Cessna 206 - Page 51

CESSNA AIRCRAFT
COMPANY
SINGLE ENGINE
STRUCTURAL REPA
IR MANUAL
Table 2. Model 182 Static Balance Limits.
CONTROL SURFACE STATIC BALANCE LIMITS APPROVED FOR FLIGHT
CONFIGURATION (INCH-LBS).
AILERON 0.0 TO +9.64
RUDDER
0.0 TO +6.0
LEFT ELEVATOR 0.0 TO +20.47
RIGHT ELEVATOR 0.0 TO +20.47
Table 3. Model 206 Static Balance Limits.
CONTROL SUR
FACE
STATIC BALA
NCE LIMITS APPROVED FOR FLIGHT
CONFIGURATION (INCH-LBS).
AILERON 0.0 TO +3.0
RUDDER (La
ndplane)
-4.0 TO +3.
0
LEFT ELEVATOR 0.0 TO +12.1
RIGHT ELEVATOR 0.0 TO +12.1
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© Cessna Aircraft Company Jun 1/2005