Cirrus DESIGN SR22T - Weight and Balance Loading Form

Cirrus Design Section 6
SR22T Weight and Balance Data
P/N 13772-003 6-9
Weight and Balance Loading Form
• Note •
The Takeoff Condition Weight must not exceed 3400 lb.
The Takeoff Condition Moment must be within the Minimum
Moment to Maximum Moment range at the Takeoff Condition
Weight. (Refer to Moment Limits).
Serial Num: __________________________ Date: ______________
Reg. Num: ___________________________ Initials:_____________
Item Description
Weight
LB
Moment/
1000
1. Basic Empty Weight
Includes unusable fuel & full oil
2. Front Seat Occupants
Pilot & Passenger (total)
3. Rear Seat Occupants
4. Baggage Area
130 lb maximum
5. Zero Fuel Condition Weight
Sub total item 1 thru 4
6. Fuel Loading
92 Gallon @ 6.0 lb/gal. Maximum
7. Ramp Condition Weight
Sub total item 5 and 6
8. Fuel for start, taxi, and run-up
Normally 9 lb at average moment of 1394.
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9. Takeoff Condition Weight
Subtract item 8 from item 7
Figure 6-3
Original Issue