曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

(Part #: DG-200, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPP-500G, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-150, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-50, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: FDIX 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDIX 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDV 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Opt Part #: FDI 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
SPL-1674 Assembly - Adapter, Control Wheel, Torque and Force Test
(Part #: F72867-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1680 Protractor - Assembly, Control Column
(Part #: 4MIT65B80307-1, Supplier: 81205, A/P Effectivity: 737-100,
-200, -200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800,
-900, -900ER, -BBJ)
(Part #: A27021-29, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
D. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
334 Left Horizontal Stabilizer - Elevator
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 581
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Zone Area
344 Right Horizontal Stabilizer - Elevator
E. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
F. Prepare for the Test
SUBTASK 27-31-00-860-079
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-00-860-080
(2) Do this task: Null Procedure - Mach Trim Actuator, TASK 27-31-00-700-801.
SUBTASK 27-31-00-010-016
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-860-081
(4) Use the bar, SPL-1677 to set the "B" dimension at 4 units of trim (39.89 +/- 0.01 inches or 1013.2
+/- 0.3 mm) (Figure 502).
G. Control Column Power Force Test
SUBTASK 27-31-00-730-009
(1) Do the control column force test (with hydraulics unpressurized):
(a) Move the captain’s control column slowly aft and hold at the elevator trailing edge up
position of 3.59 - 3.69 inches (91.2 - 93.7 mm) (Figure 523).
1) Use the force gauge, COM-1557 to make sure the force to hold the control column is
between 11 - 53 pounds (107 - 236 newtons) (Figure 514).
2) Center the control column.
(b) Move the captain’s control column slowly forward and hold at the elevator trailing edge
down position of 3.64 - 3.74 inches (92.5 - 95.0 mm) (Figure 523).
1) Use the force gauge, COM-1557 to make sure the force to hold the control column is
between 19 - 63 pounds (160 - 280 newtons) (Figure 514).
SUBTASK 27-31-00-730-019
(2) Do the control column force test (with hydraulics pressurized):
WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM THE FLIGHT CONTROL
SURFACES. THE AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS,
STABILIZER AND NOSE GEAR CAN MOVE SUDDENLY WHEN YOU SUPPLY
HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO
EQUIPMENT.
(a) Pressurize elevator hydraulic systems A and B. To pressurize them, do this task: Elevator
Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
(b) Move the captain’s control column lightly forward and aft to put the system in the neutral
position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 582
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Attach "DO-NOT-MOVE" tags on the control columns.
(c) Attach approximately 36 inches (900 mm) of masking tape to the tailcone, forward of the
right elevator index plate (Figure 523).
NOTE: Make sure there are approximately 18 inches (450 mm) of masking tape above the
index plate and approximately 18 inches (450 mm) of masking tape below the
index plate.
(d) Make a mark of the neutral position of the elevator trailing edge on the masking tape.
1) Use this mark of the neutral position as reference.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機(jī)維護(hù)手冊2(159)