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Reference Description
SPL-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
B01004 Solvent - Final Cleaning Of Metal Prior To Painting
(AMM 20-30-84/201) - Series 84
G01912 Lockwire - Monel (0.032 In. Dia.) NASM20995N~
C32
(QQ-N-281)
D. 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
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
564 Left Wing - Spoiler No. 3
565 Left Wing - Spoiler No. 2
664 Right Wing - Spoiler No. 10
665 Right Wing - Spoiler No. 11
E. Prepare for the Adjustment
SUBTASK 27-61-00-480-006
(1) Make sure that you can easily install these rig pins for the rig pin kit, SPL-1585:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 521
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) A/S-1 and A/S-1A in the aileron transfer mechanism.
(b) A/S-3 in the aileron pogo.
(c) A/S-4 in the aileron bus drums.
(d) A/S-14 in the spoiler mixer (Figure 502).
(e) A/S-15 in the aileron trim actuator.
SUBTASK 27-61-00-080-005
(2) Remove all rig pins.
SUBTASK 27-61-00-860-019
(3) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-61-00-860-020
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(4) Do this task: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
SUBTASK 27-61-00-866-005
(5) Extend the flaps (Extend the Trailing Edge Flaps, TASK 27-51-00-860-803).
SUBTASK 27-61-00-860-021
(6) Move the speed brake lever to the full up position to fully extend the spoilers.
SUBTASK 27-61-00-820-007
(7) Turn adjustment screw [51] clockwise 2 full turns, or until the stop is reached.
(a) Tighten the check nut [52].
SUBTASK 27-61-00-860-022
(8) Do this task: Retract the Trailing Edge Flaps, TASK 27-51-00-860-804.
SUBTASK 27-61-00-860-023
(9) Slowly move the speed brake lever to the DOWN position.
F. Flight Spoiler Adjustment
SUBTASK 27-61-00-860-024
(1) Measure the clearance between the trailing edge of the spoiler panels and the flaps near the
centerline of the spoiler actuators.
SUBTASK 27-61-00-860-075
(2) Make sure the clearance between the spoilers No. 5 and 8 and the flaps is 0.085 +0.000/-0.060
inch (2.16 +0.00/-1.52 millimeters).
NOTE: Measure the clearance aft of the spoiler actuator rod end. A larger or smaller
clearance is permitted at other locations along the spoiler.
SUBTASK 27-61-00-860-076
(3) Make sure the clearance between the spoilers No. 3, 4, 9 and 10 and the flaps is 0.250 +0.050/-
0.010 inch (6.35 +1.27/-0.25 millimeters).
NOTE: Measure the clearance aft of the spoiler actuator rod end. A larger or smaller
clearance is permitted at other locations along the spoiler.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 522
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-61-00-860-025
(4) Make sure the clearance between the spoilers No. 2 and 11 and the flaps is 0.300 +0.050/-0.010
inch (7.62 +1.27/-0.25 millimeters).
NOTE: Measure the clearance aft of the spoiler actuator rod end. A larger or smaller
clearance is permitted at other locations along the spoiler.
SUBTASK 27-61-00-860-028
(5) If the clearances between the spoiler panels and the flaps are not in the limits, adjust the
clearance:
(a) Make a record of the clearance.
(b) Lift the spoiler and extend the flaps to get access to the spoiler actuator:
1) Do this task: Extend the Trailing Edge Flaps, TASK 27-51-00-860-803.
2) Move the speed brake lever to the UP position to lift the spoilers.
3) Do this task: Remove Pressure from the Speed Brake Hydraulic Systems A and B,
TASK 27-62-00-800-802.
(c) Loosen the check nut [55] on the actuator rod end [56].
(d) Turn the piston rod on the spoiler actuator to adjust the clearance between the spoiler and
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(7)
