S 163-030
(2)
Wipe up spilled fluid.
S 413-031
(3)
Install the access panels.
S 863-032
(4)
Supply the system B hydraulic power (Ref 27-51-00/201).
S 863-033
(5)
Move the flap control lever to the UP position to retract the flaps.
S 863-034
(6)
Remove the system B hydraulic power (Ref 27-51-00/201).
TASK 12-22-51-603-058
7. Trailing Edge Flap Track Lubrication (Fig. 302)
____________________________________
A. Special Tools and Equipment
(1)
F80167-3 - Lubrication Tool Set - TE Flap Carriage Roller
(2)
ST992B (alternative) - Grease Gun Adapter
NOTE: The Grease Gun Adapter can be used to make the
____ lubrication of the exhaust gate fittings easier.
B. Consumable Materials
(1)
D00633 Grease BMS 3-33 (Recommended)
(2)
D00013 Grease MIL-G-23827 (Alternate)
(3)
D00014 Grease MIL-G-21164
(4)
D00015 Grease - Corrosion Preventive BMS 3-24
C. References
(1) 27-51-00/201, Trailing Edge Flap System
D. Access
(1) Location Zone 307, 407 Wing Trailing Edge Outboard Flap and Spoiler 309, 409 Wing Trailing Edge Inboard Flap and Spoiler
E. Procedure
S 863-059
(1) Supply the system B hydraulic power (AMM 27-51-00/201).
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12-22-51
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ú ú ú 03.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 309Jul 12/02
A 737-300/400/500MAINTENANCE MANUAL
S 863-064
(2)
Move the flap control lever to the 40-unit position to extend the trailing edge flaps.
S 863-065
(3)
Remove the system B hydraulic power (AMM 27-51-00/201).
S 643-074
(4)
Lubricate the trailing edge flap sequence carriage track.
F. Put the Airplane Back to Its Usual Condition
S 863-067
(1)
Supply the system B hydraulic power (AMM 27-51-00/201).
S 863-068
(2)
Move the flap control lever to the UP position to retract the flaps.
(3)
Remove the system B hydraulic power (AMM 27-51-00/201).
S 863-069
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12-22-51
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ú ú ú 03.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 310Jul 12/02
A
737-300/400/500MAINTENANCE MANUAL
FLAP POWER UNIT
SEE A
ALTERNATE DRIVE MOTOR
13 RIGHT ANGLE GEARBOX MIL-H-5606
SEE B (1 LOCATION) 9
FLAP POWER UNIT
FLAP POWER UNIT GEARBOX ALTERNATE DRIVE MOTORSEE CTORQUE TUBE COUPLINGS
FLUSH
12
MIL-H-5606
BMS 3-33
11
(1 LOCATION)(2 LOCATIONS)
1
78
FWD
OIL LEVEL CHECK PORT
FLAP POWER UNIT
3 POINTS
A
Trailing Edge Flap Drive System Lubrication
Figure 301 (Sheet 1)
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12-22-51
ALL ú ú 01 Page 311 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500
MAINTENANCE MANUAL
TORQUE TUBE COUPLINGS FLUSH
BMS 3-33
(2 LOCATIONS) 78
FWD
RIGHT ANGLE GEARBOX FLUSH
BMS 3-33
(1 LOCATION) 2
ACCESS
COVER
NOTE:TO GET ACCESS TO THE RIGHT ANGLE
GEARBOX, REMOVE THE FLAP TRACK FAIRINGS 3501 AND 3601 (AMM 12-31-31/201).
3 POINTS
B
ACCESS COVER
FLAP POWER UNIT GEARBOX
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