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737 MAX Flight Crew Operations Manual
Supplementary Procedures -
Air Systems
MN-FLT-OH-201 SP.2.7
#No Engine Bleed Takeoff and Landing
When making a no engine bleed takeoff or landing with the APU
operating.
Takeoff
Note:
If anti–ice is required for taxi, configure for a “No Engine Bleed
Takeoff” just prior to takeoff.
Note:
If anti–ice is not required for taxi, configure for a “No Engine
Bleed Takeoff” just after engine start.
Right PACK switch........................................................................AUTO
ISOLATION VALVE switch ....................................................... CLOSE
Left PACK switch ..........................................................................AUTO
Engine No. 1 BLEED air switch ...................................................... OFF
APU BLEED air switch......................................................................ON
Engine No. 2 BLEED air switch ...................................................... OFF
-800 and MAX fleet
Trim Air Switch. ................................................................................ON
WING ANTI-ICE switch .................................................................. OFF
The WING ANTI-ICE switch must remain OFF until the engine BLEED
air switches are repositioned to ON and the ISOLATION VALVE switch
is repositioned to AUTO.
After Takeoff
Note: If engine failure occurs, do not position engine BLEED air
switches ON until reaching 1500 feet or until obstacle clearance
height has been attained.
After first flap retraction:
Engine No. 2 BLEED air switch ........................................................ON
APU BLEED air switch.................................................................... OFF
When CABIN rate of CLIMB indicator stabilizes and workload permits at
pilot’s discretion:
March 1, 2021