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212
Roll control in wings - Inspection / Check
Figure 205
Roll control in wings - Inspection / Check
Figure 206
Ity : S / N 1 - 9999 7alAA Validity 27-10-00Page 214
(BA) SEP 04
ITEM
THEORETICAL
DIMENSION MAXIMUM WEAR
DIMENSION L.H. WING R.H. WING DECISION ACTION
1 Dia. 0.2362/0.2391 in
(6.0/6.075 mm) Dia. 0.2409 in
(6.120 mm)
2
3
4
5 Dia. * 0.2409 in
(6.120 mm)
6
7
8
9 Dia. 0.3543/0.3551 in
(9.0/9.022 mm) Dia. 0.3566 in
(9.058 mm)
10
(*) Maximum wear dimension without pitting marks.
AAAA
Validity : S / N 1 - 9999 Roll control bellcranks and rods
Table 201
27-10 00 (BA) Page (BA)
ITEM THEORETICAL
DIMENSION MAXIMUM WEAR
DIMENSION * BORING DECISION ACTION
1 Dia. 0.6102/0.6109 in
(15.5/15.518 mm) Dia. 0.6119 in
(15.543 mm)
2
3
4
5 Dia. 0.1968/0.1998 in
(5.0/5.075 mm) Dia. 0.2015 in
(5.120 mm)
6 Dia. 0.2362/0.244 in
(6.0/6.2 mm) /
7
Pylon assy
Table 202 (1/2)
ITEM THEORETICAL
DIMENSION MAXIMUM WEAR
DIMENSION * BORING DECISION ACTION
8 Dia. 0.198/0.1999 in
(5.030/5.078 mm) Dia. 0.2009 in
(5.105 mm)
9
10
11
12
13
(*) Maximum wear dimension without elongation or scratches.
Maximum slack value between torque rod (18) and bearings (31) : 0.039 in (1 mm).
If boring (5) is out-of-tolerance, replace the torque rod assy with P/N TB10 27013004 - refer to 27-10-01 of Illustrated Parts Catalog.
Pylon assy
Table 202 (2/2)
AAAA
Validity : S / N 1 - 9999 27-10-00Page 217
(BA) SEP 04
PAGE INTENTIONALLY LEFT BLANK
WA
Validity : S / N 1 - 9999 27-10-00Page 218
(BA) SEP 04
YAW CONTROL
DESCRIPTION AND OPERATION
1. GENERAL
The yaw control of the aircraft is provided by the rudder which is actuated and linked via control linkage to the pedals in the cockpit.
This rod-operated control is routed along the central section of the floor as far as frame C6, then into the rear section of the fuselage up to the control surface.
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