Weight And Balance Loading Form; Moment Limits - Cirrus SR22 Pilot's Operating Handbook And Flight Manual

Cirrus Design
SR22

Weight and Balance Loading Form

The Takeoff Condition Weight must not exceed 3600 lb.
The Takeoff Condition Moment must be within the Minimum
Moment to Maximum Moment range at the Takeoff Condition
Weight. (Refer to
Serial Num: __________________________ Date: ______________
Reg. Num: ___________________________ Initials:_____________
Item Description
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
3400 lb maximum
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.
9. Takeoff Condition Weight
Subtract item 8 from item 7
P/N 13772-004 P/N 13772-004
Original Issue
• Note •
Moment Limits).
Figure 6-3
Section 6
Weight and Balance Data
Weight Moment/
LB 1000
6-9 6-9