S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
AFM H8001 SINGLE & DUAL COCKPIT Revision B Page 6
FAA APPROVAL DATE: 3/19/2015
1.4. ALTITUDE LIMITATIONS: 12,000 MSL
1.5. MAXIMUM WEIGHT AND CENTER OF GRAVITY LIMITS
For Single and Dual Cockpit
Maximum Weight: 10,500 lbs.
Maximum Landing Weight: 7600 lbs.
Minimum Weight: 4500 lbs.
C.G. Range:
Forward C.G. Regardless of Weight:
6000 lbs. @ 25.0 in. AFT of Datum
Forward C.G. @ Max. Gross Weight:
10,500 lbs. @ 28.0 in. AFT of Datum
Most AFT C.G. @ Max. Gross Weight:
10,500 lbs. @ 30.5 in. AFT of Datum
Most AFT C.G. Regardless of Weight:
7600 lbs. @ 31.0 in. AFT of Datum
NOTE:
DATUM is the leading edge of the wing.
NOTE:
It is the responsibility of the airplane owner and the pilot to insure
that the airplane is properly loaded. See the Weight & Balance
Sheet for loading information.
NOTE:
Hopper rinse tank must be full when rear cockpit is occupied by
a crewmember.
NOTE:
Required forward ballast must be installed when rear cockpit is
occupied by a crewmember.
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