Altitude Limitations: 12,000 Msl; Maximum Weight And Center Of Gravity Limits - THRUSH S2R-H80 Flight Manual

1.4.

ALTITUDE LIMITATIONS: 12,000 MSL

1.5.

MAXIMUM WEIGHT AND CENTER OF GRAVITY LIMITS

Maximum Weight:
Maximum Landing Weight:
Minimum Weight:
C.G. Range:
Forward C.G. Regardless of Weight:
Forward C.G. @ Max. Gross Weight:
Most AFT C.G. @ Max. Gross Weight:
Most AFT C.G. Regardless of Weight:
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.
Hopper rinse tank must be full when rear cockpit is occupied by
a crewmember.
Required forward ballast must be installed when rear cockpit is
occupied by a crewmember.
AFM H8001 SINGLE & DUAL COCKPIT Revision B
FAA APPROVAL DATE: 3/19/2015
S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
NOTE:
DATUM is the leading edge of the wing.
For Single and Dual Cockpit
10,500 lbs.
7600 lbs.
4500 lbs.
NOTE:
NOTE:
NOTE:
6000 lbs. @ 25.0 in. AFT of Datum
10,500 lbs. @ 28.0 in. AFT of Datum
10,500 lbs. @ 30.5 in. AFT of Datum
7600 lbs. @ 31.0 in. AFT of Datum
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