PPRuNe Forums - View Single Post - Boeing advice on "aerodynamically relieving airloads" using manual stabilizer trim
Old 11th Apr 2019, 06:43
  #49 (permalink)  
Australopithecus
 
Join Date: Dec 2013
Location: Weltschmerz-By-The-Sea, Queensland, Australia
Posts: 1,367
Received 82 Likes on 38 Posts
This system description is from the 737NG FCOM.

It explains the control column (under-floor) cutout switches which have been modified in the MAX to prevent them from disabling MCAS stab trim movement. The “hidden switch” on the centre console (actually called the aisle stand) is in plain view. Its a black cover-guarded switch called the STAB TRIM OVERRIDE that will override the underfloor cutout switch. It is there to restore normal trim operation if one of those switches has failed. I don’t know if it is still fitted to the Max, but that would be moot in any event.


Stabilizer Trim​
Stabilizer trim switches on each control wheel actuate the electric trim motor ​
through the main electric stabilizer trim​ circuit when the airplane is​ flown ​
manually. With the autopilot engaged, stabilizer trim is accomplished through the ​
autopilot stabilizer trim​ circuit. The main electric and autopilot stabilizer trim ​
have two speed​ modes:​ high speed with flaps extended​ and low speed with flaps ​
retracted. If the autopilot is​ engaged, actuating either pair of stabilizer trim ​
switches automatically​ disengages the autopilot. The stabilizer​ trim​ wheels rotate ​
whenever electric stabilizer​ trim​ is​ actuated.​
The STAB TRIM MAIN​ ELECT cutout​ switch and the STAB TRIM ​
AUTOPILOT cutout switch, located on the control stand, are provided to allow ​
the autopilot or​ main​ electric trim​ inputs​ to be disconnected from the stabilizer ​
trim motor.​ ​
Control column actuated stabilizer trim cutout switches stop operation of the main ​
electric and autopilot trim when the control column movement opposes trim ​
direction. When the STAB TRIM override switch is​ positioned to​ OVERRIDE, ​
electric trim can be used regardless of control column position.​
Manual stabilizer control is accomplished through cables which allow the pilot to ​
position​ the stabilizer​ by rotating​ the stabilizer​ trim wheels. The stabilizer​ is held​ ​
in position by two​ independent​ brake systems. Manual​ rotation​ of the trim​ wheels ​
can be used to override autopilot or main​ electric trim. The effort required to ​
manually rotate the stabilizer trim wheels may be higher under certain flight ​
conditions. Grasping the stabilizer trim wheel will stop stabilizer motion
Australopithecus is offline