747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(7)

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 NOTE:____ Do not disconnect the electrical connector DN308.
 (c) (d) (e)  Turn the adjustment screw on the bottom of the rudder trim indicator until the indicator is at the zero position.Install the rudder trim indicator with the two fasteners.Set the FLT CONTROL HYD POWER TAIL switches on the P461, Pilots' Overhead Maintenance Panel to NORM.
 (6)  S 864-012Remove the electrical power (AMM 24-22-00/201).
 (7)  S 864-015Remove the hydraulic power (AMM 29-11-00/201).

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 27-28-03
 ALL  ú ú 01 Page 404 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
ELEVATORS
COMPONENT  SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE 
ACTUATOR - ELEVATOR FEEL  2  1  315Z, AFT STAB COMPARTMENT  27-31-17 
PACKAGE ACTUATOR - INBOARD ELEVATOR POWER CONTROL  2  2  344HBR, R INBOARD ELEV 334HBL, L INBOARD ELEV  27-31-07 
STICK SHAKER R, C10300 ELEV/RUD VLV SYS 4, C657 ELEV/RUD VLV SYS 2, C652 ELEV/RUD VLV SYS 1, C648 CIRCUIT BREAKERS -RUD/ELEV IND, C383 YM5A001 CIRCUIT BREAKERS -CARD - (REF 27-20-00, FIG. 101) ACTUATOR - OUTBOARD ELEVATOR POWER CONTROL PACKAGE RUD/ELEV SENSOR, C10061 STICK SHAKER L, C10299 ELEV/RUD VLV SYS 3, C654 RUD/ELEV SURFACE POSITION DIGITIZER (SPD), 2  2  6J25 6J24 180E22 180H23 180E7 180H8 117AL, MAIN EQUIP CTR, P180 7D19 7D5FLT COMPT, P6,P7 336DBL,347DAR, ELEV LEADING EDGE 334LBL,344LBR, STAB TRAILING EDGE * * * * * * * * 27-31-08 
COMPUTER - ELEVATOR FEEL, B169 2  1  312A, STAB JACKSCREW  27-31-14 
COMPUTER - L STALL WARNING MANAGEMENT, YMXOA05  4  1  117AL, MAIN EQUIP CTR, MAWEA  27-32-00 
YAXOA10COMPUTER - R STALL WARNING MANAGEMENT,  4  1  117AL, MAIN EQUIP CTR, MAWEA  27-32-00 
COLUMN - CONTROL  3  2  FLT COMPT  27-31-04 
ELEVATOR - INBOARD  1  2  REAR SPAR OF HORIZONTAL STAB  27-31-01 
FLIGHT CONTROLS HYDRAULIC POWER, M191 MODULE - (REF 27-10-00, FIG. 101)ELEVATOR - OUTBOARD  1  2  REAR SPAR OF HORIZONTAL STAB  27-31-02 
QUADRANT - ELEVATOR AFT  2  1  315A, AFT STAB COMPARTMENT  27-31-06 
QUADRANT - ELEVATOR FORWARD  3  2  CABIN, NOSE TO FIRST DOOR  27-31-05 
REGULATOR - ELEVATOR CONTROL CABLE TENSION  3  1  PASS CABIN, NOSE TO FIRST DOOR, LH  27-31-00 
SHAKER - CAPTAIN'S CONTROL COLUMN, M7983  3  1  CONTROL CABIN, LH  27-32-02 
M7984 SHAKER - FIRST OFFICER'S CONTROL COLUMN,  3  1  CONTROL CABIN, RH  27-32-02 
TRANSMITTER - L INBOARD ELEV POSITION, T1672 5  1  334GBL, HORIZONTAL STABILIZER  27-38-01 
TRANSMITTER - R INBOARD ELEV POSITION, T1673  5  1  334GBR, HORIZONTAL STABILIZER  27-38-01 
TRANSMITTER - L OUTBOARD ELEV POSITION, T438  5  1  334KBL, HORIZONTAL STABILIZER  27-38-01 
R EFIS/EICAS INTERFACE, M7351 L EFIS/EICAS INTERFACE, M7353 C EFIS/EICAS INTERFACE, M7352 TRANSMITTER - R OUTBOARD ELEV POSITION, T437 UNIT - (REF 31-61-00, FIG. 101)  5  1  334KBR, HORIZONTAL STABILIZER  27-38-01 
SHUTOFF VALVE - (REF 27-20-00, FIG. 101) RUDDER & ELEVATOR HYDRAULIC SYSTEM 4 SHUTOFF RUDDER & ELEVATOR HYDRAULIC SYSTEM 3 SHUTOFF SHUTOFF RUDDER & ELEVATOR HYDRAULIC SYSTEM 2 RUDDER & ELEVATOR HYDRAULIC SYSTEM 1UNIT - ELEVATOR FEEL  2  1  315A, AFT STABILIZER COMPARTMENT  27-31-17

 * SEE WDM EQUIPMENT LIST
Elevators - Component IndexFigure 101
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 27-30-00
 ALL  ú
 ú  01  Page 101
 ú  Oct 10/89 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
INBOARD ELEVATOR
SEEA OUTBOARD ELEVATOR SEE B
INBOARD ELEVATOR (LH SHOWN; RH OPPOSITE)
A
OUTBOARD ELEVATOR (LH SHOWN; RH OPPOSITE)
B
Elevators - Component Location Figure 102 (Sheet 1)
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