List of Effective Pages List of Effective Pages Cont. Page Status Page Status Page Status 4 2. Reissue A Reissue A 7 6. Reissue A 4 2. 4 Reissue A Reissue A 7 6. Reissue A 4 2. 5 Reissue A. Cirrus Design Pilots Operating Handbook SR2. List of Effective Pages List of Effective Pages Cont. Page Status Page Status Page Status 8 2. Reissue A 8 2. 3 Reissue A 8 2. Reissue A 8 2. 5 Reissue A 8 2. Reissue A 8 2. 7 Reissue A 8 2. Cirrus Design Pilots Operating Handbook SR2. List of Effective Pages List of Effective Pages Cont. Page Status Page Status Page Status Intentionally Left Blank PN 1. Reissue A. Foreword Foreword This Pilots Operating Handbook POH or Handbook has been prepared by Cirrus Design Corporation to familiarize operators with the aircraft. Read this Handbook carefully. It provides operational procedures that will assure the operator obtains the performance published in the manual, data designed to allow the most efficient use of the airplane, and basic information for maintaining the airplane in a like new. Front Matter Cirrus Design Foreword SR2. The Handbook This Pilots Operating Handbook has been prepared using GAMA Specification 1 for Pilots Operating Handbook, Revision 2, dated 1. October 1. 99. 6 as the content model and format guide. However, some deviations from this specification were made for clarity. The Handbook is presented in loose leaf form for ease in inserting revisions and is sized for convenient storage. Original issue pages will be identified by the words Original Issue at this location. In the event that the majority of pages in the Handbook are revised, Cirrus may determine that it is more effective to reissue the Handbook. Reissued pages will be identified by the word Reissue. Design Supplements produced for this airplane. The Log of Supplements page can be utilized as a Table of Contents for Section 9. If the airplane is modified at a non Cirrus Design facility through an STC or other approval method, it is the owners responsibility to ensure that the proper supplement, if applicable, is installed in the Handbook and that the supplement is properly recorded on the Log of. Cirrus Design Front Matter SR2. Foreword Retention of Data In the event a new title page is issued, the weight and balance data changes, equipment list changes, or the Log of Supplements is replaced, the owner must ensure that all information applicable to the airplane is transferred to the new pages and the aircraft records are current. Front Matter Cirrus Design Foreword SR2. Intentionally Left Blank Front Matter 6 PN 1. Reissue A. Cirrus Design Section 1 SR2. General Section 1 General Table of Contents Introduction. The Airplane. Engine. Propeller. Fuel. 8 Oil. Maximum Certificated Weights. Cabin and Entry Dimensions. Baggage Spaces and Entry Dimensions. Specific Loadings. Section 1 Cirrus Design General SR2. Intentionally Left Blank PN 1. Reissue A. Cirrus Design Section 1 SR2. 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. Section 1 Cirrus Design General SR2. NOTE Wing span includes position and strobe lights. Prop ground clearance at 3. Cirrus Design Section 1 SR2. General 4. 9. 3 3. Fuselage Station 4. CABIN DOOR BAGGAGE DOOR OPENING OPENING SR2. FM0. 11. 01. 9A Location Length Width Height Volume 1. Cabin 3. 6. Section 1 Cirrus Design General SR2. GROUND TURNING CLEARANCE 2. RADIUS FOR WING TIP 7. RADIUS FOR NOSE GEAR 0. RADIUS FOR INSIDE GEAR 9. RADIUS FOR OUTSIDE GEAR TURNING RADII ARE CALCULATED USING ONE BRAKE AND PARTIAL POWER. Cirrus Design Section 1 SR2. General The Airplane Engine Number of Engines. Number of Cylinders. Engine Manufacturer. Teledyne Continental Engine Model. IO 5. 50 N Fuel Metering. Fuel Injected Engine Cooling. Air Cooled Engine Type. Horizontally Opposed, Direct Drive Horsepower Rating. Section 1 Cirrus Design General SR2. Fuel Total Capacity. U. S. Gallons 3. L Total Usable. U. S. Gallons 3. L Approved Fuel Grades 1. LL Grade Aviation Fuel Blue 1. Formerly 1. 001. Grade Aviation Fuel Green Oil Capacity Sump. U. S. Quarts 7. 6 L Oil Grades All Temperatures. Cirrus Design Section 1 SR2. General Symbols, Abbreviations and Terminology General Airspeed Terminology and Symbols KCAS Knots Calibrated Airspeed is the indicated airspeed corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level. Section 1 Cirrus Design General SR2. Stalling Speed is the minimum steady flight speed at which aircraft controllable landing configuration 1. Best Angle of Climb Speed is the speed at which the airplane will obtain the highest altitude in a given horizontal distance. Cirrus Design Section 1 SR2. General Pressure Altitude is the altitude read from the altimeter when the altimeters barometric adjustment has been set to 2. Hg 1. 01. 3 mb corrected for position and instrument error. In this Handbook, altimeter instrument errors are assumed to be zero. Section 1 Cirrus Design General SR2. NMPG Nautical Miles Per Gallon is the distance in nautical miles which can be expected per gallon of fuel consumed at a specific engine power setting andor flight configuration. Unusable Fuel is the quantity of fuel that cannot be safely used in flight. Cirrus Design Section 1 SR2. General Station is a location along the airplane fuselage measured in inches from the reference datum and expressed as a number. For example A point 1. Fuselage Station 1. FS 1. 23. Section 1 Cirrus Design General SR2. Intentionally Left Blank 1 1. PN 1. 37. 72 0. Reissue A. Environmental Conditions. Nesterj Nes Emulator 1 11 PSP there. Maximum Occupancy. Systems and Equipment Limits. Cirrus Perspective Integrated Avionics System. L 3 Skywatch Traffic Advisory System. L 3 Stormscope Weather Information System. Max Viz Enhanced Vision System Optional. Air Conditioning System Optional. Section 2 Cirrus Design Limitations SR2. Smoking. Placards. PN 1. 37. 72 0. Reissue A. Cirrus Design Section 2 SR2. Limitations Introduction The limitations included in this Section of the Pilots Operating Handbook POH are approved by the Federal Aviation Administration. This section provides operating limitations, instrument markings and basic placards required by regulation and necessary for the safe operation of the aircraft and its standard systems and equipment. Section 2 Cirrus Design Limitations SR2. Airspeed Limitations The indicated airspeeds in the following table are based on Section 5, Airspeed Calibration Normal Static Source Table. When using the alternate static source, allow for the airspeed calibration variations between the normal and alternate static sources. Cirrus Design Section 2 SR2. Limitations Airspeed Indicator Markings The airspeed indicator markings are based on Section 5, Airspeed Calibration Normal Static Source Table. Stec 50 Autopilot Installation Manual© 2017