曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Pressure Removal (P/B 201)
B. 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-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. 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
D. Prepare for the Adjustment
SUBTASK 27-61-00-860-018
(1) Do this task: Remove Pressure from the Spoiler Hydraulic Systems A and B,
TASK 27-61-00-800-802.
E. Ratio Changer Input Rod Adjustment
SUBTASK 27-61-00-020-007
(1) Move the speed brake lever to the DOWN position.
SUBTASK 27-61-00-020-008
(2) Make sure the aileron control system is in the neutral position.
SUBTASK 27-61-00-820-002
(3) Install the rig pin A/S-14 from the rig pin kit, SPL-1585 in the spoiler mixer.
SUBTASK 27-61-00-820-003
(4) Install the rig pin S/B-2 from the rig pin kit, SPL-1585 in the ratio changer (Figure 501).
SUBTASK 27-61-00-820-004
(5) Make sure that you can easily install the rig pin A/S-3 from the rig pin kit, SPL-1585 in the spoiler
control quadrant.
SUBTASK 27-61-00-820-005
(6) If you cannot easily install the rig pin A/S-3, adjust the ratio changer input rod [37]:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 517
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Remove the bolt [32], washer [33], washer [34] and nut [35] that connects the ratio changer
input rod [37] to the input crank [31].
(b) Install the rig pin A/S-3 from the rig pin kit, SPL-1585 in the spoiler control quadrant.
(c) Loosen the checknut [38] on the ratio changer input rod [37].
(d) Adjust the rod end until you can install the bolt to attach the input rod.
NOTE: It must be possible to install the bolt without excessive force.
(e) Install the bolt [32] with the head up, washer [33], washer [34] and nut [35].
(f) Tighten the checknut [38] on the ratio changer input rod [37].
SUBTASK 27-61-00-820-006
(7) Remove the rig pins A/S-3, A/S-14, and S/B-2.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-61-00-410-004
(1) Do this task: Put the Spoiler Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-61-00-840-802.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 518
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Ratio Changer Input Rod Adjustment
Figure 502 (Sheet 1 of 2)/27-61-00-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 519
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Ratio Changer Input Rod Adjustment
Figure 502 (Sheet 2 of 2)/27-61-00-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 520
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-61-00-820-803
5. Flight Spoiler Adjustment
(Figure 501, Figure 502, Figure 503)
A. References
Reference Title
20-30-84-910-801 Final Cleaning of Metal Prior to Painting (Series 84) (P/B 201)
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
27-62-00-800-802 Remove Pressure from the Speed Brake Hydraulic Systems A and B
(P/B 201)
27-62-00-840-801 Put the Speed Brake Hydraulic systems A and B Back to the
Condition Before the Pressurization (P/B 201)
B. 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.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600-700-800-900 飛機維護手冊6 AIRCRAFT MAINTENANCE MANUA(6)