1) With rigging pin SB-1 installed, dimension A in figure 504 is within specified limits using rigging tool MIT65-45116. If not, this condition may be met by adjusting control rod per paragraph 2.C.(3).
(d)
Ground Spoiler Interlock Valve
506
Nov 15/72 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-62-0 Page 502A
1) If airplane weight is on landing gear, dimension B in Fig. 505 is 1.62 inch minimum.
NOTE: Dimension B is to be used for system verification only. Do not use when rigging valve.
2) If airplane is jacked with right main gear oleo fully extended, rigging pin S/B-3 fits freely.
3) If not this condition may be met by adjusting push-pull cable per par. 2.C.(4).
(e)
No. 1 and No. 8 Ground Spoilers
1) With ground spoilers hydraulically retracted and wing flaps full up, spoiler to flap clearance is within limits shown in Fig. 506. If not, this condition may be met by adjusting actuator rod end per par. 2.C.(5).
(f)
No. 4 and No. 5 Ground Spoilers
1) With ground spoilers hydraulically retracted and wing flaps full up, ground spoiler to flap clearance is within limits shown in Fig. 506. If not, this condition may be met by adjusting actuator rod end per par. 2.C.(5).
B. Equipment and Materials
(1)
Cable Tensiometer, 0 to 150 pound range for 1/8 inch cable
(2)
Rigging Pins Kit - F70207-3, -52, -61 or -84:
(4)
Ground Spoiler Control Valve Rigging Tool - MIT65-45116
(5)
Grease, MIL-G-23827
(6)
Corrosion Preventive Compound, MIL-C-11796, Class 3 (Ref 20-30-41)
(7)
Sealant - BMS 5-95 (Ref 20-30-11)
REF NO. F70207-( ) DIAMETER (INCHES) LENGTH (INCHES) FUNCTION
S/B-1 S/B-2 S/B-3 -11 -13 -11 0.309-0.311 0.309-0.311 0.309-0.311 6.7 +0.25 2.35 +0.06 6.7 +0.25 Speed Brake Forward Drum Speed Brake Input Quadrant Ground Spoiler Interlock Valve
504
Feb 20/88 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-62-0 Page 503
C. Adjust Speed Brake Control System
(1) Adjust Speed Brake Control Lever
(a)
Place speed brake control lever in DOWN detent. Ensure that lever latch is in detent on control stand.
(b)
In fuselage lower nose compartment, check that rigging pin SB-1 can be freely installed through speed brake forward quadrant into structure. If rigging pin cannot be installed freely accomplish the following steps: 1) Disconnect upper end of lower control rod from idler link (Fig. 502). 2) Loosen checknut and adjust rod end until rod end bolt fits freely with rigging pin
SB-1 installed. 3) Install rod end bolt with washer under bolt head. Secure bolt with washer and
locknut. 4) Tighten checknut on rod end. 5) Ensure that rod end is visible in inspection hole of control rod.
(c) Adjust control lever detents. 1) Place speed brake control lever in DOWN detent. Ensure that lever latch is in detent on control stand.
2) Check that center of DOWN detent mark on control stand indicator plate aligns with indicator on aft face of control lever. If not within limits, loosen indicator plate attaching screws and move plate until it aligns with indicator on speed brake lever. Tighten attaching screws.
506
27-62-0 Page 504 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Feb 01/95
3) Disconnect detent spring from speed brake forward drum cam roller.
4) Install rig pin SB-1 in forward drum quadrant.
5) Loosen bolts in cam roller lever arm bracket and adjust to align roller contact
surface with index mark on detent cam. Tighten bolts. (See section A-A, figure/502.)
6) Connect detent spring to cam roller lever arm. Remove rigging pin SB-1 from forward drum quadrant.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 3(120)
