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Flap System Operation With Alternate Control, TASK 27-51-00-860-802.
(c) To manually extend the flaps, do this task: Trailing Edge Flap System Manual Operation,
TASK 27-51-00-980-801.
------------------------- END OF TASK ---------------------------
TASK 27-51-00-860-804
8. Retract the Trailing Edge Flaps
A. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
B. Procedure
SUBTASK 27-51-00-860-017
(1) Do one of these tasks to retract the trailing edge flaps:
(a) To retract the flaps with hydraulic power, do this task: Trailing Edge Flap System
Operation With Primary Control, TASK 27-51-00-860-801.
(b) To retract the flaps with electrical power in alternate mode, do this task: Trailing Edge Flap
System Operation With Alternate Control, TASK 27-51-00-860-802.
(c) To manually retract the flaps, do this task: Trailing Edge Flap System Manual Operation,
TASK 27-51-00-980-801.
------------------------- END OF TASK ---------------------------
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TASK 27-51-00-860-805
9. Trailing Edge Flap System Operation With Leading Edge Flaps and Slats Disabled
A. General
(1) This task gives instructions to operate the trailing edge flap system with the leading edge flaps
and slats retracted and disabled.
(2) You can operate the trailing edge flaps with primary or alternate control or manually after you do
the Disable the Leading Edge Slats part of this task.
B. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
29-21-00-000-802 Standby Hydraulic System Power Removal (P/B 201)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
SWPM 20-60-03 Standard Wiring Practices Manual
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1675 Assembly - Lock, Flight Controls
(Part #: F80049-18, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80049-12, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
D. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D00467 Fluid - Landing Gear Shock Strut BMS3-32, Type
II
G50171 Compound - Corrosion Inhibiting Compound,
Interior Application - D5026NS or ZC-026
E. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
4 Cover 27-51-55-02-110 GUN 001-028, 101-121,
155-157, 201-999
5 Packing 27-51-55-02-115 GUN 001-028, 101-121,
155-157, 201-999
F. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
118 Electrical and Electronics Compartment - Right
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(Continued)
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
G. Access Panels
Number Name/Location
117A Electronic Equipment Access Door
H. Disable the Leading Edge Slats
SUBTASK 27-51-00-860-057
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-51-00-860-058
(2) Make sure the trailing edge flaps and the leading edge flaps and slats are in the retracted
position. If they are not in the retracted position, do this task: Retract the Trailing Edge Flaps,
TASK 27-51-00-860-804.
SUBTASK 27-51-00-860-059
(3) Remove the standby hydraulic system power, do this task: Standby Hydraulic System Power
　
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