(b)
Install the forward fairing (AMM 54-32-01/401).
(c)
Install the forward leading edge fairing (AMM 54-32-01/401), if removed to get access to the upper link.
(d)
Install the wing junction fairings (AMM 54-32-02/401), if removed to get access to the midspar fuse bolts.
(e)
Install the forward panels of the aft fairing (AMM 54-32-02/401), if removed to get access to the diagonal brace pins.
(f)
Install the strut access panels (AMM 54-31-01/401), if removed.
S 444-059-B00
WARNING: MAKE SURE THAT ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE
_______ LEADING EDGE SLATS BEFORE YOU REACTIVATE THE LEADING EDGE SLAT SYSTEM. IF YOU DO NOT OBEY THE PRECAUTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(7)
Do the activation procedure for the leading edge slats
(AMM 27-81-00/201).
S 444-063-B00
(8)
Do the activation procedure for the thrust reverser
(AMM 78-31-00/201).
H. Put the Airplane Back in its Usual Condition (Engine Supported).
S 094-050-B00
CAUTION: DO NOT REMOVE THE ENGINE SLING UNTIL THE WORKSTANDS ARE CLEAR.
_______ IF YOU DO NOT MOVE THE WORK STANDS, DAMAGE TO THE ENGINE, STRUT, WING STRUCTURE OR STANDS CAN OCCUR.
(1) Remove the engine sling:
(a)
Make sure the workstands are clear of the airplane.
(b)
Slowly remove the load from the sling.
(c)
Remove the sling from the engine, and return the sling to storage.
S 224-063-B00
(2)
Do a check that the clearance between the nacelle strut and the wing attach fitting is as shown (Figure 402, Detail B).
S 444-061-B00
(3)
Reactivate the electrical, fuel, and hydraulic systems:
(a)
Make sure the fuel and hydraulic fluid lines to the engine are filled.
(b)
Pressurize the hydraulic system (AMM 29-09-00/201).
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54-10-01
ALL ú ú B03 Page 424 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(c)
Open the hydraulic EDP supply shutoff-valve and connect the electrical plug to the valve.
(d)
Open the engine fuel shutoff-valve, and connect the electrical plug to the valve.
(e)
Remove the DO-NOT-OPERATE identifier from FUEL CONTROL toggle switches, found on the engine start module.
(f)
Remove the electrical ground wire.
S 214-064-B00
CAUTION: MAKE SURE THE INSIDE OF THE STRUT IS FREE OF ALL TOOLS AND
_______ UNWANTED OBJECTS. IF YOU DO NOT REMOVE ALL TOOLS AND UNWANTED OBJECTS, BLOCKAGE OF THE DRAIN TUBES CAN OCCUR.
(4)
Make sure that all tools and loose material are removed, and the strut cavities are free of unwanted material before you install the access doors.
S 414-062-B00
(5)
Install all access doors and panels.
(a)
Install the engine fan cowl panels (AMM 71-11-02/401).
(b)
Install the forward fairing (AMM 54-32-01/401).
(c)
Install the forward leading edge fairing (AMM 54-32-01/401), if removed to get access to the upper link.
(d)
Install the wing junction fairings (AMM 54-32-02/401), if removed to get access to the midspar fuse bolts.
(e)
Install the forward panels of the aft fairing (AMM 54-32-02/401), if removed to get access to the diagonal brace pins.
(f)
Install the strut access panels (AMM 54-31-01/401), if removed.
S 444-102-B00
WARNING: MAKE SURE THAT ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE
_______ LEADING EDGE SLATS BEFORE YOU REACTIVATE THE LEADING EDGE SLAT SYSTEM. IF YOU DO NOT OBEY THE PRECAUTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(6)
Do the activation procedure for the leading edge slats (AMM 27-81-00/201).
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