FAA APPROVED AIRPLANE FLIGHT MANUAL

8-17 Original Issue 8-18 Original Issue 8-19 Original Issue 8-20 Original Issue 8-21 Original Issue 8-22 Original Issue 8-23 Original Issue 8-24 Original Issue 8-25 Original Issue 8-26 Original Issue 8-27 Original Issue 8-28 Original Issue 8-29 Original Issue 8-30 Original Issue 8-31 Original Issue 8-32 Original Issue 9-1 Original Issue 9-2 Original Issue 10-1 Original Issue 10-2 Original Issue 10-3 Original Issue 10-4 Original Issue 10-5 Original Issue 10-6 Original Issue 10-7 Original Issue 10-8 Original Issue 01 Aug 2023 Original Issue CIRRUS FRONTMATTER SR20 FOREWORD P/N 44763-001 NOT FAA APPROVED Frontmatter-1 Foreword This Airplane Flight Manual (AFM) has been prepared by Cirrus to famil- iarize operators with the aircraft. Read this AFM carefully. It provides oper- ational procedures that will ensure the operator obtains the performance published in the manual, data designed to allow the most efficient and safe use of the airplane, and basic information to assist in maintaining the airplane in airworthy condition. • N OTE • All limitations, procedures, maintenance & servicing require- ments, and performance data contained in this AFM are manda- tory for compliance with FAA operating rules and for continued airworthiness of the airplane. This AFM includes the material required to be furnished to the pilot by the Code of Federal Regulations (CFRs) and additional information provided by Cirrus and constitutes the FAA Approved Airplane Flight Manual for the aircraft. The Airplane Flight Manual This AFM has been prepared using GAMA Specification #1 for Airplane Flight Manual, Revision 2, dated 18 October 1996 as the content model and format guide. However, some deviations from this specification were made for clarity. The AFM is presented in loose-leaf form for ease in inserting revisions and is sized for convenient storage. Tabbed dividers throughout the AFM allow quick reference to each section. Logical and convenient Tables of Contents are located at the beginning of each section to aid in locating specific data within that section. The AFM is divided into ten sections as follows: Section 1 ........................................................................................ General Section 2 ..................................................................................Limitations Section 3 ..............................................................Emergency Procedures Section 3A ............................................................ Abnormal Procedures Section 4 ....................................................................Normal Procedures Section 5 ...................................................................... Performance Data Section 6 ...................................................................Weight and Balance Section 7 .................................................................. Systems Description Section 8 .............................................................Handling and Servicing Section 9 ................................................................... Log of Supplements Section 10 ................................................................... Safety Information Original Issue 01 Aug 2023 FRONTMATTER CIRRUS FOREWORD SR20 Frontmatter-2 NOT FAA APPROVED P/N 44763-001 The data presented in this AFM is the result of extensive flight tests and is approved by the Federal Aviation Administration. However, as new proce- dures or performance data are developed, the AFM will be revised. • N OTE • It is the responsibility of the owner to ensure that the Airplane Flight Manual is current at all times. Therefore, it is very important that all revisions be properly incorporated into this AFM as soon as they become available. Revising the Airplane Flight Manual Two types of revisions may be issued for this manual: Temporary and Numbered. Temporary revisions are printed on yellow paper, normally cover only one topic or procedure, and are issued to provide safety related information in a timely manner. All the information needed to properly file a temporary revision is included on the revision itself. Typically, a temporary revision is superseded and replaced by the next numbered revision. Numbered revisions are printed on white paper, normally cover several subjects, and are issued as general updates to the AFM. Each numbered revision includes an “Instruction Sheet”, a “List of Effective Pages”, and a “Revision Highlights” page. The “Instruction Sheet” is intended to assist the manual holder in removing superseded pages and inserting new or superseding pages. The “List of Effective Pages” shows the issue or revision status of all pages in the AFM. The “Revision Highlights” page gives a brief description of changes made to each page in the current revision. Identifying Revised Material Each page in the AFM has the issue date at the lower inside corner opposite the page number and the revision level under the part number. Issue dates will correspond to the issue dates of the Original Issue, any revisions, or reissues on the List of Effective Pages. The Original Issue and its issue date will be listed on the List of Effective Pages. In the event that the majority of pages in the AFM are revised, Cirrus may determine that it is more effective to reissue the AFM. Reissues will be identified by the word “Reissue” followed by a letter indicating the reissue level; for example, “Reissue A” on the List of Effective Pages along with its issue date. Revisions will be identi- fied by the word “Revision” followed by the revision number on the List of Effective Pages; for example, “Revision 2” (Original Issue, Revision 2) or “Revision B1” (Reissue B, Revision 1). Revised material on a page can be identified by a change bar located at the outside page margin. 01 Aug 2023 Original Issue CIRRUS FRONTMATTER SR20 SUPPLEMENTS P/N 44763-001 NOT FAA APPROVED Frontmatter-3 Revisions to the Airplane Flight Manual AFM revisions, temporary revisions, and supplements can be downloaded from Cirrus at www.cirrusaircraft.com, or from the Authorized Service Center website. Paper copies of AFM revisions and supplements can be purchased from Cirrus Connection at www.cirrusconnection.com. Supplements The Supplements section (Section 9) of this AFM contains FAA Approved Supplements necessary to safely and efficiently operate the airplane when equipped with optional equipment not provided with the standard airplane or not included in the AFM. Supplements are essentially “mini-manuals” and may contain data corresponding to most sections of the AFM. Data in a supplement either adds to, supersedes, or replaces similar data in the basic AFM. Section 9 includes a “Log of Supplements” page preceding all Cirrus 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 facility through an STC or other approval method, it is the owner’s responsibility to ensure that the proper supple- ment, if applicable, is installed in the AFM and that the supplement is prop- erly recorded on the “Log of Supplements” page. FAA Approved AFM Supplements must be in the airplane for flight oper- ations when the subject optional equipment is installed or the special oper- ations are to be performed. Retention of Data In the event a new title page is issued, the weight and balance data changes, the equipment list changes, or the “Log of Supplements” is replaced, the owner must ensure that all information applicable to the airplane is trans- ferred to the new pages and the aircraft records are current. It is not a requirement that owners retain information, such as supplements, that is not applicable to their airplane. In the event a new AFM is purchased, the owner must ensure that all infor- mation applicable to the airplane is transferred to the new AFM and the aircraft records are current. Original Issue 01 Aug 2023 FRONTMATTER CIRRUS WARNINGS, C AUTIONS, AND NOTES SR20 Frontmatter-4 NOT FAA APPROVED P/N 44763-001 Warnings, Cautions, and Notes Warnings, Cautions, and Notes are used throughout this AFM to focus attention on special conditions or procedures as follows: • WARNING • Warnings are used to call attention to operating procedures which, if not strictly observed, may result in personal injury or loss of life. • CAUTION • Cautions are used to call attention to operating procedures which, if not strictly observed, may result in damage to equipment. • N OTE • Notes are used to highlight specific operating conditions or steps of a procedure. Airplane Serial Number Effectivity For aircraft serial numbers with an alphabetical suffix, the letter designa- tion should be ignored when reading effectivity notes in service and oper- ating documents. For example, "2491H" is the same as "2491" when referencing effectivity to determine applicable operation for this aircraft. 01 Aug 2023 Original Issue P/N 44763-001 NOT FAA APPROVED 1-1 CIRRUS S ECTION 1: G ENERAL SR20 Section 1: General Table of Contents Introduction.......................................................................................... 3 The Airplane ........................................................................................ 7 Engine ............................................................................................... 7 Propeller ............................................................................................ 7 Hartzell ............................................................................................ 7 Fuel ................................................................................................... 7 Approved Fuel Grades .................................................................... 7 Oil ...................................................................................................... 8 Maximum Certificated Weights.......................................................... 8 Specific Loadings .............................................................................. 8 Noise Characteristics ........................................................................ 8 Terminology....................................................................................... 9 Original Issue 01 Aug 2023 S ECTION 1: GENERAL CIRRUS SR20 1-2 NOT FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue Intentionally Left Blank CIRRUS S ECTION 1: G ENERAL SR20 I NTRODUCTION P/N 44763-001 NOT FAA APPROVED 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 manual. • N OTE • For specific information regarding the organization of this Hand- book, revisions, supplements, and procedures to be used to obtain publications, see the “Foreword” section. All liquid volumes referenced in this publication are expressed in United States Customary Units, e.g., U.S. Gallons. Original Issue 01 Aug 2023 S ECTION 1: GENERAL CIRRUS I NTRODUCTION SR20 1-4 NOT FAA APPROVED P/N 44763-001 Figure 1-1: Airplane Three View 74 inches 3-BLADE 188 cm 38.3 ft 11.67 m 9.1 ft 2.8 m 26.0 ft 7.92 m 8.9 ft 2.71 m SR20_FM01_5662 01 Aug 2023 Original Issue CIRRUS S ECTION 1: G ENERAL SR20 I NTRODUCTION P/N 44763-001 NOT FAA APPROVED 1-5 Figure 1-2: Airplane Interior Dimensions Location Length Width Height Volume Cabin 122” 49.3” 49.7” 137 cu ft Baggage Compartment 36” 39.8” 38.5” 32 cu ft 20.5" 39.8" 49.3" 240 220 200 180 160 140 120 16.0" 49.7" 27.0" 38.5" FS 10.5" 33.4" 39.0" 20.0" 33.3" 32.0" SR20_FM01_5632 100 222 CABIN DOOR OPENING BAGGAGE DOOR OPENING 20.0" 5.0" Station Fuselage Original Issue 01 Aug 2023 S ECTION 1: GENERAL CIRRUS I NTRODUCTION SR20 1-6 NOT FAA APPROVED P/N 44763-001 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_5398 01 Aug 2023 Original Issue CIRRUS S ECTION 1: G ENERAL SR20 T HE A IRPLANE P/N 44763-001 NOT FAA APPROVED 1-7 The Airplane Engine Number of Engines ............................................................................................ 1 Number of Cylinders ......................................................................................... 4 Engine Manufacturer ...........................................................Lycoming Engines Engine Model .................................................................................IO-390-C3B6 Fuel Metering ..................................................................................Fuel Injected Engine Cooling .................................................................................. Air Cooled Engine Type........................................... .Horizontally Opposed, Direct Drive Horsepower Rating.......................................................... 215 HP @ 2700 RPM Propeller Hartzell Propeller Type............................................................................Constant Speed Three-Blade Propeller, Metal (Standard): Model Number......................................................... HC-E3YR-1RF/F7392S-1 Diameter ....................................................................... 74.0” (73.0” Minimum) Refer to Section 2, Powerplant Limitations for servicing limitations. Three-Blade Propeller, Composite (Optional): Model Number............................................................... 3C1-R919A1/76C03-2 Diameter .................................................................................... 74.0” Minimum 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) Original Issue 01 Aug 2023 S ECTION 1: GENERAL CIRRUS THE A IRPLANE SR20 1-8 NOT FAA APPROVED P/N 44763-001 Oil Oil Capacity (Sump)......................................................... 7 U.S. Quarts (6.6 L) Refer to Section 2, Powerplant Limitations, for approved oil grades. Maximum Certificated Weights Maximum Takeoff Gross Weight.........................................3150 lb (1429 kg) Maximum Baggage Compartment Loading.............................. 130 lb (59 kg) Specific Loadings Wing Loading................................................................. 21.7 lb per square foot Power Loading..............................................................................14.7 lb per HP Noise Characteristics The certificated noise levels for the aircraft established in accordance with CFR 36 Appendix G are: No determination has been made by the Federal Aviation Administration that the noise levels of this airplane are or should be acceptable or unaccept- able for operation at, into, or out of, any airport. The above noise levels were established at 3150 pounds takeoff weight and 2700 RPM. Configuration Actual Maximum Allowable Hartzell 3-blade Propeller, HC-E3YR-1RF/F7392S-1, Metal (Standard) 82.9 dB(A) 88.0 dB(A) Hartzell 3-blade Propeller, 3C1-R919A1/76C03-2, Composite (Optional) 81.7 dB(A) 88.0 dB(A) 01 Aug 2023 Original Issue CIRRUS S ECTION 1: G ENERAL SR20 T HE A IRPLANE P/N 44763-001 NOT FAA APPROVED 1-9 Terminology Table 1: General Airspeed Terminology General Airspeed Terminology Terminology Definition KCAS Knots Calibrated Airspeed is the indicated airspeed corrected for position and instrument error. KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator. The IAS values published in this AFM assume no instrument error. KTAS Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature. VG Best Glide Speed is the speed at which the greatest flight distance is attained per unit of altitude lost with power off. VO Operating Maneuvering Speed is the maximum speed at which application of full control movement will not overstress the airplane. V FE_50% Maximum Flap Extended Speed (50%) is the highest speed permissible with wing flaps extended to the 50% position (typical of takeoff and approach) V FE_100% Maximum Flap Extended Speed (100%) is the highest speed permissible with wing flaps extended to the 100% position (typical of landing). V NO Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, and then only with caution. V NE Never Exceed Speed is the speed that may not be exceeded at any time. V PD Maximum Demonstrated Parachute Deployment Speed is the maximum speed at which parachute deployment has been demonstrated. Original Issue 01 Aug 2023 S ECTION 1: GENERAL CIRRUS THE A IRPLANE SR20 1-10 NOT FAA APPROVED P/N 44763-001 Table 2: Meteorological Terminology V REF Landing reference speed or threshold crossing speed. VS Stalling Speed is the minimum steady flight speed at which the aircraft is controllable. VS0 Stalling Speed is the minimum steady flight speed at which the aircraft is controllable in the landing configuration (100% flaps) at the most unfavorable weight and balance. V X Best Angle of Climb Speed is the speed at which the airplane will obtain the highest altitude in a given horizontal distance. The best angle-of-climb speed normally increases slightly with altitude. V Y Best Rate of Climb Speed is the speed at which the airplane will obtain the maximum increase in altitude per unit of time. The best rate-of-climb speed decreases slightly with altitude. Meteorological Terminology Terminology Definition IMC Instrument Meteorological Conditions are meteorological conditions expressed in terms of visibility, distance from cloud, and ceiling less than the minima for visual flight defined in 14 CFR 91.155. ISA International Standard Atmosphere (standard day) is an atmosphere where (1) the air is a dry perfect gas, (2) the temperature at sea level is 15 °C, (3) the pressure at sea level is 29.92 in.Hg (1013.2 millibars). MSL Mean Sea Level is the average height of the surface of the sea for all stages of tide. In this AFM, altitude given as MSL is the altitude above the mean sea level. It is the altitude read from the altimeter when the altimeter’s barometric adjustment has been set to the altimeter setting obtained from ground meteorological sources. General Airspeed Terminology (Continued) Terminology Definition 01 Aug 2023 Original Issue CIRRUS S ECTION 1: G ENERAL SR20 T HE A IRPLANE P/N 44763-001 NOT FAA APPROVED 1-11 Table 3: Engine Power Terminology OAT Outside Air Temperature is the free air static temperature obtained from in-flight temperature indications or from ground meteorological sources. It is expressed in either °C or °F. PA Pressure Altitude is the altitude read from the altimeter when the altimeter’s barometric adjustment has been set to 29.92 in.Hg (1013.21 mb) corrected for position and instrument error. In this Handbook, altimeter instrument errors are assumed to be zero. Standard Temperature Standard Temperature is the temperature that would be found at a given pressure altitude in the standard atmosphere. It is 59 °F (15 °C) at sea level pressure altitude and decreases approximately 4 °F (2 °C) for each 1000 feet of altitude increase. See ISA definition. Engine Power Terminology Terminology Definition HP Horsepower is the power developed by the engine. MCP Maximum Continuous Power is the maximum power that can be used continuously. MAP Manifold Pressure is the pressure measured in the engine’s induction system expressed as in.Hg. RPM Revolutions Per Minute is engine rotational speed. Static RPM Static RPM is RPM attained during a full-throttle engine runup when the airplane is on the ground and stationary. Meteorological Terminology (Continued) Terminology Definition Original Issue 01 Aug 2023 S ECTION 1: GENERAL CIRRUS THE A IRPLANE SR20 1-12 NOT FAA APPROVED P/N 44763-001 Table 4: Performance and Flight Planning Terminology Performance and Flight Planning Terminology Terminology Definition g One “g” is a quantity of acceleration equal to that of earth’s gravity. Demonstrated Crosswind Velocity Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane during taxi, takeoff, and landing was demonstrated during certification testing. Demonstrated crosswind is not considered to be limiting. Service Ceiling Service Ceiling is the maximum altitude at which the aircraft at maximum weight has the capability of climbing at a rate of 100 feet per minute. GPH Gallons Per Hour is the amount of fuel (in gallons) consumed by the aircraft per hour. 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 and/or flight configuration. Unusable Fuel Unusable Fuel is the quantity of fuel that cannot be safely used in flight. Usable Fuel Usable Fuel is the fuel available for flight planning. 01 Aug 2023 Original Issue CIRRUS S ECTION 1: G ENERAL SR20 T HE A IRPLANE P/N 44763-001 NOT FAA APPROVED 1-13 Table 5: Weight and Balance Terminology Weight and Balance Terminology Terminology Definition Reference Datum Reference Datum is an imaginary vertical plane from which all horizontal distances are measured for balance purposes. Fuselage Station Fuselage Station (FS) is a location along the airplane fuselage measured in inches from the reference datum and expressed as a number. For example: A point 123 inches aft of the reference datum is FS 123. CG Center of Gravity is the point at which an airplane would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane. Arm Arm is the horizontal distance from the reference datum to the center of gravity (CG) of an item. The airplane’s arm is obtained by adding the airplane’s individual moments and dividing the sum by the total weight. Moment Moment is the product of the weight of an item multiplied by its arm. Basic Empty Weight Basic Empty Weight is the actual weight of the airplane including all operating equipment that has a fixed location in the airplane. The basic empty weight includes the weight of unusable fuel and full oil. MAC Mean Aerodynamic Chord is the chord drawn through the centroid of the wing plan area. LEMAC Leading Edge of Mean Aerodynamic Chord is the forward edge of MAC given in inches aft of the reference datum (fuselage station). Maximum Gross Weight Maximum Gross Weight is the maximum permissible weight of the airplane and its contents as listed in the aircraft specifications. Maximum Takeoff Weight Maximum Takeoff Weight is the maximum weight approved for the start of the takeoff run. Original Issue 01 Aug 2023 S ECTION 1: GENERAL CIRRUS THE A IRPLANE SR20 1-14 NOT FAA APPROVED P/N 44763-001 Useful Load Useful Load is the basic empty weight subtracted from the maximum takeoff weight. It is the maximum allowable combined weight of pilot, passengers, fuel, and baggage. Weight and Balance Terminology (Continued) Terminology Definition 01 Aug 2023 Original Issue P/N 44763-001 FAA APPROVED 2-1 CIRRUS S ECTION 2: L IMITATIONS SR20 Section 2: Limitations Table of Contents Introduction.......................................................................................... 3 Certification Status ............................................................................ 3 Taxiing, Takeoff, and Landing Limitations........................................... 4 Operational Limits ............................................................................. 4 Airspeed Limitations ............................................................................ 4 Operating Speeds ............................................................................. 4 Flap Speeds ...................................................................................... 4 Airspeed Indicator Markings................................................................ 5 Powerplant Limitations ........................................................................ 6 Engine ............................................................................................... 6 Fuel .................................................................................................. 6 Oil ...................................................................................................... 6 Propeller ............................................................................................ 8 Hartzell ............................................................................................ 8 Engine Instrument Markings & Annunciations................................... 9 Powerplant ...................................................................................... 9 Fuel ................................................................................................. 10 Electrical.......................................................................................... 10 Weight Limits..................................................................................... 11 Center of Gravity Limits..................................................................... 11 Maneuver Limits ................................................................................ 13 Flight Load Factor Limits ................................................................... 13 Minimum Crew Requirements ........................................................... 13 Kinds of Operation............................................................................. 13 Kinds of Operation Equipment List.................................................. 13 Maximum Operating Altitude Limits................................................... 17 Outside Air Temperature Limit .......................................................... 17 Takeoff Temperature....................................................................... 17 Maximum Occupancy........................................................................ 18 Serials w/ 2+1 Rear Seat................................................................. 18 Child Restraint System Limits........................................................ 18 Serials w/ Observer’s Seat .............................................................. 18 Child Restraint System Limits........................................................ 19 Serials w/o 2+1 Rear Seat or Observer’s Seat................................ 19 Systems and Equipment Limits ......................................................... 20 Flap Limitations ............................................................................... 20 Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS SR20 2-2 FAA APPROVED P/N 44763-001 Icing ................................................................................................. 20 Autopilot........................................................................................... 20 Minimum Autopilot Speed.............................................................. 20 Maximum Autopilot Speed............................................................. 20 Minimum-Use-Height ..................................................................... 20 Engagement Limits ........................................................................ 21 Navigation and Communication Equipment .................................... 21 Attitude and Heading Reference System (AHRS) ......................... 21 Cirrus Perspective Touch+ Integrated Avionics System.................. 22 Traffic Avoidance System (TAS) ..................................................... 24 Navigation Map and Weather Map ..................................................24 Safe Taxi, Taxiway Routing and Chartview.....................................24 Terrain Proximity Map ..................................................................... 24 Synthetic Vision System (SVS) ....................................................... 25 Terrain Awareness Warning System (Optional) .............................. 25 Max Viz Enhanced Vision System (Optional) ..................................25 Stormscope Weather Information System (Optional) ...................... 25 Air Conditioning System ................................................................. 26 Inflatable Restraint System.............................................................. 26 Cirrus Airframe Parachute System (CAPS).....................................26 Other Limitations ...............................................................................26 Smoking........................................................................................... 26 Crew Communication ...................................................................... 26 Placards............................................................................................. 27 Exterior Placards ............................................................................. 27 Interior Placards .............................................................................. 29 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 I NTRODUCTION P/N 44763-001 FAA APPROVED 2-3 Introduction The limitations included in this Section of the Airplane Flight Manual (AFM) 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. • Note • Compliance with the operating limitations in this section and in Section 9 is required by the Code of Federal Regulations. For installed equipment described in an FAA Approved AFM Supplement, refer to Section 9: Log of Supplements of this AFM for amended operating limits. Certification Status The aircraft is certificated under the requirements of 14 CFR, Part 23, Airworthiness Standards: Normal Category, Part 36, Noise Standards, and Special Conditions prescribed by the Administrator. Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS TAXIING , TAKEOFF, AND L ANDING L IMITATIONS SR20 2-4 FAA APPROVED P/N 44763-001 Taxiing, Takeoff, and Landing Limitations Operational Limits This airplane may be operated on any smooth runway surface. Maximum Tailwind for Takeoff and Landing................................... 10 knots Airspeed Limitations Operating Speeds Operating Maneuvering Speed (V O ) ................................................ 133 KIAS Never Exceed Speed (VNE ) ................................................................ 201 KIAS Max. Structural Cruising Speed (VNO )............................................. 164 KIAS Flap Speeds Maximum flap extended speed, 50% (V FE_50% ).............................. 150 KIAS Maximum flap extended speed, 100% (VFE_100% ).......................... 110 KIAS 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 A IRSPEED I NDICATOR M ARKINGS P/N 44763-001 FAA APPROVED 2-5 Airspeed Indicator Markings The airspeed indicator markings are based on Section 5, Airspeed Calibra- tion - Normal Static Source Table. When using the alternate static source, allow for the airspeed calibration variations between the normal and alter- nate static sources. Marking Value (KIAS) Remarks White Arc 62 to 110 Full Flap Operating Range. Lower limit is the most adverse stall speed in the landing configuration. Upper limit is the maximum speed permissible with flaps extended. Green Arc 71 to 164 Normal Operating Range. Lower limit is the maximum weight stall at most forward C.G. with flaps retracted. Upper limit is the maximum structural cruising speed (V NO ). Yellow Arc 164 to 201 Caution Range. Operations must be conducted with caution and only in smooth air. Red Arc 201 Never Exceed Speed (V NE). Maximum speed for all operations. Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS POWERPLANT L IMITATIONS SR20 2-6 FAA APPROVED P/N 44763-001 Powerplant Limitations Engine Lycoming Engines......................................................................... IO-390-C3B6 Power Rating .................................................................... 215 HP @ 2700 RPM Maximum RPM ..................................................................................2700 RPM • N OTE • Due to the mechanical design of the propeller governor, it is normal for the engine to temporarily exceed 2700 RPM during some phases of flight. If necessary, a slight reduction in throttle setting will decrease the RPM to keep the engine operating at or below 2700 RPM. Power Lever Movement ...........GREATER THAN 3 SECONDS FOR FULL RANGE • N OTE • Abrupt full range power lever movement can result in engine damage. Idle to maximum power movements of the power lever should be made slowly (approximately 3 seconds for full range motion). Fuel Approved Fuel........................ Aviation Grade 100 LL (Blue) or 100 (Green) Total Fuel Capacity................................................. 58.5 U.S. gallons (221.4 L) Total Fuel Each Tank ............................................. 29.3 U.S. gallons (110.9 L) Total Usable Fuel (all flight conditions) .............. 56.0 U.S. gallons (212.0 L) Maximum Allowable Fuel Imbalance .......................7.5 U.S. gallons (28.4 L) The fuel pump must be set to ON for takeoff, climb, maneuvering flight, landing. Oil Maximum Oil Temperature ..................................................... 235 °F (113 °C) Minimum Oil Temperature for Takeoff................................... 100 °F (38 °C) Minimum Oil Pressure for Idling.............................................................25 psi Normal Operating Range of Oil Pressure ....................................... 55 - 95 psi Maximum Oil Pressure for Starting, Warm up, Taxi, & Takeoff ......115 psi 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 POWERPLANT L IMITATIONS P/N 44763-001 FAA APPROVED 2-7 Approved Oils: Engine Break-In: For first 50 hours of operation or until oil consumption stabilizes, use straight mineral oil conforming to SAE J1966 or MIL-L-6082B SAE grades. If engine oil must be added to the factory-installed oil, add only SAE J1966 or MIL-L-6082B straight mineral oil. After Engine Break-In: Use only oils conforming to SAE J1899 or MIL-L-22851 Ashless Dispersant SAE grades. • N OTE • The correct grade of oil to be used is based on environmental conditions. If the aircraft is going to be flown into an area that is much warmer or colder than the aircraft is usually operated in, use a different viscosity of oil. During operation, if the oil inlet temperatures are near the maximum permitted temperatures, then a higher viscosity oil can help to decrease the temperatures. Recommended Oil Grades a Ambient Air Temperature (SL) Engine Break-In After Engine Break-In Single Viscosity Multi- Viscosity Single Viscosity Multi- Viscosity All Temperatures - - - SAE 15W-50 SAE 20W-50 Above 80 °F (27 °C) SAE 60 - SAE 60 - Above 60 °F (16 °C) SAE 50 - SAE 40 SAE 50 - 30 °F (-1 °C) to 90 °F (32 °C) SAE 40 - SAE 40 - 0 °F (-18 °C) to 70 °F (21 °C) SAE 30 - SAE 30 SAE 40 SAE 20W-40 Below 10 °F (-12 °C) SAE 20 - SAE 20 SAE 30 SAE 20W-30 a. For additional qualified oil grades and viscosities, refer to the Lycoming Service Instruction No. 1014. Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS POWERPLANT L IMITATIONS SR20 2-8 FAA APPROVED P/N 44763-001 Propeller Hartzell Propeller Type ............................................................................Constant Speed Three-Blade Propeller, Metal (Standard): Model Number..........................................................HC-E3YR-1RF/F7392S-1 Diameter........................................................................74.0” (73.0” Minimum) Three-Blade Propeller, Composite (Optional): Model Number...............................................................3C1-R919A1/76C03-2 Diameter.....................................................................................74.0” Minimum 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 POWERPLANT L IMITATIONS P/N 44763-001 FAA APPROVED 2-9 Engine Instrument Markings & Annunciations The following describes the engine instrument markings. Powerplant Instrument (Range & Units) Red Arc/Bar Yellow Arc/Bar Green Arc/Bar Yellow Arc/Bar Red Arc/Bar Lower Warning Range Min. Caution Range Normal Range Max. Caution Range Upper Warning Range Cylinder Head Temperature (100 °F to 500 °F) –– –– 240 to 435 435 to 465 > 465 Engine Speed (0 to 3000 RPM) –– –– 500 to 2700 –– > 2700 a Exhaust Gas Temperature (500 °F to 1750 °F) –– –– 1000 to 1600 –– –– Manifold Pressure (10 to 35 Inch Hg) –– –– 15 to 29.5 –– –– Oil Pressure (0 to 115 PSI) 0 to 25 b 25 to 55 b 55 to 95 95 to 115 > 115 b Oil Temperature (75 °F to 250 °F) –– –– 100 to 235 –– > 235 Percent Power (0 to 100%) –– –– 0 to 100 –– –– a. Engine Speed Warning when RPM between 2710 and 2730 for more than 10 seconds OR when RPM greater than or equal to 2730 for more than 5 seconds. b. Oil Pressure Caution when oil pressure is between 25 and 54 psi and RPM is greater than 1000. Oil Pressure Warning when oil pressure is below 25 psi, OR oil pressure is above 115 psi. Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS POWERPLANT L IMITATIONS SR20 2-10 FAA APPROVED P/N 44763-001 Fuel Electrical Instrument (Range & Units) Red Arc/Bar Yellow Arc/Bar Green Arc/Bar Yellow Arc/Bar Red Arc/Bar Minimum Minimum Caution Range Normal Range Maximum Caution Range Maximum Fuel Flow (0 to 25 U.S. Gal/Hr) –– –– 0 to 21 a –– –– Fuel Quantity (0 to 28 U.S. Gallon) 0 0 to 10 10 to 28 –– –– a. Top of green arc dynamically changes based on altitude. Instrument (Range & Units) Red Arc/Bar Yellow Arc/Bar Green Arc/Bar Yellow Arc/Bar Red Arc/Bar Minimum Minimum Caution Range Normal Range Maximum Caution Range Maximum Essential Bus Volts (0 to 36 Volts) 0 to 24.4 –– 24.5 to 32 –– > 32 Main Bus 1 Voltage (0 to 36 Volts) –– 0 to 24.4 24.5 to 32 –– > 32 Main Bus 2 Voltage (0 to 36 Volts) –– 0 to 24.4 24.5 to 32 –– > 32 Alternator 1 Current (0 to 100 Amps) –– 0 to 1 a 2 to 100 –– –– Alternator 2 Current (0 to 100 Amps) –– 0 to 1 a 2 to 100 –– –– Battery 1 Current (-80 to 80 Amps) –– -80 to <-4b -4 to 80 –– –– a. 20 second delay of Caution CAS message. b. 30 second delay of Caution CAS message. 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 WEIGHT L IMITS P/N 44763-001 FAA APPROVED 2-11 Weight Limits Maximum Takeoff Weight.................................................... 3150 lb (1429 kg) Maximum Landing Weight................................................... 3150 lb (1429 kg) Maximum Weight in Baggage Compartment .......................... 130 lb (59 kg) Center of Gravity Limits CG Envelope Weight (lb) FS (inches) Forward Light 2100 137.8 Forward Intermediate 2700 139.1 Forward Gross 3150 141.1 Aft Gross 3150 148.1 Aft Light 2100 148.1 Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS CENTER OF GRAVITY L IMITS SR20 2-12 FAA APPROVED P/N 44763-001 Figure 2-1: Center of Gravity Envelope FS 148.1 2100 lb FS 137.8 2100 lb FS 139.1 2700 lb FS 141.1 3150 lb FS 148.1 3150 lb 2100 2300 2500 2600 2800 3000 2000 2200 2400 2700 2900 3100 3200 Fuselage Station (FS) Weight - Pounds 138 136 140 142 144 146 148 150 SR20_FM02_5739 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 M ANEUVER L IMITS P/N 44763-001 FAA APPROVED 2-13 Maneuver Limits Acrobatic maneuvers are prohibited. Spins are prohibited. This airplane is certified in the Normal category. • N OTE • Because the aircraft has not been certified for spin recovery, the Cirrus Airframe Parachute System (CAPS) must be deployed if the airplane departs controlled flight per 23-ACE-88. Refer to Section 3, Inadvertent Spin Entry. Flight Load Factor Limits Flaps UP (0%), any weight ..............................................................+3.8g, -1.9g Flaps 50%, any weight ...........................................................................+1.9g, 0g Flaps 100% (Down), any weight ..........................................................+1.9g, 0g Minimum Crew Requirements The minimum flight crew is one pilot. Kinds of Operation The aircraft is equipped and approved for the following type operations: • VFR day and night. • IFR day and night. Kinds of Operation Equipment List The following listing summarizes the equipment required under Code 14 of Federal Regulations (CFR) Part 23 for airworthiness under the “listed kind of operation”. Those minimum items of equipment necessary under the operating rules are defined in 14 CFR Part 91. • N OTE • All references to types of flight operations on the operating limita- tions placards are based upon equipment installed at the time of Airworthiness Certificate issuance. Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS K INDS OF OPERATION SR20 2-14 FAA APPROVED P/N 44763-001 System, Instrument and/or Equipment Kinds of Operation Remarks, Notes, and/or Exceptions VFR Day VFR Night IFR Day IFR Night PLACARDS AND MARKINGS Airplane Flight Manual 1 1 1 1 Garmin Cockpit Reference Guide 1 1 1 1 COMMUNICATIONS VHF COM A/R A/R 1 1 ELECTRICAL POWER Battery 1 1 1 1 1 Battery 2 - - 1 1 Alternator 1 1 1 1 1 Alternator 2 - - 1 1 Electrical Indications 1 1 1 1 Circuit Breakers A/R A/R A/R A/R As required. EQUIPMENT & FURNISHINGS Emergency Locator Transmitter 1 1 1 1 Egress Hammer 1 1 1 1 Restraint System A/R A/R A/R A/R One seat belt for each occupant. Inflatable Restraints - - - - FIRE PROTECTION Fire Extinguisher 1 1 1 1 FLIGHT CONTROLS Flap Position Indicator 1 1 1 1 Flap System 1 1 1 1 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 K INDS OF OPERATION P/N 44763-001 FAA APPROVED 2-15 Pitch Trim Indicator 1 1 1 1 Pitch Trim System 1 1 1 1 Roll Trim Indicator 1 1 1 1 Roll Trim System 1 1 1 1 Stall Warning System 1 1 1 1 Stick Shaker - - - - FUEL Auxiliary Fuel Pump 1 1 1 1 Fuel Quantity Indicators 2 2 2 2 Fuel Selector Valve 1 1 1 1 Automatic Fuel Selection - - - - ICE & RAIN PROTECTION Alternate Engine Air Induction System 1 1 1 1 Alternate Static Air Source 1 1 1 1 Pitot Heat - - 1 1 LANDING GEAR Wheel Pants - - - - May be removed. LIGHTS Anticollision Lights 2 2 2 2 Instrument Lights - 1 - 1 Navigation Lights - 2 - 2 Landing Light - 1 - 1 For hire operations. System, Instrument and/or Equipment Kinds of Operation Remarks, Notes, and/or Exceptions VFR Day VFR Night IFR Day IFR Night Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS K INDS OF OPERATION SR20 2-16 FAA APPROVED P/N 44763-001 Flash Light - 1 - 1 Ice Inspection Light - - - 1 NAVIGATION & PITOT STATIC Primary ADAHRS 1 1 2 2 Standby ADARS - - 1 1 Magnetic Compass A/R A/R A/R A/R Pitot System 1 1 1 1 Static System, Normal 1 1 1 1 VHF NAV - - A/R A/R GPS - - A/R A/R PFD/MFD 1 1 2 2 Touchscreen Controller 1 1 2 2 Marker Beacon Receiver - - A/R A/R Remote Audio Panel A/R A/R 1 1 Transponder 1 1 1 1 ENGINE INDICATING Cylinder Head Temperature - - - - Exhaust Gas Temperature - - - - Fuel Flow 1 1 1 1 Manifold Pressure 1 1 1 1 Oil Pressure 1 1 1 1 Oil Quantity (Dipstick) 1 1 1 1 System, Instrument and/or Equipment Kinds of Operation Remarks, Notes, and/or Exceptions VFR Day VFR Night IFR Day IFR Night 01 Aug 2023 Original Issue CIRRUS S ECTION 2: L IMITATIONS SR20 M AXIMUM O PERATING A LTITUDE L IMITS P/N 44763-001 FAA APPROVED 2-17 Maximum Operating Altitude Limits Maximum Airport Elevation ...................................................... 10,000 ft MSL Maximum Operating Altitude.................................................... 17,500 ft MSL The operating rules (CFR Part 91 and CFR Part 135) require the use of supplemental oxygen at specified altitudes below the maximum operating altitude. Outside Air Temperature Limit Takeoff Temperature Minimum Takeoff Temperature ...............................................-40 °F (-40 °C) Oil Temperature 1 1 1 1 Engine Speed 1 1 1 1 SPECIAL EQUIPMENT Cirrus Airframe Parachute (CAPS) 1 1 1 1 System, Instrument and/or Equipment Kinds of Operation Remarks, Notes, and/or Exceptions VFR Day VFR Night IFR Day IFR Night Original Issue 01 Aug 2023 S ECTION 2: L IMITATIONS CIRRUS M AXIMUM O CCUPANCY SR20 2-18 FAA APPROVED P/N 44763-001 Maximum Occupancy Serials w/ 2+1 Rear Seat Occupancy of this airplane is limited to “4+1” persons, the pilot and four passengers. If carrying three rear seat passengers, occupants must be wearing a seat belt and shoulder harness with their hips and back firmly against the seat back as shown in the following illustration. If three rear seat passengers cannot meet these requirements, occupancy is limited to four persons. Child Restraint System Limits 1. Rear seat configuration for LATCH / ISOFIX compliant child seats is limited to two seats in the outboard positions. 2. A single non-LATCH / ISOFIX compliant seat may be installed in the center seat position. 3. Installation of three child seats in the rear seat is prohibited. Figure 2-2: Rear Passenger Seat Arrangement Serials w/ Observer’s Seat Occupancy of this airplane is limited to three persons, the pilot and two passengers. SR20_FM02_5319 01 Aug 2023 Original Issue