Piper PA-39 Twin Comanche C/R - Page 75

TWINCOMANCHECjR
IT IS THE RESPONSIBILITY OF THE OWNER AND PILOT TQ ASCERTAIN THAT THE
AIRPLANE ALWAYS REMAINS WITHIN THE ALLOWABLE WEIGHT VS. CENTER OFGR.I\\‘IT\r
ENVELOPE WHILE IN FLIGHT.
82 83 84 05
00 B? 00 09
so 91 92
c. G. LOCATION (INCHES AR DATUMI
Moment change due to retracting Landing Gear = +1266 in-I&
1
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ISSUED: November 28.1969
REISSUED: June 1,197O
REVISED: March 17.1971
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REPORT: 1605PARTIIPAGES
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MODEL: P-4-39 i
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