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TB20 MAINTENANCE MANUAL 32 起落架 TB20飞机维护手册(100)

时间:2011-11-03 13:08来源:蓝天飞行翻译 作者:航空
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7) Position travel jig (6), 8110 TB20 00000, on the nose landing gear. Attach jig with two clamps on its upper section.
8) Move the centering plate of travel jig forward and check the rudder neutral position.
9) If necessary, adjust R.H. interconnection rod (2) - refer to 20-00-11.
10) If the rudder still fails to reach the neutral position, remove tail cone 222 - refer to 53-20-04, and adjust rudder input rod - refer to 20-00-11.
11) If necessary, actuate L.H. interconnection rod (4) to align rudder pedals (3) - refer to 20-00-11. NOTE : Comply with the 11.8 in (300 mm) dimension - refer to 27-20-01.
12) Remove nose wheel travel jig (6).
13) Check rudder travel - refer to 27-20-00.
CAUTION : EXERCISE SPECIAL CARE WHEN REMOVING THE TOOL TO AVOID DAMAGING INSTALLED ANTENNAS AND THE SKINS.
14) Remove the rudder travel jig.
15) Lower the aircraft to ground and remove the jack.
16) Install the nose landing gear door - refer to 32-20-07.
17) Make sure all the tools and materials are removed and the work area is clean and free from debris. Post-MOD. 151
18) Install dorsal fin 225.
All
19) If removed, install tail cone 222 - refer to 53-20-04.
20) Install engine cowlings 121 and 131 - refer to 71-10-01.
 
0,4 mm
( 0.016 in )
Centering device - Adjustment / test
Figure 201 - Without travel iig
ABAA
Validity : S / N 1 - 9999 32 50 00Page 203
(CA) JUN 01
 
Centering device - Adjustment / test
Figure 201A - With travel iiq
ABAA
Validity : S / N 1 - 9999 32 50-00Page 204
(CA) JUN 01
 
POSITION INDICATING SYSTEM AND ALARMS
DESCRIPTION AND OPERATION
1. GENERAL
The position indicating system and alarms supply the pilot with information and necessary means to control, check and visualize the landing gear extension or retraction.
This assembly includes :
- 1 configuration and control box,
- 1 alarm box,
- 1 ground safety microswitch.
2. LOCATION (Figure 1)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Configuration and control box 1 250 / 32-60-00
Alarm box 1 250 / 31-50-00
Ground safety microswitch 2 730 / 740 / 32-60-01

3. DESCRIPTION (Figure 1)
A. Configuration and control box
NOTE : S / N 1 - 464, 466 - 525 - see Detail A, S / N 465, 526 - 9999 - see Detail B.
The landing gear configuration and control panel is located on the R.H. side of the L.H. subpanel. The following elements are located on the landing gear control panel :
- A press-to-test button "TEST" to check indicator lights,
- A red warning light when landing gear is operating ("up" - "down") or non-locked,
 
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