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.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:757-200 MAINTENANCE MANUAL SUPPLEMENT Part II 维护手册补充(9)