AIRPLANE INFORMATION MANUAL
for the
CIRRUS DESIGN SR22
• NOTE •
AT THE TIME OF ISSUANCE, THIS INFORMATION MANUAL
WAS HARMONIZED WITH THE SR22 PILOT'S OPERATING
HANDBOOK REV A7 (P/N 13772-001), AND WILL NOT BE
KEPT CURRENT. THEREFORE, THIS INFORMATION MANUAL
IS FOR REFERENCE ONLY AND CANNOT BE USED
AS A SUBSTITUTE FOR THE OFFICIAL PILOT'S OPERATING
HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT
MANUAL.
P/N 20880-001 June 2007
Information Manual
Copyright © 2003 - All Rights Reserved
Cirrus Design Corporation
4515 Taylor Circle
Duluth, MN 55811
Information Manual 1-1
Cirrus Design Section 1
SR22 General
Section 1
General
Table of Contents
Introduction .....................................................................................1-3
The Airplane....................................................................................1-6
Engine..........................................................................................1-6
Propeller ......................................................................................1-6
Fuel..............................................................................................1-6
Oil ...............................................................................................1-7
Maximum Certificated Weights ....................................................1-7
Cabin and Entry Dimensions .......................................................1-7
Baggage Spaces and Entry Dimensions .....................................1-7
Specific Loadings.........................................................................1-7
Symbols, Abbreviations and Terminology.......................................1-8
General Airspeed Terminology and Symbols ..............................1-8
Meteorological Terminology.........................................................1-9
Engine Power Terminology........................................................1-10
Performance and Flight Planning Terminology..........................1-10
Weight and Balance Terminology..............................................1-11
June 2007
1-2 Information Manual
Section 1 Cirrus Design
General SR22
Intentionally Left Blank
June 2007
Information Manual 1-3
Cirrus Design Section 1
SR22 General
Introduction
This section contains information of general interest to pilots and
owners. You will find the information useful in acquainting yourself with
the airplane, as well as in loading, fueling, sheltering, and handling the
airplane during ground operations. Additionally, this section contains
definitions or explanations of symbols, abbreviations, and terminology
used throughout this handbook.
• Note •
For specific information regarding the organization of this
Handbook, revisions, supplements, and procedures to be
used to obtain revision service for this handbook, refer to the
“Foreword” immediately following the title page
June 2007
1-4 Information Manual
Section 1 Cirrus Design
General SR22
Figure 1-1
78 inches 3-BLADE
198 cm
38.3 ft
11.67 m
10.8 ft
3.29 m
7 inches
18 cm
26.0 ft
7.92 m
SR22_FM01_1371A
8.8 ft
2.70 m
NOTE:
• Wing span includes
position and strobe lights.
• Prop ground clearance at
3400 lb - 7" inches (18 cm).
• Wing Area = 144.9 sq. ft.
Airplane Three View
June 2007
Information Manual 1-5
Cirrus Design Section 1
SR22 General
10.8 ft. (3.30 m)
0.5 ft. (.15 m)
24.8 ft. (7.54 m)
-RADIUS FOR NOSE GEAR 7.0 ft. (2.16 m)
-RADIUS FOR OUTSIDE GEAR
-RADIUS FOR INSIDE GEAR
-RADIUS FOR WING TIP
PARTIAL POWER. ACTUAL TURNING RADIUS MAY VARY AS
MUCH AS THREE FEET.
TURNING RADII ARE CALCULATED USING ONE BRAKE AND
GROUND TURNING CLEARANCE
SR22_FM01_1370
Figure 1-2
Turning Radius
June 2007
1-6 Information Manual
Section 1 Cirrus Design
General SR22
The Airplane
Engine
Number of Engines..............................................................................1
Number of Cylinders............................................................................6
Engine Manufacturer ........................................... Teledyne Continental
Engine Model.......................................................................... IO-550-N
Fuel Metering.................................................................... Fuel Injected
Engine Cooling .....................................................................Air Cooled
　
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