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Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-37-860-001
(2) Use the bar, SPL-1677 to set the B dimension at 39.89 +/- 0.01 inches (1013.21 +/- 0.25
millimeters) (Figure 401).
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SUBTASK 27-31-37-860-002
(3) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-37-860-003
(4) Open these circuit breakers and install safety tags:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 2 C01064 AFCS SYS B MACH TRIM DC
B 3 C01046 AFCS SYS B FCC DC
B 4 C00716 AFCS SYS B ENGAGE INTLK
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
C 1 C01037 AFCS SYS B MACH TRIM AC
C 2 C01042 AFCS SYS B SNSR EXC AC
D 10 C00840 FLIGHT CONTROL STAB TRIM ACTUATOR
F/O Electrical System Panel, P6-3
Row Col Number Name
D 13 C00311 INDICATOR MASTER DIM BUS 1
D 14 C00312 INDICATOR MASTER DIM BUS 2
SUBTASK 27-31-37-480-001
CAUTION: YOU MUST INSTALL THE SAFETY PIN, F80153-1 IN THE RIG PIN HOLE OF THE
ELEVATOR FEEL COMPUTER. IF THE ELEVATOR FEEL COMPUTER IS NOT
ATTACHED TO THE INPUT ARM, IT CAN BE EASILY DAMAGED WHEN IT IS
REMOVED.
(5) Install the pin, SPL-1673 in the input arm [8] and the elevator feel computer assembly [1].
F. Elevator Feel Computer Removal
SUBTASK 27-31-37-020-001
CAUTION: DO NOT LIFT THE ELEVATOR FEEL COMPUTER BY THE INPUT ARM, OR APPLY A
TORQUE OF MORE THAN 300 POUND-INCHES (33.9 NEWTON-METERS) TO THE INPUT
ARM. THE ELEVATOR FEEL COMPUTER IS VERY SENSITIVE AND IT CAN EASILY BE
DAMAGED.
(1) Remove the elevator feel computer assembly [1]:
(a) Disconnect the spring [16] from the elevator feel computer assembly [1].
(b) Remove the nut [23], washer [22], and bolt [21] to disconnect the stabilizer pushrod [2] from
the input arm [8].
(c) Disconnect the electrical connector [7] from the elevator feel computer assembly [1].
WARNING: RELEASE THE CONNECTION SLOWLY AND LET THE PRESSURE DECREASE
BEFORE YOU COMPLETELY REMOVE THE HYDRAULIC LINE, IF YOU
DISCONNECT THE HYDRAULIC LINE WHEN IT HAS PRESSURE, A SPRAY OF
HYDRAULIC FLUID CAN CAUSE INJURY TO PERSONS.
(d) Disconnect the hydraulic lines, pitot lines, and static lines from the elevator feel computer
assembly [1].
NOTE: Install tags on lines and port fittings to clearly show the correct connection
location. See (Flareless Tubing Assembly Removal, TASK 20-10-51-000-801) for
instructions on correct tubing removal.
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(e) Install caps to the hydraulic lines, pitot lines, and static lines.
(f) Install plugs to all ports.
(g) Remove the nuts [6], washers [5], washers [4], and bolts [3] that attach the elevator feel
computer assembly [1] to the airplane structure.
(h) Remove the elevator feel computer assembly [1] from the airplane.
SUBTASK 27-31-37-540-001
(2) Discard the packings [9], packings [12], packings [14], packings [17], and packings [19].
------------------------- END OF TASK ---------------------------
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Elevator Feel Computer Installation
Figure 401 (Sheet 1 of 3)/27-31-37-990-801
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Elevator Feel Computer Installation
Figure 401 (Sheet 2 of 3)/27-31-37-990-801
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Elevator Feel Computer Installation
Figure 401 (Sheet 3 of 3)/27-31-37-990-801
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TASK 27-31-37-400-801
3. Elevator Feel Computer - Installation
(Figure 401)
A. References
Reference Title
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
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