Cirrus SR22T Workbook

SR-Series Workbook ___________________________________________________
Cirrus Aircraft, Duluth, MN
19
6. Weight and Balance
This section will cover Section 6 (Weight and Balance) from your Pilots
Operating Handbook. Answers to all questions will be found in the
appropriate section of the POH, unless otherwise noted.
Aircraft information:
Basic Empty Weight: (22) 2400 lbs (20) 2135 lbs
Moment: (22) 326.563 (20) 301.758
Payload:
Pilot 160 lbs Front Pax 160 lbs
Rear Pax 200 lbs Baggage 130 lbs
Fuel Full Fuel
NOTE: You cannot leave anyone or any baggage behind.
You may use the following table to aid in calculations.
For Moment/1000, refer to loading table in POH.
Description
Weight
Moment/1000
1. Empty Weight
Includes unusable fuel & full oil
2. Front Seat Occupants
Pilot and Passenger
3. Rear Seat Occupants
4. Baggage Area
130 lb maximum
5. Zero Fuel Condition
Sub total items 1 thru 4
6. Fuel Load
(22) 92 Gallon @ 6.0 lb/gal maximum
(20) 56 Gallon @ 6.0 lb/gal maximum
7. Ramp Weight
Sub total items 5 and 6
8. Fuel for Start, taxi, and runup
(22) Normally 9 lb at avg moment of 1394
(20) Normally 6 lb at avg moment of 922.8
9. Takeoff Weight
Subtract Item 8 from item 7

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots