737 MAX Flashcards
Landing Gear Extension Speed
270KTS
Landing Gear Extended Speed
320KTS
Landing Gear Retraction Speed
235KTS
Flap Speeds
1-5=250KTS
10=210KTS
15=200KTS
25=190KTS
30=175KTS
40=166KTS
Max speed for alternate flap extension
230KTS
Max operating altitude with flaps extended
20,000FT
Max Tailwind for Takeoff and Landing
15KTS
Takeoff Crosswind Limitations
TALPA
6=34
5=25
4=22
3=20
2=15
1=13
Landing Crosswind Limitations
TALPA
6=40
5=40
4=35
3=25
2=17
1=15
Maximum Usable Fuel
Mains= 3,869KG
Centre=12,990KG
Total= 20,728KG
Max fuel Temperature
49’C
Min Fuel Temperature
-43’C or 3 degrees above fuel freezing temp
Max Fuel Imbalance
453KG
Maximum Differential Pressure
9.1PSI
Autopilot Limits on takeoff and landing
400AGL on Takeoff
50AGL on Landing
APU limitations
Electrical = 41,000FT
Bleed= 17,000FT
Bleed+Electrical= 10,000FT
Severe Turbulence Penetration Speed
280KIAS/.76M
Can aileron trim be used with autopilot engaged?
No
Max Windspeed During Autoland Operations
Headwind = 24KTS
Crosswind = 20KTS
Tailwind = 15KTS
Maximum Takeoff or Landing Altitude
8,400FT
Altitude Difference for RVSM
200FT in flight
50FT between Captain and FO 1-5000FT
60FT 5001-10000FT
75FT between either pilot and field elevation
At what point is a go around prohibited?
After thrust reverser deployment on landing
How long do you have to wait after APU start before selecting it for a bleed source?
2 minutes
Minimum Engine Oil for Dispatch
66 Percent
Minimum Brake Pressure
2800PSI
Minimum Hydraulic Fluid for Dispatch
76 Percent RF will appear
Minimum pavement width for 180 degree turn
80FT
What altitude will the CABIN ALT warning light come on?
10,000FT, masks will drop at 14,000FT
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
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
RVR requirements for CAT 2/3 respectively
CAT 2 = RVR A 1200
CAT 3 = RVR A,B,C 600
PIC requirements for CAT 2/3
300 Turbojet, 100 B737
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
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
What systems does the standby hydraulic system power?
Thrust Reversers
Rudder
Leading Edge Flaps and Slats (extend only)
Standby Yaw Damper
Minimum voltage for APU start
23 Volts
Maximum holding speeds
6000 and below = 200KIAS
Above 6000 to 14000 = 230KIAS
Above 14000 = 265KIAS
