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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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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