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737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
Page 604
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E. Prepare for the Inspection
SUBTASK 27-51-00-480-013
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEAR.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEAR CAN RETRACT AND CAUSE
INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) If the downlock pins are not installed in the nose and main landing gear, do this task: Landing
Gear Downlock Pins Installation, TASK 32-00-01-480-801.
SUBTASK 27-51-00-010-012
(2) Extend the trailing edge flaps to the 40-unit position. To extend the flaps, do this task: Extend the
Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-51-00-040-007
(3) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
F. Outboard Flap Inspection
(Figure 602)
SUBTASK 27-51-00-010-013
(1) At the flap supports, remove the leading edge skin panel [2] from the main flap [1] forward of the
carriage:
(a) Remove the bolts [3] that attach the leading edge skin panel [2].
(b) Remove the leading edge skin panel [2] from the main flap [1].
Open these access panels:
Number Name/Location
567BT Flap, Forward Carriage Bearing And Fitting
567ET Flap, Forward Carriage Bearing And Fitting
667BT Flap, Forward Carriage Bearing And Fitting
667ET Flap, Forward Carriage Bearing And Fitting
SUBTASK 27-51-00-210-004
(2) Do a detailed visual inspection of these items at the flap supports:
NOTE: These are flap supports No. 1, 2, 7 and 8.
(a) Aft flap drive rod, push rod and bellcrank
(b) Carriage rollers
(c) Aft link and fittings
(d) Forward carriage bearing and fitting.
SUBTASK 27-51-00-210-005
(3) Do a detailed visual inspection of the deflection control rollers between the inboard and
outboard flaps and at the outboard end of the outboard flap.
SUBTASK 27-51-00-210-006
(4) At the outboard aft flap, do a detailed visual inspection of these items:
(a) Aft flap track attachments.
NOTE: There are four aft flap tracks on the outboard flap.
(b) Inboard and outboard programming rollers.
(c) Inboard and outboard aft flap pushrods.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
Page 605
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(d) Rubstrips common to the aft flap support tracks, and common to the inboard and outboard
edge program tracks.
(e) Inboard and outboard aft flap track rollers.
SUBTASK 27-51-00-410-012
(5) Install the leading edge skin panels [2] on the main flap [1] forward of the carriage:
(a) Close these access panels:
Number Name/Location
567BT Flap, Forward Carriage Bearing And Fitting
567ET Flap, Forward Carriage Bearing And Fitting
667BT Flap, Forward Carriage Bearing And Fitting
667ET Flap, Forward Carriage Bearing And Fitting
Put the leading edge skin panel [2] in its location on the leading edge of the main flap [1].
(b) Apply compound, C00528 to the holes for the bolts [3].
(c) Install the bolts [3] to attach the leading edge skin panel [2].
(d) Apply sealant, A00247 to fill all of the clearances around the skin panel [2] that are more
than 0.05 inch (1.27 millimeters).
G. Inboard Flap Inspection
(Figure 603)
SUBTASK 27-51-00-210-007
(1) At the outboard flap support for the inboard flap, do a detailed visual inspection of these items:
NOTE: These are flap supports No. 3 and 6.
(a) Aft flap drive rod and crankshaft
(b) Carriage rollers
SUBTASK 27-51-00-210-008
(2) At the inboard flap support for the inboard flap, do a detailed visual inspection of these items:
NOTE: These are flap supports No. 4 and 5.
(a) Carriage rollers
SUBTASK 27-51-00-210-009
(3) At the inboard aft flap, do a detailed visual inspection of these items:
(a) Aft flap track attachments.
NOTE: There are two aft flap tracks on the inboard flap.
(b) Inboard and outboard programming rollers.
(c) Inboard and outboard aft flap pushrods.
(d) Rubstrips common to the aft flap support tracks, and common to the inboard and outboard
edge program tracks.
(e) Inboard and outboard aft flap track rollers.
SUBTASK 27-51-00-440-006
(4) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-00
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