Cessna SKYMASTER 336 1964 Service Manual page 239

16-17. STRUCTURAL ALIGNMENT.
16-18. The dimensions and angles shown in figures
16-3 and 16-4 will establish structural alignment in
accordance with the following chart:
Wing root angle of incidence ........
. 2. 0
Wing tip angle of incidence
.........
0.0°
Wing twist (washout)
. . . ..... . 2.0
Stabilizer angle of incidence (on ground,
unsupported) .............
3. 0°
Stabilizer angle of incidence (in flight) . ...
-3. 5
NOTE
On airplanes prior to Serial No. 336-0033,
except 336-0016, the stabilizer angle of inci-
dence on the ground and unsupported is -2. 5
°
,
and the in-flight condition is -3. 0°.
SHOP NOTES:
16-4