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Lynx 737 > 737 MAX > Flashcards

737 MAX Flashcards

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

A

280KIAS/.76M

18
Q

Can aileron trim be used with autopilot engaged?

A

No

19
Q

Max Windspeed During Autoland Operations

A

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

20
Q

Maximum Takeoff or Landing Altitude

A

8,400FT

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?

A

2 minutes

24
Q

Minimum Engine Oil for Dispatch

A

66 Percent

25
Q

Minimum Brake Pressure

A

2800PSI

26
Q

Minimum Hydraulic Fluid for Dispatch

A

76 Percent RF will appear

27
Q

Minimum pavement width for 180 degree turn

A

80FT

28
Q

What altitude will the CABIN ALT warning light come on?

A

10,000FT, masks will drop at 14,000FT

29
Q

T/O config warning will sound under what circumstances?

A

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
Q

An approach is considered stable when what criteria are met?

A

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
Q

RVR requirements for CAT 2/3 respectively

A

CAT 2 = RVR A 1200
CAT 3 = RVR A,B,C 600

32
Q

PIC requirements for CAT 2/3

A

300 Turbojet, 100 B737

33
Q

What systems are powered by the A hydraulic system?

A

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
Q

What systems are powered by the B hydraulic system?

A

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
Q

What systems does the standby hydraulic system power?

A

Thrust Reversers
Rudder
Leading Edge Flaps and Slats (extend only)
Standby Yaw Damper

36
Q

Minimum voltage for APU start

A

23 Volts

37
Q

Maximum holding speeds

A

6000 and below = 200KIAS
Above 6000 to 14000 = 230KIAS
Above 14000 = 265KIAS

Lynx 737 (1 decks)

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