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Torque rod 1 210 / 230 218 / 236 27-10-00
Intermediate bellcrank 2 500 / 600 512 / 612 27-10-00
Outboard bellcrank 2 500 / 600 516 / 616 27-10-00
Input rod 2 500 / 600 516 / 616 27-10-00
3. DESCRIPTION
A. Torque rod
Located in the fuselage front section and crossing the cabin floor, the torque rod links and interconnects the control wheels / pylon assembly with the control rods. A lever is secured to its rear end ; the travel of the lever is limited by two adjustable stops, which are factory-adjusted, then -riveted to the cabin floor.
B. Intermediate bellcrank
Located at the wing root, the intermediate bellcrank reverses motion at the wing spar feedthru. It is linked to the torque rod and to the outboard bellcrank by two non-adjustable control rods.
C. Outboard bellcrank
Located in the wings, forward of the aileron inboard end, the outboard bellcrank converts the side motion of the control rod into longitudinal motion of the input rod.
ABAA
Validity : S / N 1 - 9999 27 10-00Page 1
(CA) MAR 00
D. Input rod
Located in the aileron inboard section, the input rod links the outboard bellcrank to the aileron. The two adjustable ends of the rod enable aileron travel adjustment.
ABAA
Validity : S / N 1 - 9999 27-10 00 (CA) MAR R g e 2
00
Roll control - Identification and location of components
Figure 1 (1 / 3)
B - Intermediate bellcrank
Roll control - Identification and location of components
Figure 1 (2 / 3)
Roll control - Identification and location of components
Figure 1 (3 / 3)
ABAA
Validity : S / N 1 - 9999 27 10-00Page 5
(cA) MAR 00
PAGE INTENTIONALLY LEFT BLANK
ROLL CONTROL
MAINTENANCE PRACTICES
1. SERVICING
None
2. REMOVAL / INSTALLATION
None
3. ADJUSTMENT / TEST - ROLL CONTROL
A. Tools and consumable materials
- Clinometer (Qty 2)
- Hydraulic jacks
- Ruler 47 in (1.20 m)
- Clamps
- Aileron travel jig 8653 TB10 00000 (Qty 2)
NOTE 1 : Travel jigs are used only in Paragraph C. in replacement of clinometers and jacks.
NOTE 2 : Travel adjustment can be performed with a single jig or clinometer, but adjusting
R.H. and L.H. ailerons simultaneously is time- and handling-saving.
B. Adjustment of ailerons without travel jig(s) (Figures 202, 204, 205 and 207)
NOTE : The adjustment of the roll control must be preceded by a check of slack values - see Paragraph 4. C.
3) Level the aircraft - refer to 08-10-00.
4) Remove the cowling under hull 218.
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本文链接地址:TB20 MAINTENANCE MANUAL 27 FLIGHT CONTROLS TB20飞机维护手册 飞行操纵(9)
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