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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 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA
