CESSNA AIRCRAFT COMPANY
SINGLE ENGINE
STRUCTURAL REPAIR 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 SURFACE
STATIC BALANCE LIMITS APPROVED FOR FLIGHT
CONFIGURATION (INCH-LBS).
AILERON
0.0 TO +3.0
RUDDER (Landplane)
-4.0 TO +3.0
LEFT ELEVATOR
0.0 TO +12.1
RIGHT ELEVATOR
0.0 TO +12.1
51-60-00
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© Cessna Aircraft Company
Jun 1/2005
Summary of Contents for 172 Skyhawk SERIES
Page 11: ...CHAPTER STANDARD PRACTICES STRUCTURES ...
Page 68: ...CHAPTER 52 DOORS ...
Page 74: ...CHAPTER 53 FUSELAGE ...
Page 97: ...CHAPTER 55 STABILIZERS ...
Page 106: ...CHAPTER 56 WINDOWS ...
Page 115: ...CHAPTER 57 WINGS ...
Page 158: ...CHAPTER 71 POWER PLANT ...