Cirrus Design
Section 6
SR22T
Weight and Balance Data
P/N 13772-005
6-9
P/N 13772-005
6-9
Weight and Balance Loading Form
• Note •
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
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
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 (negative number)
Normally 9 lb at average moment of 1394 (1.4).
9.
Takeoff Condition Weight
Subtract item 8 from item 7
Figure 6-3
Original Issue
