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TCH.1C-27J-2-27JG
2-7.1
ADJUSTMENT CABIN CONTROL CABLES
TENSION (refer to figure 
2-3, sheet 1/7
) and (refer
to figure 
2-3, sheet 2/7
) (Cont'd)
NOTE
If the above requirement is not obtained,
re-adjust the cable tension properly.
5.Check that the control wheels (2) rotations are free
without interferences.
6.Check that the clearance between all quadrants ends
and the cable guard bolts for the whole aileron control
is in the range 0.039 to 0.06 in (1 to 1.6 mm) (cable
3.2 mm), range 0.039 to 0.078 in (1 to 2.00 mm)
(cable 4 mm) (Table 2-3).
Table 2-3. Clearance between flight controls pulleys
and guard pins
CONTROL LINE
CABLE DIAMETER
CLEARANCE
Ailerons
Cable 5/32" (4 mmm)
0.039 thru 0.078 in (1 thru 2
mm)
Cable 1/8" (3.2 mm)
0.039 thru 0.062 in (1 thru 1.6
mm)
Rudder
Cable 1/8" (3.2 mm)
0.039 thru 0.062 in (1 thru 1.6
mm)
Elevator
Cable 5/32" (4 mm)
0.039 thru 0.078 in (1 thru 2
mm)
Cable 1/8" (3.2 mm)
0.039 thru 0.062 in (1 thru 1.6
mm)
Pitch trim
Cable 1/8" (3.2 mm)
0.031 thru 0.059 in (0.8 thru
1.5 mm)
Flaps
Cable 1/8" (3.2 mm)
0.039 thru 0.062 in (1 thru 1.6
mm)
7.Close the access panel 130B and 130C.
27-10-05
2-35