S 044-003
(2)
Open these circuit breakers and install DO-NOT-CLOSE tags:
(a) P18 Load Control Panel
1) FLIGHT RECORDER AC
2) FLIGHT RECORDER POSITION SENSORS
S 014-004
(3) Remove the forward access panel, 1103.
E. Transmitter Rod Removal
S 834-005
(1) Set the rudder pedals to the neutral position.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
AIRPLANES POST-SB 31-3112; ú 31-24-43
AIRPLANES WITH RUDDER PEDAL FORCE ú
TRANSMITTER ROD INSTALLED ú 01 Page 401 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
FORWARD QUADRANT
FORWARD RIG PIN HOLE
RIG PIN
FWD
(R-3 ON THE CAPTAIN'S QUADRANT)
(R-4 ON THE FIRST OFFICER'S QUADRANT)
A
Rudder Force Transmitter Rod
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
AIRPLANES POST-SB 31-3112; ú 31-24-43
AIRPLANES WITH RUDDER PEDAL FORCE ú
TRANSMITTER ROD INSTALLED ú 01 Page 402 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
K24585
A 737-300/400/500MAINTENANCE MANUAL
FRONTREAR SPAR SPAR
SEE A
ACCESS PANEL, 9525
RUDDER AFT QUADRANT STA 1007.65 ACCESS PANEL, 9530 ACCESS PANEL, 9509
LEFT SIDE VIEW
SEE CSEE B TRANSMITTER ROD RUDDER FORCE
SEE D
FWD R-5 HOLE RIG PIN
CONNECTOR ELECTRICAL A UNIT CENTERING FEEL AND
Rudder Force Transmitter Rod Installation Figure 402 (Sheet 1)
K24599
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
AIRPLANES POST-SB 31-3112; ú 31-24-43
AIRPLANES WITH RUDDER PEDAL FORCE ú
TRANSMITTER ROD INSTALLED ú 01 Page 403 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
WASHER
WASHER
BOLT
RUDDER FORCE TRANSMITTER ROD
Rudder Force Transmitter Rod Installation
Figure 402 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
AIRPLANES POST-SB 31-3112; ú 31-24-43
AIRPLANES WITH RUDDER PEDAL FORCE ú
TRANSMITTER ROD INSTALLED ú 01 Page 404 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
K24604
A 737-300/400/500MAINTENANCE MANUAL
Rudder Force Transmitter Rod Installation
Figure 402 (Sheet 3)
K24607
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
AIRPLANES POST-SB 31-3112; ú 31-24-43
AIRPLANES WITH RUDDER PEDAL FORCE ú
TRANSMITTER ROD INSTALLED ú 01 Page 405 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 834-006
(2) Install these rig pins (Fig. 401):
(a)
R-3 in the captain's forward quadrant.
(b)
R-4 in the first officer's forward quadrant.
S 024-007
(3) Remove the transmitter rod:
(a)
Remove access panel 9509 and open access door 9513.
(b)
Remove access panels 9509 and 9513.
(c)
Disconnect the electrical connector from the transmitter rod.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 仪表 INSTRUMENTS(106)
