AIRPLANE INFORMATION MANUAL
for the
CIRRUS DESIGN SR20
A l l - E l e c t r i c S R 2 0
A i r c r a f t S e r i a l s 1 2 6 8 a n d S u b s e q u e n t
• NOTE •
At the time of issuance, this Information Manual was
harmonized with the SR20 Pilot's Operating Handbook Rev
A9 (P/N 11934-003), 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.
Information Manual
P/N 13999-003 March 2010
Copyright © 2001 - All Rights Reserved
Cirrus Design Corporation
4515 Taylor Circle
Duluth, MN 55811
Information Manual 1-1
Cirrus Design Section 1
SR20 General
Section 1
General
Table of Contents
Introduction .....................................................................................1-3
The Airplane....................................................................................1-6
Engine..........................................................................................1-6
Propeller ......................................................................................1-6
Fuel..............................................................................................1-7
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
March 2010
1-2 Information Manual
Section 1 Cirrus Design
General SR20
Intentionally Left Blank
March 2010
Information Manual 1-3
Cirrus Design Section 1
SR20 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
March 2010
1-4 Information Manual
Section 1 Cirrus Design
General SR20
Figure 1-1
76" 2-BLADE
74" 3-BLADE
35.5'
11.0'
9.2'
7"
26.0'
SR20_FM01_1004A
NOTE:
• Wing span includes
position and strobe lights.
• Prop ground clearance at
3000 lb - 7" (2 blade),
8" (3 blade).
• Wing Area = 135.2 sq. ft.
Airplane Three View
March 2010
Information Manual 1-5
Cirrus Design Section 1
SR20 General
23' 11"
9' 11"
SR20_FM01_1002
GROUND TURNING CLEARANCE
TURNING RADII ARE CALCULATED USING ONE BRAKE AND
PARTIAL POWER. ACTUAL TURNING RADIUS MAY VARY AS
MUCH AS THREE FEET.
-RADIUS FOR WING TIP
-RADIUS FOR INSIDE GEAR 6"
-RADIUS FOR OUTSIDE GEAR
-RADIUS FOR NOSE GEAR
12' 2"
Figure 1-2
Turning Radius
March 2010
1-6 Information Manual
Section 1 Cirrus Design
General SR20
The Airplane
Engine
Number of Engines..............................................................................1
Number of Cylinders............................................................................6
Engine Manufacturer ........................................... Teledyne Continental
Engine Model........................................................................IO-360-ES
Fuel Metering.................................................................... Fuel Injected
Engine Cooling .....................................................................Air Cooled
　
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