TASK 24-11-21-004-001
2. Generator Drive Oil Cooler Removal (Fig. 401)
__________________________________
A. References
(1)
AMM 78-31-00/201, Thrust Reverser System
B.
Access
(1)
Location Zone
504 Engine No. 1, LH
505 Engine No. 1, RH
604 Engine No. 2, LH
605 Engine No. 2, RH
(2)
Access Panel
5738L Thrust Reverser Cowl Assembly
5738R Thrust Reverser Cowl Assembly
5739L Thrust Reverser Cowl Assembly
5739R Thrust Reverser Cowl Assembly
C.
Procedure
S 014-002
(1)
Open the right fan duct cowl and thrust reverser half (AMM 78-31-00/201).
S 874-021
(2)
AIRPLANES WITH A VSCF GENERATOR/CONVERTER; Release the pressure in the VSCF Generator/Converter oil system.
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A
737-300/400/500
MAINTENANCE MANUAL
OIL TANK (REF)
GENERATOR DRIVE FWD
OIL COOLER AND TUBING
SEE A
OIL COOLER
SEE B
FAN
CASE
TUBING SEE C
VIEW TOWARDS AFT
A
Generator Drive Oil Cooler Installation Figure 401 (Sheet 1)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
B
Generator Drive Oil Cooler Installation
Figure 401 (Sheet 2)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
OIL TANK
(REF)
TEE-FITTING
OIL COOLER
INLET HOSE
OIL FILTER
(REF)
OIL COOLER
OUTLET LINE
FWD
C
Generator Drive Oil Cooler Installation
Figure 401 (Sheet 3)
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A
737-300/400/500MAINTENANCE MANUAL
WARNING:_______REMOVE THE OVERFILL DRAIN FITTING SLOWLY. HOT GAS OR OIL CAN COME OUT WHEN THE ENGINE IS HOT. HOT GAS OR OIL CAN BURN YOU.
(a)
Remove the overfill drain fitting.
(b)
Remove the pressure-fill valve.
S 874-020
(3) AIRPLANES WITH A CONSTANT SPEED DRIVE;
Release the pressure in the CSD oil system.
(a) Push the vent valve cap on the top of the CSD to remove the internal pressure.
S 034-003
(4) Remove the union from the oil-in port:
(a)
Remove the hose from the oil-in port on the oil cooler.
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