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D. Move the right stabilizer manual trim lever (or alternate electrical trim switch) on the control stand in both the airplane nose up and airplane nose down directions. Verify that the stabilizer does not move. If the stabilizer does move, an arm or control valve is failed in the energized position and dispatch is not allowed until repairs are made.
5. Remove electrical and hydraulic power.
6. If left or right stabilizer trim control module (M211, M212) is inoperative, placard the associated left or right autopilot channel - INOP.
NOTE: If the left or right stabilizer trim control module is found to be inoperative and the associated autopilot is placarded INOP, it is not necessary to perform the MAINTENANCE steps for an inoperative autopilot (DDG Item 22-10-1). The only operational consideration from 22-10- 1 is already mandated by proviso b) in 27-41-2.
OPERATIONS (O)
STAB TRIM Light may illuminate. If light illuminates, trimming using the control wheel switches will be reduced to half the normal rate. The MEL procedure confirms full trim rate is available from the alternate trim system prior to dispatch.
 
EICAS STATUS MESSAGES
None
PLACARD
Over associated indicator - STAB TRIM INDICATOR INOP
 
  B757 - 200 MINIMUM EQUIPMENT LIST

EICAS STATUS MESSAGES
None
PLACARD
Near flap handle - AUTO FLAP LOAD RELIEF INOP
OPERATIONS (O)
Maximum landing weight must be equal to or less than the values listed in the following table:

Model  Maximum Landing Weight
757-200 83,000 kg
 
 
B757 - 200 MINIMUM EQUIPMENT LIST

 

NUMBER INSTALLED
1 NUMBER REQUIRED FOR DISPATCH
REMARKS OR EXCEPTIONS
0 (M) May be inoperative open provided FSEU’s and by-pass valves are verified to operate normally.
0 (M) May be inoperative open provided FSEU’s, FSAM, and by-pass valves are verified to operate normally.
1 

 
NOTE: 757-200 airplanes prior to Line Number 981 are equipped with three Flap Slat Electronic Units (FSEUs). 757-200 airplanes beginning at Line Number 981 are equipped with two FSEUs and one Flap Slat Accessory Module (FSAMs).
EICAS STATUS MESSAGES
FLAPS ISLN VAL
PLACARD
Airplane flight log - FLAP ISLN VLV INOP OPEN
MAINTENANCE (M)
1. Verify that isolation valve (shutoff valve in the depressurization module) is open:
A. Provide electrical power (AMM 24-22-00/201).
WARNING: KEEP PERSONNEL AND EQUIPMENT CLEAR OF ALL CONTROL SURFACES TO PREVENT INJURY OR DAMAGE.
B. Pressurize left hydraulic system (AMM 29-11-00/201).
C. Verify that flaps respond to flap lever input.
2. Verify proper operation of bypass valve.
A. Place flap lever in 1 position.
B. Open and collar FLAP/SLAT SHUTOFF 1 circuit breaker on panel P11.
C. Ground pin #4 on FSEU data bus test receptacle in the cargo compartment, station 560R, for at least ten seconds. (For airplanes without this pin, apply the ground to any of the four pins in terminal block TB183-YA19 on the back of the E5-1 shelf).
　
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