(a)
C54001-37 Sling Equipment, Strut Removal/Installation
(b)
C54003-1 Socket, Midspar Fuse Pin Removal/Installation
(c)
Crane, approved to lift 5,000 pounds
(d)
Dynamometer, 0-5,000 pound capacity, | 2% accuracy
(2)
Lift Equipment (Engine supported)
(a)
C54004-1 Sling Equipment, Engine Fan Case
(b)
C54005-1 Pin/Bolt Removal and Installation Kit (Brass Slugs)
(c)
Crane, approved to lift 12,000 pounds.
1) Pull Pac Cylinder BRP-306, P-80 Pump, HC-941 Hose Assembly (Alternative) - ENERPAC, Division of Applied Power, Inc., Butler, Wisconsin
(d)
Dynamometer, 0-6,000 pound capacity, | 2% accuracy
1) Two dynamometers are necessary if the crane has an adjustable Load Limiter or if you use a precision Load positioner.
2) A third dynamometer of 12,000 pound capacity is necessary if the crane does not have an adjustable Load Limiter.
(e) Chain Hoist, 6000 pound capacity (2 are necessary).
(3) Tag Lines - used for control of the engine/strut sling.
B. Consumable Materials
(1)
D00013 Grease - MIL-G-23827 (Alternative)
(2)
D00015 Grease - Corrosion Preventative, BMS 3-24 (Recommended)
C. References
(1)
AMM 27-81-00/201, Leading Edge Flap and Slat Control System
(2)
AMM 29-09-00/201, Hydraulic Resevoir Pressurization System
(3)
AMM 54-32-01/401, Forward Fairing
(4)
AMM 54-32-02/401, Aft Fairings
(5)
AMM 71-00-02/401, Power Plant
(6)
AMM 71-11-02/401, Fan Cowl Panels
(7)
AMM 78-31-00/201, Thrust Reverser System
D. Access
(1) Location Zone
500 Left Nacelle
600 Right Nacelle
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
E. Prepare to remove the pin/bolt (engine removed).
S 864-062-B00
(1) Ground the aircraft to an approved lug.
S 044-001-B00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
S 044-063-B00
WARNING: OBEY THE PRECAUTIONS IN THE PROCEDURE WHEN YOU DO THE
_______ DEACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS. IF YOU DO NOT OBEY THE PRECAUTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(3)
Do the deactivation procedure for the leading edge slats
(AMM 27-81-00/201).
S 014-003-B00
(4)
Remove the access doors, panels and fairings.
(a)
Remove the forward panel of the aft fairing (AMM 54-32-02/401), to get access to the diagonal brace pins.
(b)
Remove the wing junction fairing (AMM 54-32-02/401), if it is necessary to get access to the midspar fuse bolts.
(c)
Remove the forward leading edge fairing (AMM 54-32-01/401), if it is necessary to get access to the upper link pins.
(d)
Remove the forward fairing (AMM 54-32-01/401).
(e)
Remove the engine fan-cowl panels (AMM 71-11-02/401).
S 044-026-B00
WARNING: KEEP ELECTRICAL POWER OFF DURING THE DISCONNECTION OR
_______ CONNECTION OF THE FUEL, HYDRAULIC, AND ELECTRICAL LINES. THE ACCIDENTAL APPLICATION OF PRESSURIZED FLUIDS, ENERGIZING OF ELECTRICAL CIRCUITS, OR FIRE COULD CAUSE INJURY TO PERSONS.
(5) Deactivate the electrical, fuel, and hydraulic systems.
(a) Make sure the external electrical power is disconnected, and that the airplane is grounded.
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