(2)
F72867-1 - Control Wheel Adapter Fitting
B.
Standard Tools and Equipment
(1)
Spring Scale - 0-50 pound push-pull scale with the scale graduations of 0.5 pounds or smaller
(2)
Scale - 0-2 feet, graduated in inches, tenths and hundredths of an inch
C.
References
(1)
AMM 27-31-00/201, Elevator and Tab Control System
(2)
AMM 27-31-41/501, Elevator Balance Panels
(3)
SRM 51-60-04, Outboard Elevator Balancing Procedures
D.
Access
(1)
Location Zone
101 Control Cabin, LH
102 Control Cabin, RH
711 Elevator and Tab, LH
712 Elevator and Tab, RH
E.
Procedure
S 865-045
(1)
Do this task: "Remove the Elevator Hydraulic Systems A and B" (AMM 27-31-00/201).
(2)
Use the trammel bar to set the B dimension at 41.57 |0.05 inches.
S 865-046
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 02 Page 547 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-047
(3)
Do this task: "Null Procedure - Mach Trim Actuator" (AMM 27-31-00/201).
S 735-048
(4)
Do the friction and balance test of the elevator surface:
(a)
Move the control columns in a longitudinal direction through full travel 20 times.
CAUTION: DO NOT PUT A LOAD OF MORE THAN 65 POUND ON THE ELEVATORS
_______ AT ONE TIME. IF THE LOAD IS TOO HEAVY, IT CAN CAUSE DAMAGE TO THE ELEVATORS.
(b)
Measure the breakaway forces: 1) Hold the captain's control column at the neutral position. 2) Push the elevator with your hand until the trailing edge of
each elevator aligns with the index mark, then release (Fig. 505).
(c)
If the elevator trailing edge moves down from the index mark, do the balance adjustment (SRM 51-80-02).
(d)
If one of the two trailing edges do not stay at the index mark, use the spring scale to measure the force required to move them back. 1) Measure the force that you use to move the trailing edge up
0.75 |0.15 inch from the index mark (which is referred to
as the up force). 2) Make a record of this force. 3) Measure the force that you use to move the trailing edge
down 0.75 |0.15 inch from the index mark (which is referred to as the down force). 4) If the down force is less than the up force, do the balance adjustment (SRM 51-60-04).
5) If the down force is greater than the up force, calculate the sum of these two forces. a) If the sum of these two forces is less than 16 pound,
do the test of the elevator limit travel. b) If the sum of these two forces is more than 16 pounds, do the elevator balance panel test (AMM 27-31-41/501).
S 865-059
(5) Do this task: "Put the Elevator Hydraulic Systems A and B Back to the Condition Before the Pressure Removal" (AMM 27-31-00/201).
TASK 27-31-00-735-014
8. System Test - Elevator Limit Travel
___________________________________
A. Special Tools and Equipment
(1)
F80055-1 - Trammel Bar
B.
Standard Tools and Equipment
(1)
Spring Scale - 0-50 pound push-pull scale with the scale graduations of 0.5 pounds or smaller
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 03 Page 548 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
(2)
Loading block (17 inches long, 2 x 4 wood block)
(3)
Scale - 0-2 feetReferences
(1)
AMM 27-31-00/201, Elevator and Tab Control SystemAccess
(1)
Location Zone 101 Control Cabin, LH 102 Control Cabin, RH 711 Elevator and Tab, LH 712 Elevator and Tab, RH
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(120)
