3. Fin should be vertical and in line with center of fuselage.
4. Aileron Travel: 30° up, 15° down, tolerance ±2°.
5. Flap Travel: 10°, 25°, 40° tolerance ±2°.
6. Rudder Travel: 27° right and left, tolerance ±2°.
7. Stabilator Tab Travel: 3° up, 12° down, tolerance ±1°.
Cable tensions for the various controls are as follows:
Rudder: 40 ± 5 lbs. Stabilator: 40+5 lbs.
Ailerons: 40 ± 5 lbs. Stabilator Trim: 10 ± 1 lb.
Flaps: Approx. 10 lbs.
For extreme cases of wing heaviness, the flap on the wing
heavy side may be adjusted down from the zero position as
desired.
The service manual should be consulted for the proper method
of adjusting surface travels.
SERIAL NUMBER PLATE
The serial number plate is located near the stabilator on
the left side of the airplane. Refer to this number for service or
warranty matters.
753 806 49
740118
CHEROKEE"E" SECTION VI
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