Alt Enroute
1,000' AGL
37
Autopilot Min Alt ILS Coupled Approach
50' AGL
38
Autopilot Min Altitude ILS-Autoland
After Touchdown
39
Autopilot Min Altitude Non-Precision Approach
50' below MDA, VNAV DA
40
Aileron Trim with A/P Engage
Prohibited
41
Arming VNAV on the ground
Prohibited
42
Headsets
Req'd below 18,000', except as permitted by MEL
43
Engine Limits
Max and Min Limits in Red Caution in Amber Normal in White Arc
44
Engine EGT Limit for T/O
950C for 5 Minutes
45
Engine EGT Max Cont
925C
46
Engine EGT Starting
725C
47
Engine Oil Quantity for Dispatch
12 quarts prior to start
48
Engine Oil in Amber
Operation limited to 45 minutes. If in Amber with T/O Thrust, do not take off.
49
Engine Ignition
Must be on for: Takeoff Landing Operation in Heavy Rain Anti-Ice Operation Severe Turbulence
50
Reverse Thrust
Prohibited in Flight
51
Alternate Mode EEC
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
APU Bleed and Electrical Load, Flight
Max Altitude 10,000'
53
APU Bleed and Electrical Load, Ground
Max Altitude 15,000'
54
APU Bleed
Max Altitude 17,000'
55
APU Electrical Load
Max Altitude 41,000'
56
APU Bleed Valve Closed When
1. Ground Air Connected and isolation valve open. 2. Engine #1 Bleed Valve Open. 3. Isolation and Engine #2 Bleed Valves Open.
57
APU
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
Speed Brakes
1. Do not deploy below 1,000' RA. 2. Do not extend past Flight Detent in flight
59
Flight Controls
Avoid rapid and large alternating control inputs. May cause structural failure at any speed.
60
Fuel Tank Temps
Maximum: 49C Minimum: -43C Jet B prohibited
61
Fuel Balance
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
Fuel Loading
Main Tanks 1 & 2 must be full if center tank contains more than 1,000 lbs.
63
Center Fuel Tank Switches
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
Center Tank Fuel Pump
Dry Running is Prohibited.