737 MAX Flashcards

(37 cards)

1
Q

Landing Gear Extension Speed

A

270KTS

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2
Q

Landing Gear Extended Speed

A

320KTS

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3
Q

Landing Gear Retraction Speed

A

235KTS

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4
Q

Flap Speeds

A

1-5=250KTS
10=210KTS
15=200KTS
25=190KTS
30=175KTS
40=166KTS

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5
Q

Max speed for alternate flap extension

A

230KTS

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6
Q

Max operating altitude with flaps extended

A

20,000FT

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7
Q

Max Tailwind for Takeoff and Landing

A

15KTS

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8
Q

Takeoff Crosswind Limitations

A

TALPA
6=34
5=25
4=22
3=20
2=15
1=13

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9
Q

Landing Crosswind Limitations

A

TALPA
6=40
5=40
4=35
3=25
2=17
1=15

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10
Q

Maximum Usable Fuel

A

Mains= 3,869KG
Centre=12,990KG
Total= 20,728KG

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11
Q

Max fuel Temperature

A

49’C

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12
Q

Min Fuel Temperature

A

-43’C or 3 degrees above fuel freezing temp

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13
Q

Max Fuel Imbalance

A

453KG

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14
Q

Maximum Differential Pressure

A

9.1PSI

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15
Q

Autopilot Limits on takeoff and landing

A

400AGL on Takeoff
50AGL on Landing

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16
Q

APU limitations

A

Electrical = 41,000FT
Bleed= 17,000FT
Bleed+Electrical= 10,000FT

17
Q

Severe Turbulence Penetration Speed

18
Q

Can aileron trim be used with autopilot engaged?

19
Q

Max Windspeed During Autoland Operations

A

Headwind = 24KTS
Crosswind = 20KTS
Tailwind = 15KTS

20
Q

Maximum Takeoff or Landing Altitude

21
Q

Altitude Difference for RVSM

A

200FT in flight
50FT between Captain and FO 1-5000FT
60FT 5001-10000FT
75FT between either pilot and field elevation

22
Q

At what point is a go around prohibited?

A

After thrust reverser deployment on landing

23
Q

How long do you have to wait after APU start before selecting it for a bleed source?

24
Q

Minimum Engine Oil for Dispatch

25
Minimum Brake Pressure
2800PSI
26
Minimum Hydraulic Fluid for Dispatch
76 Percent RF will appear
27
Minimum pavement width for 180 degree turn
80FT
28
What altitude will the CABIN ALT warning light come on?
10,000FT, masks will drop at 14,000FT
29
T/O config warning will sound under what circumstances?
Trailing edge flaps are not between 1-25 Trailing edge flaps are asymmetric or uncommanded motion Leading edge not configured or have uncommanded motion Speed brake is not down Spoiler control valve is open and pressurizing the spoiler interlock valve Park brake is set Trim is not in takeoff range
30
An approach is considered stable when what criteria are met?
Aircraft in final configuration Appropriate thrust setting Airspeed on target +10 to -5 Sink rate no greater than 1000FPM unless briefed Established on path 1 dot vertically .5 dot laterally In a position to land within the touchdown zone
31
RVR requirements for CAT 2/3 respectively
CAT 2 = RVR A 1200 CAT 3 = RVR A,B,C 600
32
PIC requirements for CAT 2/3
300 Turbojet, 100 B737
33
What systems are powered by the A hydraulic system?
Ailerons Rudder Elevator and Elevator Feel Flight Spoilers 2,4,9,11 Ground Spoilers 1,6,7,12 No.1 Thrust Reverser Autopilot A Normal Nose Wheel Steering Landing Gear Landing Gear Transfer Valve PTU
34
What systems are powered by the B hydraulic system?
Ailerons Rudder Elevator and Elevator Feel Flight Spoilers 3,5,8,10 LE Flaps and Slats Trailing Edge Flaps Normal Brakes No.2 Thrust Reverser Autopilot B Alternate Nose Wheel Steering Landing Gear Transfer Unit Yaw Damper
35
What systems does the standby hydraulic system power?
Thrust Reversers Rudder Leading Edge Flaps and Slats (extend only) Standby Yaw Damper
36
Minimum voltage for APU start
23 Volts
37
Maximum holding speeds
6000 and below = 200KIAS Above 6000 to 14000 = 230KIAS Above 14000 = 265KIAS