(6)
Ladder - Stand (to observe the elevator trailing edge displacement scale on the tail cone)
(7)
Sensor Calibration Tool - Angle-of-Airflow; F72786-181
(8)
AIRPLANES WITH -911 FCC; Voltmeter - Digital; battery powered, Fluke Model 27STD
(9)
Breakout Box - C22005-2
(10)
Adapter Cable - C22005-5References
(1)
AMM 21-58-00/501, Equipment Cooling System
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 29-15-00/201, Hydraulic A, B, and Standby System
(4)
AMM 34-28-00/201, Inertial Reference System
Prepare for the Rigging Tests
S 845-128
(1) Do the preparation for DFCS BITE test in this task: Test - Digital Flight Control System". "Operational
S 745-148
(2) Do these steps to get access to the Rigging Tests: (a) Push the INIT REF key on the CDU keyboard to show the POS INIT page or PERF INIT page. (b) Push the LSK adjacent to <INDEX to show the INIT REF INDEX 1/1 page.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 08 Page 550 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
A
737-300/400/500MAINTENANCE MANUAL
Push the LSK adjacent to MAINT> to show the MAINT BITE INDEX
1/1 page.
Push the NEXT PAGE key on the CDU keyboard to show the DFCS
BITE TEST OVERNIGHT MAINT 2/2 page.
Push the LSK adjacent to <RIGGING to do the rigging test.
Do the preparation steps as shown on the CDU display.
Push the LSK adjacent to <CONTINUE.
Make sure that the Rigging Tests Index is shown on the CDU
display.
NOTE: This permits the selection of the DFCS Rigging Tests.
____
~...............................
| DFCS BITE TEST |
| RIGGING -A / -B 50.00 |
| <ELEVATOR AILERON> |
| |
| <FLAPS STABILIZER> |
| |
| <CWS MACH TRIM> |
| |
| |
| |
| |
| |
| <INDEX EXIT> |
| |
2...............................1
Do the preparation steps as shown on the CDU dipslay.Do the BITE rigging tests as shown on the CDU display.
NOTE: The shear rivets on the actuator control arms can wear
____ and can cause problems with the actuator drive. Refer to the actuator removal/installation for the shear rivet check.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
22-11-00
ú ú 11 Page 551 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
E. Elevator Rigging Tests
S 865-070
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1)
Supply hydraulic power (AMM 29-15-00/201).
S 745-066
(2)
Push the LSK adjacent to <ELEVATOR from the Rigging Tests Index.
S 745-182
(3)
Push the LSK adjacent to <CONTINUE.
S 745-067
(4)
Push the LSK adjacent to <COMPLETE ELEV RIG to do a complete test of the elevator rigging.
S 745-068
(5)
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.
S 745-069
(6)
Make sure the values of the A and B sides are in the limits as shown below or on the CDU display.
S 745-072
(7)
Do the pitch sensor check:
(a) For test 51.01 and test 51.11 make sure the stabilizer B
dimension is within the limits shown on the CDU. Test 51.01 STAB POS (VAC) Limits: -0.07 to 0.07
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 自动飞行 AUTOFLIGHT 1(67)
