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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 715-007
(2)
Move the speed brake lever from the DOWN position to the UP position.
(a)
Make sure the speed brakes move to the up position.
S 715-008
(3)
Move the speed brake lever from the UP position to the DOWN position.
(a)
Make sure the speed brakes move to the retracted position.
S 865-009
(4) Remove the systems A and B hydraulic power (AMM 27-62-00/201).
TASK 27-62-00-825-002
3. Speed Brake Control System Adjustment
_____________________________________
A. General
(1)
Refer to Fig. 501 for the locations of the rig pins and the tension of the control cables.
(2)
Before you do the adjustment or the test of the speed brake control system, you must make sure these systems are serviceable:
(a)
The aileron control system (AMM 27-11-00/501).
(b)
The trailing edge flaps (AMM 27-51-00/501).
(3)
During the procedure, unless otherwise noted, the weight of the airplane must be on the landing gear. The ground spoiler interlock valve must be open which will permit the operation of the ground spoilers.
B.
Special Tools and Equipment
(1)
MIT65-45116 Ground Spoiler Control Valve Rigging Tool
(2)
Rig Pin Kit - F70207-107:
~............................................................................... | | | DIAMETER | LENGTH | | |REF NO.| F70207-( )| (INCHES) | (INCHES) | FUNCTION | ................................................................................. | S/B-1 | -11 | 0.309-0.311 | 6.7 |0.25 | SPEED BRAKE FORWARD DRUM | | S/B-2 | -101 | 0.309-0.311 | 3.7 |0.06 | SPEED BRAKE INPUT QUADRANT | | S/B-3 | -11 | 0.309-0.311 | 6.7 |0.25 | GROUND SPOILER INTERLOCK VALVE | 2.......…...........….............…............…................................1
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ú ú ú 01.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 502Jul 12/02
C.
D.
E.
F.
G.
A
737-300/400/500MAINTENANCE MANUAL
Standard Tools and Equipment
(1)
Cable Tensiometer, 0 to 150 pound range for 1/8-inch cable
(2)
AIRPLANES WITH A SPEED BRAKE LEVER POSITION SENSOR; Angle Position Indicator - Accuracy of |0.02 degree, Resolution 0.001 degree - North Atlantic Model 8810 (Preferred) (60 Plant Ave, Hauppauge, NY)
(3)
AIRPLANES WITH A SPEED BRAKE LEVER POSITION SENSOR; Angle Position Indicator - Accuracy of |0.02 degree, Resolution 0.001 degree - ILC-DDC Model HSR 203-1 (Optional) (105 Wilbur Place, Bohemia, NY 11716)
Consumable Materials
(1)
A00247 Sealant BMS 5-95
(2)
B00365 Solvent - Methyl-Ethyl-Ketone TT-M-261
(3)
C00308 Corrosion Preventive Compound, MIL-C-11796, Class 3
(4)
D00633 Grease - BMS 3-33 (Recommended)
(5)
D00013 Grease - MIL-G-23827 (Alternate)References
(1)
07-11-11/201, Jack Airplane
(2)
24-22-00/201, Manual Control
(3)
27-62-00/201, Speed Brake Control SystemAccess
(1)
Location Zone 101 Control Cabin - Left 102 Control Cabin - Right 202 Lower Nose Compartment 216 Left Main Wheel Well 217 Right Main Wheel Well 307 Left Wing Trailing Edge Outboard Flap and Spoilers 309 Left Wing Trailing Edge Inboard Flap and Spoilers 407 Right Wing Trailing Edge Outboard Flap and Spoilers 409 Right Wing Trailing Edge Inboard Flap and Spoilers
Procedure
S 825-010
(1)
Adjust the speed brake control lever:
(a)
Move the speed brake lever to the DOWN position.
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