(s)
Move the captain's control column slowly aft until the right elevator is at 1.20 |0.05 inches up from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 20.5 |2.0
pounds.
(t)
Move the captain's control column slowly forward until the right elevator is at 1.20 |0.05 inches down from the neutral index. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 21.75 |5.25
pounds.
(u)
Move the captain's control column slowly aft until the right elevator is at 4.80 |0.05 inches up from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 39.0 |4.0
pounds.
(v)
Move the captain's control column slowly forward until the right elevator is at 4.80 |0.05 inches down from the neutral index. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 47.0 |4.5
pounds.
(w)
Set the FLT CONTROL B switch to OFF and the FLT CONTROL A switch to ON.
(x)
Move the captain's control column slowly aft until the left elevator is at 1.20 |0.05 inches up from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 20.5 |2.0
pounds.
(y)
Move the captain's control column slowly forward until the left elevator is at 1.20 |0.05 inches down from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 21.75 |5.25
pounds.
(z)
Move the captain's control column slowly aft until the left elevator is at 4.80 |0.05 inches up from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 39.0 |4.0
pounds.
(aa) Move the captain's control column slowly forward until the left elevator is at 4.80 |0.05 inches down from the neutral index. 1) Hold the control column at this position.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 02 Page 567 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
2) Make sure the column force is in the limit of 47.0 |4.5 pounds. (ab) Set the FLT CONTROL A switch to OFF and the FLT CONTROL B switch to ON.
(ac) Move the captain's control column slowly aft until the right elevator is at of 1.20 |0.05 inches up from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 20.5 |2.0
pounds.
(ad) Move the captain's control column slowly forward until the right elevator is at 1.20 |0.05 inches down from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 21.75 |5.25
pounds.
(ae) Move the captain's control column slowly aft until the right elevator is at 4.80 |0.05 inches up from the neutral position. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 39.0 |4.0
pounds.
(af) Move the captain's control column slowly forward until the right elevator is at 4.80 |0.05 inches down from the neutral index. 1) Hold the control column at this position. 2) Make sure the column force is in the limit of 47.0 |4.5
pounds.
(ag) Set the FLT CONTROL B switch to OFF.
(ah) Release the pressure from the pitot system to zero.
NOTE: Do not disconnect the pressure line from the airplane.
____
(ai) Set the FLT CONTROL A switch to on.
S 755-101
(4)
Do a test of the autopilot authority in this task: "Elevator Rigging Test" (AMM 22-11-01/501).
(a)
Set the FLT CONTROL A switch to off.
S 625-095
(5)
Make sure the the seals are removed from the drain holes in each feel pitot tube on the fin.
S 035-096
(6)
Make sure the pressure gage lines are removed from the drain holes of the pitot system A and B below the feel computer.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 2(130)
