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036. Failure to supply power per this procedure will cause the “Autostow Fault” light to illuminate on the SAC module.
b)  Hydraulic power is on (AMM 29-11-00/201).
WARNING: Keep persons and equipment away from all control surfaces when hydraulic power is supplied.  Ailerons, elevators, rudder, flaps, slats, spoilers and stabilizer are fully powered surfaces.  Injury to persons or damage to equipment can occur when hydraulic power is supplied.
c)  Verify airplane is in GROUND mode.  Landing gear not tilted, air/ground switches not slugged.
Aviation Partners Boeing 757-200 MAINTENANCE MANUAL SUPPLEMENT  Part II
2) Verify the following circuit breakers on the P11circuit breaker panel are closed:
Circuit:  C/B No. 
Aileron Position Right  J23 
Aileron Position Left  J14 
Aileron Trim  J15 
EICAS Upper Display  J3 
EICAS Lower Display  J30 
L EICAS Computer   J2 
R EICAS Computer  J29 
FSEU1 POWER  G12 
FSEU1 CONT  G13 
FSEU1 SENSOR  G14 
FSEU2 POWER  C14 
FSEU2 CONT  C15 
FSEU2 SENSOR  C16 
FSEU3 POWER  G21 
FSEU3 CONT  G22 

Circuit:  C/B No. 
FSEU3 SENSOR  G23 
RADIO ALT, LEFT  F5 
RADIO ALT, RIGHT  F26 
RADIO ALT, CENTER  F20 
AUTO SPEEDBRAKE   G11 
L FMCS CMPTR  E9 
R FMCS CMPTR  E30 
L FMCS CDU  E8 
R FMCS CDU  E29 
L ADC COMP  A10 
L AIR DATA SENSOR  A11 
L AIR DATA BARO CORRECT  A12 
R ADC COMP  F30 
R AIR DATA SENSOR  F31 
R AIR DATA BARO CORRECT  F32 

3) Verify the following circuit breakers are closed:
Circuit breaker panel  Circuit Name  C/B No. 
P6  SPDBRK AUTOSTOW  K22 
P11  AUTO SPEEDBRAKE SYSTEM  G11 

4)  Select Flap detent 1.
5)  Verify airplane is in GROUND mode.  Landing gear not tilted, air/ground switches not slugged. a) Set the Speed Brake Handle in the Down and Locked Position b) Set the Thrust Lever to the IDLE position.
6)  Input 222,000 lbs (100,697 kg) in the FMC.
NOTE:

Values in (x) represent x1000kg. Typed values below are arbitrary, but will work for all aircraft. Any summation of FUEL weight value from 0-123, with ZFW value from 100-220 to give 222 GR WT is acceptable]
a.  When the MENU page is displayed on either CDU, press LSK 1L (FMC) on that CDU. 
b.  PRESS, the INIT/REF button on CDU-1. 
c.  PRESS, LSK 6L (INDEX) on CDU-1. 
d.  PRESS, 3L (PERF) on CDU-1. 
　
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