737 MAX Flight Crew Operations Manual
Supplementary Procedures -
Air Systems
SP.2.8
MN-FLT-OH-201
Engine No. 1 BLEED air switch ........................................................ ON
ISOLATION VALVE switch ......................................................... AUTO
Landing
If additional go–around thrust is desired, configure for a “No Engine Bleed
Landing.”
When below 10,000 feet:
WING ANTI-ICE switch .............................................................OFF
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
March 1, 2021