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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
UPPER SHROUD THE SHUTOFF VALVE PNEUMATIC LINE FOR CLAMP JUMPER BONDING ENGINE MOUNT) (TO APU ASSEMBLY BEAM FOR THE APU UPPER SHROUD BOLT
PNEUMATIC LINE FILTER FOR THE SHUTOFF VALVE NUT BONDING JUMPER STRUCTURE) (TO THE AIRPLANE
FWD B BLEED AIR LINE BLEED AIR DUCT CHECK VALVE FOR THE FUEL SENSING FLOW CONTROL (4 LOCATIONS) WASHER INSTALLATION BONDING JUMPER C INBD
(2 LOCATIONS) WASHER
NUT
UPPER SHROUD FWD
CLAMP
BONDING JUMPER SHROUD FUEL LINE
SCREW (6 LOCATIONS) SCREW
BONDING JUMPER INSTALLATION D
Upper Shroud Installation Figure 401 (Sheet 2)
E55221
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49-12-31
ALL ú ú 01 Page 403 ú Mar 15/96
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////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
APU
COMPARTMENT
STRUCTURE
SEE E AIRPLANE
MOUNTING
AIRPLANE BRACKET
MOUNTING
BRACKET RING MOUNT
STRUT
SEE F (VERTICAL)
SEE G RING MOUNT
RING MOUNT
STRUT (AXIAL)
AIRPLANE
MOUNTING UPPER
BRACKET SHROUD
SEE I
SEE H RING MOUNT
E
STRUT (LATERAL)
APU COMPARTMENT STRUCTURE
AIRPLANE MOUNTING
RIGHT AFT MOUNT
BRACKET
F
RING MOUNT STRUT (VERTICAL)
AIRPLANERING MOUNT MOUNTING
BRACKET
RING MOUNT
STRUT
(LATERAL)
FWD UPPER SHROUD BONDING JUMPER
SEE C
RIGHT FORWARD MOUNT
G
Upper Shroud Installation Figure 401 (Sheet 3)
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ALL ú ú 02 Page 404 ú Nov 15/94
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MOUNTING AIRPLANE BRACKET APU COMPARTMENT STRUCTURE
RING MOUNT STRUT (VERTICAL)
RING MOUNT
SHROUD UPPER
FWD
LEFT FORWARD MOUNT H
MOUNTING AIRPLANE BRACKET
RING MOUNT RING MOUNT STRUT (VERTICAL) STRUT (AXIAL) RING MOUNT
SHROUD UPPER FWD
I LEFT AFT MOUNT
Figure 401 (Sheet 4) Upper Shroud Installation
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////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
S 034-006
(3)
Remove the APU power plant (AMM 49-11-00/401).
S 014-016
(4)
Open the access door, 3701, for the stabilizer trim.
S 034-043
(5)
Disconnect the pressure line:
(a) Disconnect the pressure line to the pneumatic actuator for the shutoff valve for the cooling air.
NOTE: To get to the pressure line, go through the access door
____
for the stabilizer trim.
(b)
Install a cap on the pressure line.
(c)
Install a plug on the pneumatic actuator.
S 034-008
(6) In the APU compartment, disconnect the electrical receptacles from the upper shroud:
(a)
AIRPLANES WITH THE ETC; Disconnect the receptacle for the ETC, D10140, from the fitting on the upper shroud.
(b)
Disconnect the receptacle for the APU harness, D452, from the fitting on the upper shroud.
(c)
Disconnect the receptacle for the starter motor, D4802J, from the fitting on the upper shroud.
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