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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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////////////////////////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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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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