曝光台 注意防骗
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(h) Move the captain’s control column aft with a push/pull gauge (0-50 lbs), STD-1100 to set the
elevator trailing edge to 1.20 +/- 0.05 inches (30.5 +/- 1.3 millimeters) up from the neutral
position.
1) Make sure the force to hold the control column at this position is 38.0 +/- 4.0 pounds
(169.0 +/- 17.8 newtons).
(i) Move the captain’s control column forward with a push/pull gauge (0-50 lbs), STD-1100 to
set the elevator trailing edge to 1.20 +/- 0.05 inches (30.5 +/- 1.3 millimeters) down from
the neutral position.
1) Make sure the force to hold the control column at this position is 38.0 +/- 4.0 pounds
(169.0 +/- 17.8 newtons).
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EFFECTIVITY
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(j) Set the FLT CONTROL A switch to the OFF position and FLT CONTROL B switch to the ON
position.
(k) Move the captain’s control column aft with a push/pull gauge (0-50 lbs), STD-1100 to set the
elevator trailing edge to 1.20 +/- 0.05 inches (30.5 +/- 1.3 millimeters) up from the neutral
position.
1) Make sure the force to hold the control column at this position is 38.0 +/- 4.0 pounds
(169.0 +/- 17.8 newtons).
(l) Move the captain’s control column forward with a push/pull gauge (0-50 lbs), STD-1100 to
set the elevator trailing edge to 1.20 +/- 0.05 inches (30.5 +/- 1.3 millimeters) down from
the neutral position.
1) Make sure the force to hold the control column at this position is 38.0 +/- 4.0 pounds
(169.0 +/- 17.8 newtons).
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-00-00-080-001
(1) Remove the adapter, SPL-1674 and control column assembly protractor, SPL-1680 from the
captain’s control column.
SUBTASK 27-00-00-080-002
(2) Remove the 3M #250 tape, G00270.
SUBTASK 27-00-00-080-003
(3) Remove the vinyl adhesive Scotch Brand No.471 tape, G02219 and black polyethylene sheet film,
G00252, used to cover and seal the drain holes, and the 4-foot or longer piece of the orange
barricade barricade tape, G02443 from the drain hole in each pitot probe.
SUBTASK 27-00-00-080-004
(4) Remove the regulator, SPL-1742:
(a) Disconnect the pressure lines of the regulator, SPL-1742 from the two pitot probes.
(b) Disconnect the pressure gage lines of the regulator, SPL-1742 from the drain holes.
SUBTASK 27-00-00-420-001
(5) Install the drain plugs to the systems A and B pitot lines.
SUBTASK 27-00-00-410-001
(6) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-00-00-860-008
(7) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
SUBTASK 27-00-00-930-008
(8) Attach a LIGHT INOP placard to the FEEL DIFF PRESS light.
------------------------- END OF TASK ---------------------------
TASK 27-00-00-440-803
7. MMEL 27-10 (DDPG) Restoration - FEEL DIFF PRESS Light Inoperative
A. General
(1) This task puts the airplane back to its usual condition after operation with the FEEL DIFF PRESS
light on the flight controls panel inoperative.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-00-00
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D633A101-GUN
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B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-00-00-960-002
(1) Replace the FEEL DIFF PRESS light.
SUBTASK 27-00-00-810-003
(2) If the FEEL DIFF PRESS light was not the problem, then do these steps to correct the fault:
(a) Find the fault code or description of the fault that occurred.
(b) If you find a fault code, then do these steps:
1) Go to the Fault Code Index in the applicable chapter of the FIM and find the fault code.
NOTE: The first two digits of the fault code is the FIM chapter.
2) Find the task number on the same line as the fault code.
3) Go to the task in the FIM and do the steps in the task.
(c) If you find a description of the fault, then do these steps:
1) Go to the Observed Fault List at the beginning of the FIM and find the best description
for the fault.
2) Find the task number on the same line as the fault description.
3) Go to the task in the FIM and do the steps in the task.
SUBTASK 27-00-00-930-009
(3) Remove the LIGHT INOP placard from the FEEL DIFF PRESS light.
------------------------- END OF TASK ---------------------------
TASK 27-00-00-040-804
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(47)
