D. Procedure
S 214-010
(1)
Make sure the control column is in the neutral position.
S 434-011
(2)
Install the control column position transducer into the collar bracket.
S 204-035
(3)
Make sure the transducer mark EZ is align with the collar bracket mark.
(4)
Install and tighten the screw to the collar bracket.
S 434-012
GUN 001-008, 010, 101 POST-EO B531006; ú 31-31-08
GUN 051, 102-999 ú ú 11 Page 404 ú Jan 28/02
A
757 MAINTENANCE MANUAL
S 434-013
(5)
Install the crank arm into the transducer.
S 434-014
(6)
Align the crank arm slot with the index mark on the transducer's serrated shaft.
S 434-015
(7)
Install and tighten the screw that holds the crank arm.
S 434-016
(8)
Connect the electrical connector to the transducer.
S 034-017
(9)
Remove the rig pin E/ST6 from the crank and shaft assembly on the control column.
E. Control Column Position Transducer Test
S 864-058
(1)
If you use test equipment other than the hand-held download unit (HHDLU), install the tester to the test connector at the right side panel, P61.
S 864-059
(2)
If you use the hand-held download unit (HHDLU), attach the HHDLU to the test connector at the front side of the flight data recorder.
NOTE: To get access to the FDR, open the lower ceiling panel No. 1
____ above the aft galley (AMM 25-22-02/401). The HHDLU can only be connected to the AlliedSignal flight data recorder (FDR).
S 864-019
(3)
Supply electrical power (AMM 24-22-00/201).
S 864-020
(4)
Remove the DO-NOT-CLOSE tags and close these P11 panel circuit breakers :
(a)
11C11, STICK SHAKER LEFT
(b)
11E17, FLT CONT COMPUTER POWER LEFT
(c)
11E20, FLT CONT COMPUTER PWR CENTER
(d)
11E35, FLT CONT COMPUTER PWR RIGHT
(e)
11H11, STAB TRIM CONT L
(f)
11H17, FLT CONT SHUTOFF TAIL LEFT
(g)
11H18, FLT CONT SHUTOFF TAIL CENTER
(h)
11H20, STAB TRIM CONT RIGHT
(i)
11H28, FLT CONT SHUTOFF TAIL RIGHT
(j)
11J7, FLIGHT RECORDER AC
(k)
11J8, FLIGHT RECORDER DC
(l)
11J21, STICK SHAKER RIGHT
GUN 001-008, 010, 101 POST-EO B531006; ú 31-31-08
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本文链接地址：757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 1(142)
