(b)
Use the bolts to attach the flange assembly to the turbine
frame.
1) Tighten the bolts to 85-95 pound-inches
(9.5-10.5 Newton meters).
S 417-006-C00
(22) Do these steps to install the flame arrestor:
(a)
Lightly lubricate the threads of the bolts with grease, GP460, Aeroshell 8.
(b)
Use the bolts to attach the flame arrestor to the oil inlet
cover.
1) Tighten the bolts to 110-115 pound-inches
(11-13 Newton meters).
S 417-007-C00
(23) Do these steps to attach the oil supply tube to the oil supply tube of the aft sump (Fig. 701):
(a)
Lubricate the threads of the oil supply tube for the aft sump with oil, CFMI SB 79-001.
(b)
Loosely connect the oil supply tube with the oil supply tube
for the aft sump.
S 417-008-C00
(24) Do these steps to attach the shield end clamp (Fig. 701):
(a) Install the shield end clamp between the union nut and the
turbine frame.
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(b)
Lightly lubricate the threads of the bolt with grease, GP460, Aeroshell 8.
(c)
Use the bolt and a nut to attach the shield end clamp.
1) Tighten the nut to 50-55 pound-inches (5.5-6.5 Newton meters).
G. Put the Airplane Back to Its Usual Condition
S 417-003-C00
(1)
Do this task: Install the Primary Exhaust Plug (AMM 78-11-02/401).
S 417-004-C00
(2)
Do this task: Install the Primary Exhaust Sleeve
(AMM 78-11-01/401).
S 797-027-C00
(3)
Do this task: Minimum Idle Leak Check (AMM 71-00-00/501 ,
Test No. 3).
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TURBINE FRAME - APPROVED REPAIRS
________________________________
1. General
_______
A. This procedure gives the instructions for the replacement of the oil supply tube through the No. 6 strut.
TASK 72-56-00-968-001-C00
2. Oil Supply Tube Replacement
___________________________
A. Equipment
(1) Jackscrews (856A1130P11)
B. Consumable Materials
(1)
Molykote G rapid (CP2104)
(2)
Grease (CP2101)
C. References
(1)
72-56-00/601, Turbine Frame
(2)
78-11-01/401, Turbine Exhaust Sleeve
(3)
78-11-02/401, Turbine Exhaust Plug
D. Access
(1)
Location Zones
502/602 Left Fan Cowl Panels
503/603 Right Fan Cowl Panels
504/604 Left Thrust Reversers
505/605 Right Thrust Reversers
506 Engine No. 1 - Turbine Frame
606 Engine No. 2 - Turbine Frame
(2)
Access Panels 5737L Engine No. 1 - Right Fan Cowl Panel 5738L Engine No. 1 - Left Thrust Reverser 5739L Engine No. 1 - Right Thrust Reverser 5746L Engine No. 1 - Left Fan Cowl Panel 5837R Engine No. 2 - Right Fan Cowl Panel 5838R Engine No. 2 - Left Thrust Reverser 5839R Engine No. 2 - Right Thrust Reverser 5846R Engine No. 2 - Left Fan Cowl Panel
E. Procedure (Fig. 801)
S 018-051-C00
(1) Open the left and right fan cowl panel (AMM 71-11-02/201).
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