Cirrus DESIGN SR22T User Manual

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.
––
9. Takeoff Condition Weight
Subtract item 8 from item 7
Figure 6-3
Original Issue

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches