Table 2. Model 182 Static Balance Limits.
CONTROL SURFACE
AILERON
RUDDER
LEFT ELEVATOR
RIGHT ELEVATOR
Table 3. Model 206 Static Balance Limits.
CONTROL SURFACE
AILERON
RUDDER (Landplane)
LEFT ELEVATOR
RIGHT ELEVATOR
CESSNA AIRCRAFT COMPANY
SINGLE ENGINE
STRUCTURAL REPAIR MANUAL
STATIC BALANCE LIMITS APPROVED FOR FLIGHT
CONFIGURATION (INCH-LBS).
0.0 TO +9.64
0.0 TO +6.0
0.0 TO +20.47
0.0 TO +20.47
STATIC BALANCE LIMITS APPROVED FOR FLIGHT
CONFIGURATION (INCH-LBS).
0.0 TO +3.0
-4.0 TO +3.0
0.0 TO +12.1
0.0 TO +12.1
© Cessna Aircraft Company
51-60-00
Page 8
Jun 1/2005