Cirrus SR20 Guide de configuration rapide

AIRPLANE INFORMATION MANUAL

for the

CIRRUS DESIGN SR20

Aircraft Serials 2016 and Subsequent with

Cirrus Perspective Avionics System

At the time of issuance, this Information Manual was harmo-

nized with the SR20 Pilot's Operating Handbook September

2011 (P/N 11934-004), and will not be kept current.

Therefore, this Information Manual is for reference only and can-

not be used as a substitute for the official Pilot's Operating

Handbook and FAA Approved Airplane Flight Manual.

Information Manual

P/N 13999-004 September 2011

Cirrus Design Corporation

4515 Taylor Circle

Duluth, MN 55811

P/N 13999-004 Info Manual 1-1

Cirrus Design Section 1

SR20 General

Section 1

General

Table of Contents

Introduction ........................................................................................ 3

The Airplane....................................................................................... 7

Engine............................................................................................. 7

Propeller ......................................................................................... 7

Fuel................................................................................................. 8

Oil .................................................................................................. 8

Maximum Certificated Weights ....................................................... 8

Cabin and Entry Dimensions .......................................................... 8

Baggage Spaces and Entry Dimensions ........................................ 8

Specific Loadings............................................................................ 8

Symbols, Abbreviations and Terminology.......................................... 9

General Airspeed Terminology and Symbols ................................. 9

Meteorological Terminology.......................................................... 10

Engine Power Terminology........................................................... 11

Performance and Flight Planning Terminology............................. 11

Weight and Balance Terminology................................................. 12

September 2011

1-2 P/N 13999-004 Info Manual

Section 1 Cirrus Design

General SR20

September 2011

Intentionally Left Blank

Cirrus Design Section 1

SR20 General

P/N 13999-004 Info Manual 1-3

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, See

“Revising the Handbook” on page 3 of the “Foreword” section.

All liquid volumes referenced in this publication are expressed

in United States Customary Units, e.g., U.S. Gallons.

September 2011

1-4 P/N 13999-004 Info Manual

Section 1 Cirrus Design

General SR20

Figure 1-1

Airplane Three View

74 inches 3-BLADE

188 cm

38.3 ft

11.67 m

9.1 ft

2.8 m

9 inches (minimum)

23 cm (minimum)

26.0 ft

7.92 m

8.9 ft

2.71 m

NOTE:

• Wing span includes

position and strobe lights.

• Prop ground clearance at

3050 lb - 9 inches (23 cm).

• Wing Area = 144.9 sq. ft.

SR20_FM01_2415

September 2011

Cirrus Design Section 1

SR20 General

P/N 13999-004 Info Manual 1-5

Location Length Width Height Volume

Cabin 122” 49.3” 49.7 137 cu ft

Baggage

Compartment

36” 39.8” 38.5” 32 cu ft

Figure 1-2

Airplane Interior Dimensions

39.8"

49.3"

240220

200

180160140120

16.0"

49.7"

25.0"

38.5"

10.5"

33.4" 39.0"

20.0"

33.3"

32.0"

SR22_FM06_1019

100

222

CABIN DOOR

OPENING

BAGGAGE DOOR

OPENING

20.0"

21.0"

5.0"

Station

Fuselage

September 2011

1-6 P/N 13999-004 Info Manual

Section 1 Cirrus Design

General SR20

Figure 1-3

Turning Radius

9.1 ft. (2.77 m)

0.5 ft. (0.15 m)

24.3 ft. (7.41 m)

7.0 ft. (2.16 m)

RADIUS FOR NOSE GEAR

RADIUS FOR OUTSIDE GEAR

RADIUS FOR INSIDE GEAR

RADIUS FOR WING TIP

TURNING RADII ARE CALCULATED USING ONE BRAKE AND

PARTIAL POWER. ACTUAL TURNING RADIUS MAY VARY AS

MUCH AS THREE FEET.

GROUND TURNING CLEARANCE

SR20_FM01_2413

September 2011

Cirrus Design Section 1

SR20 General

P/N 13999-004 Info Manual 1-7

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

Engine Type.................................... Horizontally Opposed, Direct Drive

Horsepower Rating................................................ 200 hp @ 2700 rpm

Propeller

Hartzell

Propeller Type ............................................................. Constant Speed

Two-Blade Propeller:

Model Number...................................................BHC-J2YF-1BF/F7694

Diameter.............................................................76.0” (73.0” Minimum)

Three-Blade Propeller:

Model Number............................................... PHC-J3YF-1MF/F7392-1

Diameter.............................................................74.0” (72.0” Minimum)

Model Number............................................... PHC-J3YF-1RF/F7392-1

Diameter.............................................................74.0” (72.0” Minimum)

September 2011

1-8 P/N 13999-004 Info Manual

Section 1 Cirrus Design

General SR20

Fuel

Total Capacity .............................................58.5 U.S. Gallons (221.0 L)

Total Usable................................................56.0 U.S. Gallons (212.0 L)

Approved Fuel Grades:

100 LL Grade Aviation Fuel (Blue)

100 (Formerly 100/130) Grade Aviation Fuel (Green)

Oil

Oil Capacity (Sump) .............................................8 U.S. Quarts (7.6 L)

Oil Grades:

All Temperatures .............................................SAE 15W-50 or 20W-50

Below 40 °F (4°C).................................................. SAE 30 or 10W-30

Above 40 °F (4°C) ...................................................................SAE 50

Maximum Certificated Weights

Maximum Gross for Takeoff...................................... 3050 lb (1383 Kg)

Maximum Baggage Compartment Loading.................... 130 lb (59 Kg)

Standard Empty Weight.............................................. 2050 lb (930 Kg)

Maximum Useful Load................................................ 1000 lb (454 Kg)

Full Fuel Payload .......................................................... 671 lb (304 Kg)

Cabin and Entry Dimensions

Refer to the preceding figures for dimensions of the cabin interior and

entry door openings.

Baggage Spaces and Entry Dimensions

Refer to the preceding figures for dimensions of the cabin interior and

entry door openings

Specific Loadings

Wing Loading..................................................... 22.2 lb per square foot

Power Loading.................................................................15.0 lb per hp

September 2011

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