EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-01
ALL ú ú 01 Page 433 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(k)
Tighten the bolt 30.
(l)
Install the washer (23) and the nut (25) on the bolt assembly (24). Tighten the nut to 800-1000 pound-inches more than the run-on torque.
(m)
Install the washer (12) and the nut (13) at the upper actuator. Tighten the nut to 800-1000 pound-inches more than the run-on torque.
(n)
Install the bushings (8) and the bolts (9) for the lower actuator (7) and its reaction link (14).
(o)
Install the washers (12) and the nuts (13) on the bolts (9). Tighten the nuts to 800-1000 pound-inches more than the run-on torque.
S 434-075
(10)
Do this step to connect the control rod of the position transmitter to the front spar of the rudder:
(a)
Install the bolt (34), the washer (35), and the nut (36).
S 214-076
(11)
Make sure the seals for the lower rudder do not have damage.
S 224-098
(12)
Make sure the seals have the correct clearances (Fig. 403).
S 434-077
(13)
Do the procedure above to install the lower rudder.
TASK 27-21-01-714-078
6. Upper and Lower Rudder Test___________________________
A. Special Tools and Equipment
(1)
G12001-XX Rig pin NS-6
B.
References
(1)
09-11-00/201, Towing
(2)
12-21-17/301, Rudder and Rudder Trim Control System
(3)
24-22-00/201, Manual Control
(4)
29-11-00/201, Main Hydraulic Supply System
(5)
31-61-00/201, Integrated Display System
C.
Access
(1)
Location Zone
325 Lower Rudder
326 Upper Rudder
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-01
ALL ú ú 01 Page 434 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(2)
Access Panel
324BL Inspection Access Panel
324CL Inspection Access Panel
324DL Inspection Access Panel
324EL Inspection Access Panel
324FL Inspection Access Panel
324GL Inspection Access Panel
324HL Inspection Access Panel
324KL Inspection Access Panel
324LL Inspection Access Panel
324UL Inspection Access Panel
D.
Procedure
S 864-079
(1)
Supply electrical power (Ref 24-22-00/201).
S 864-080
(2)
Supply power to EICAS (Ref 31-61-00/201).
S 864-100
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(3)
Supply hydraulic power for hydraulic systems No. 1 and No. 4 (Ref 29-11-00/201).
S 714-127
(4)
Move the rudder pedals fully left, then move them fully right.
S 714-086
(5)
Make sure the rudders move smoothly.
S 284-087
(6)
Look at the rudder position indication on the EICAS maintenance page for the flight controls.
(a)
When the rudder pedals are in their fully left and fully right positions, make sure the rudder position indication shows
31.5 +/- 1.5 degrees.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(76)
