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TB20 MAINTENANCE MANUAL 27 FLIGHT CONTROLS TB20飞机维护手册 飞行操纵(32)

时间:2011-11-01 13:12来源:蓝天飞行翻译 作者:航空
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- cracks, buckling and corrosion,
- correct safetying of attachment bolts nuts (6) with cotter pins.
3) Inspect levers (7) for :
- distortions, cracks, corrosion, binding and slack,
- correct safetying of hinge pins attachment nuts (8) with cotter pins,
- slack and loose rivets on spacers (4) of levers (7).
4) Inspect the supports of levers (7) for :
- distortions, cracks, corrosion and loose rivets,
- correct tightening of nuts on frame C9.
5) Inspect input rod (5) for :
- slack, buckling, cracks, binding and corrosion,
S / N 1 - 663, 665 - 709 Pre-Kit OPT10 912700
- the condition of attachment rivets of yoke (10) and tapped end (12). S / N 664, 710 - 9999 and S / N 1 - 663, 665 - 709 Post-Kit OPT10 912700
- correct tightening of attachment nuts (11) of yoke (10) and tapped end (12). S / N 1 - 9999
- correct safetying of nut (13) of adjustable rod end (14),
- correct safetying of input rod (5) attachment nuts (9) with cotter pins.
D. Check of the elevator rotational free play (Tables 201 and 202)
1) With control wheel blocked, actuate elevator and check that play at trailing edge is 0.197 in (5 mm) maximum.
2) If play exceeds 0.197 in (5 mm), perform the following operations
a) Remove the elevator - refer to 55-20-01.
b) Mark and remove elevator control rods and levers.
c) Clean rods and levers with a clean lintfree cloth soaked with cleaning agent (TB 11-002).
d) Perform a dimensional check of elevator control supports, rods and levers borings and elevator hinge bearings borings - see Tables 201 and 202.
e) Replace the defective components or contact the manufacturer for repair.
f) Install elevator control rods and levers - refer to 20-00-11.
g) Install the elevator - refer to 55-20-01.
E. Final steps
1) Make sure all the tools and materials are removed and the work area is clean and free from debris.
2) Install inspection doors 235L and 235R, 211 L and 211 R or install the covers of the instrument panel, then reposition and lock the instrument panel.
ABAA
Validity : S / N 1 - 9999 27-30-00 Page 207
(CA) SEP 04
 
3) Install baggage compartment bottom door 242 and close baggage compartment door 219.
4) Install tail cone 222 - refer to 53-20-00.
5) Install the cowling under hull 218 and remove the warning sign prohibiting main switch-breaker operation.
ABAA
Validity : S / N 1 - 9999 27-30 Page 208
00 (CA) SEP 04
 
  1 - "Nose up" stop
2 - "Nose down" stop
3 - Rod
4 - Spacer
5 - Input rod
6 - Nut
7 - Lever 8 - Nut
9 - Nut
10 - Yoke
11 - Nut
12 - Tapped end
13 - Nut
14 - Adjustable rod end
 
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