Maintenance and Inspection Procedures Manual
Type:
CT
Series:
CTLS
LSA
Page: AII-2
AF 04800001
Revision No. 3
Date: 14 Sep 2008
Adjustment report 2
Airplane serial number:
Inspector:
Control surface
Position
Limits, degrees/mm
Actual,
degrees/mm
Note
Flap left
up (deg)
5.5 deg, Tol.+0.5 deg, -0.5
deg
up (mm)
Flap left
down (deg)
35 deg, Tol.+1 deg, -1 deg
down (mm)
Flap right
up (deg)
5.5 deg, Tol.+0.5 deg, -0.5
deg
up (mm)
Flap right
down (deg)
35 deg, Tol.+1 deg, -1 deg
down (mm)
Aileron left
up (deg)
26.5 deg, Tol.+1.5 deg, -1.5
deg
Aileron and flap zero
position
up (mm)
109 mm, Tol.+6 mm, -6 mm
is -6 degrees
Aileron left
down (deg) 12.5 deg, Tol.+1.5 deg, -1.5
deg
Aileron and flap zero
position
down (mm)
52 mm, Tol.+6 mm, -6 mm
is -6 degrees
Aileron right
up (deg)
26.5 deg, Tol.+1.5 deg, -1.5
deg
Aileron and flap zero
position
up (mm)
109 mm, Tol.+6 mm, -6 mm
is -6 degrees
Aileron right
down (deg) 12.5 deg, Tol.+1.5 deg, -1.5
deg
Aileron and flap zero
position
down (mm)
52 mm, Tol.+6 mm, -6 mm
is -6 degrees
Stabilizer
up (deg)
14 deg, Tol.+1 deg, -1 deg
Stabilizer
down (deg)
9 deg, Tol.+1 deg, -1 deg
Trim tab
down (deg)
1 deg, Tol +0.5 deg, -0.5 deg
Handle (wheel)
neutral
down (mm)
2 mm, Tol + 1 mm, - 1 mm
Stabilizer in neutral
position
Trim tab
up (deg)
23.5 deg, Tol - 2.5 deg
Handle (wheel)
forward
up (mm)
50 mm, Tol - 5 mm
Stabilizer TE up
Trim tab
down (deg)
6.5 deg, Tol -2.5 deg
Handle (wheel)
rearward
down (mm)
14 mm, Tol -5 mm
Stabilizer TE down
Rudder
left (deg)
28.5 deg, Tol.+1.5 deg, -1.5
deg
left (mm)
217 mm, Tol.+11 mm, -11 mm
Rudder
right (deg)
28.5 deg, Tol.+1.5 deg, -1.5
deg
right (mm)
217 mm, Tol.+11 mm, -11 mm
Date:
Inspector's
signature: