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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