(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
D. Procedure (Fig. 805)
S 018-055-C00
(1) Open the left and right fan cowl panel (AMM 71-11-02/201).
S 018-076-C00
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 TO OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO THE EQUIPMENT CAN OCCUR.
(2) Open the left and right thrust reverser (AMM 78-31-00/201).
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72-56-00
ALL ú ú C02 Page 811 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 038-028-C00
(3) Remove the bolt and the clamp from the oil scavenge tube. (a) The clamp is found on the LPT frame at the No. 5 and 6 strut positions.
S 038-029-C00
(4) Remove the lockwire and bolts that hold the bracket and blanking plug.
S 028-046-C00
(5) Remove the bracket.
S 428-030-C00
(6) Install the bracket as follows: (a) Apply a light layer of grease (CP2101) to the bracket bolts. (b) Make sure the blanking plug is in its correct position. (c) Put the bracket in its correct position. (d) Install the bolts. 1) Torque the bolts to 95-105 pound-inches (11.0-12.0 Newton meters). (e) Install the lockwire on the bracket bolts.
S 438-031-C00
(7) Install the clamp to the oil scavenge tube as follows (Fig. 805): (a) Apply a light layer of grease (CP2101) to the bolt. (b) Install the bolt and the clamp on the tube and bracket. 1) Torque the bolt to 55-60 pound-inches (6.0-7.0 Newton meters).
S 418-077-C00
WARNING: OBEY THE INSTRUCTIONS AMM 78-31-00/201 TO CLOSE THE THRUST
_______ REVERSER. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(8) Close the left and right thrust reverser (AMM 78-31-00/201).
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72-56-00
ALL ú ú C02 Page 812 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 048-058-C00
(9) Close the left and right fan cowl panels (AMM 71-11-02/201).
TASK 72-56-00-968-032-C00
4. Studs for the LPT Frame Strut Replacement
_________________________________________
A. General
(1)
You can use this procedure to temporarily replace one or two studs without removal of the engine from the airplane.
(2)
This repair is permitted without special inspections or restrictions for as long as the engine stays on the airplane.
(3)
When the engine is removed from the airplane, the studs must be repaired using the CFMI Shop Manual before you install the engine on an airplane again.
B. Equipment
(1)
Narrow grinding wheel
(2)
Jackscrews (856A1130)
C. Consumable Materials
(1)
D00601 Grease, graphite (CP2101) - GP460 Aeroshell 8
(2)
D00000 - Liquid Wrench - CP2162
D. References
(1)
AMM 70-20-02/201, Tightening Practices and Torque Values
(2)
AMM 71-11-02/201, Fan Cowl Panels
(3)
AMM 78-11-01/401, Turbine Exhaust Sleeve
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