Page 1 THIS MANUAL INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY 14 CFR 23 AND ADDITIONAL INFORMATION PROVIDED BY CIRRUS AIRCRAFT AND CONSTITUTES THE FAA APPROVED AIRPLANE FLIGHT MANUAL. Model - Serial #:...
Page 3: List Of Effective Pages
IRRUS IRPLANE LIGHT ANUAL SR20 FFECTIVE AGES List of Effective Pages Use this page to determine the current effective date for each page in the AFM. Supplements are issued individually and are controlled by the Log of Supplements Page in Section 9.
Page 4 IRRUS IRPLANE LIGHT ANUAL SR20 FFECTIVE AGES List of Effective Pages (Cont.) Page Status Page Status Page Status 3A-11 Original Issue Original Issue 8-13 Original Issue 3A-12 Original Issue Original Issue 8-14 Original Issue 3A-13 Original Issue 5-10 Original Issue...
Page 5 TAFM IRRUS AFM Temporary Change SR20 SR20 Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Airplane Flight Manual. Affected SR20 Basic Airplane Flight Manual: Publications: • P/N 44763-001 Original Issue...
Page 6 TAFM IRRUS AFM Temporary Change SR20 Intentionally Left Blank 2 of 8 FAA APPROVED TAFM 24-01 Original Issue 15 Jul 2024...
Page 7 SR20 OREWORD 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.
Page 8: Identifying Revised Material
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”...
Page 9 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-...
Page 10: Warnings, Cautions, And Notes
RONTMATTER IRRUS SR20 ARNINGS AUTIONS OTES 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.
Page 11: Table Of Contents
1: G IRRUS ECTION 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 ................
Page 12 1: G ECTION ENERAL IRRUS SR20 Intentionally Left Blank NOT FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 13: Introduction
1: G IRRUS ECTION ENERAL SR20 NTRODUCTION 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.
Page 14 1: G ECTION ENERAL IRRUS SR20 NTRODUCTION Figure 1-1: Airplane Three View 26.0 ft 7.92 m 8.9 ft 2.71 m 38.3 ft 11.67 m 74 inches 3-BLADE 188 cm 9.1 ft SR20_FM01_5662 2.8 m NOT FAA APPROVED P/N 44763-001 01 Aug 2023...
Page 15 1: G IRRUS ECTION ENERAL SR20 NTRODUCTION Figure 1-2: Airplane Interior Dimensions 49.3" 39.8" Fuselage Station 49.7" 38.5" 27.0" 16.0" 20.0" 10.5" 32.0" 39.0" 33.4" 20.0" 33.3" 5.0" 20.5" CABIN DOOR BAGGAGE DOOR OPENING OPENING SR20_FM01_5632 Location Length Width Height...
Page 16 1: G ECTION ENERAL IRRUS SR20 NTRODUCTION Figure 1-3: Turning Radius GROUND TURNING CLEARANCE 24.3 ft. (7.41 m) RADIUS FOR WING TIP 7.0 ft. (2.16 m) RADIUS FOR NOSE GEAR 0.5 ft. (0.15 m) RADIUS FOR INSIDE GEAR 9.1 ft.
Page 17: The Airplane
1: G IRRUS ECTION ENERAL SR20 IRPLANE 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............
Page 18: Oil
1: G ECTION ENERAL IRRUS SR20 IRPLANE 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..............
Page 19: Terminology
1: G IRRUS ECTION ENERAL SR20 IRPLANE 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.
Page 20 1: G ECTION ENERAL IRRUS SR20 IRPLANE General Airspeed Terminology (Continued) Terminology Definition Landing reference speed or threshold crossing speed. Stalling Speed is the minimum steady flight speed at which the aircraft is controllable. Stalling Speed is the minimum steady flight speed at...
Page 21 1: G IRRUS ECTION ENERAL SR20 IRPLANE Meteorological Terminology (Continued) Terminology Definition 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. Pressure Altitude is the altitude read from the altimeter when the altimeter’s barometric adjustment has been...
Page 22 1: G ECTION ENERAL IRRUS SR20 IRPLANE Table 4: Performance and Flight Planning Terminology Performance and Flight Planning Terminology Terminology Definition One “g” is a quantity of acceleration equal to that of earth’s gravity. Demonstrated Demonstrated Crosswind Velocity is the velocity of...
Page 23 1: G IRRUS ECTION ENERAL SR20 IRPLANE 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...
Page 24 1: G ECTION ENERAL IRRUS SR20 IRPLANE Weight and Balance Terminology (Continued) Terminology Definition 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.
Page 25 2: L IRRUS ECTION 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..............
Page 26 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 ..............
Page 27 2: L IRRUS ECTION IMITATIONS SR20 LACARDS Placards Interior Placards Figure 2-4: Placards (5 of 5) CAPS Overhead Placard : IRRUS IRFRAME ARACHUTE YSTEM EMERGENCY USE ONLY SEAT BELTS MUST BE WORN AT ALL TIMES TO ACTIVATE: PULL HANDLE DOWN STEADILY WITH...
Page 28 2: L ECTION IMITATIONS IRRUS SR20 LACARDS Intentionally Left Blank 4 of 8 FAA APPROVED TAFM 24-01 15 Jul 2024 Original Issue...
Page 29: Introduction
2: L IRRUS ECTION IMITATIONS SR20 NTRODUCTION 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.
Page 30: Taxiing, Takeoff, And Landing Limitations
2: L ECTION IMITATIONS IRRUS SR20 AXIING AKEOFF ANDING IMITATIONS 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 ) ..........
Page 31: Airspeed Indicator Markings
2: L IRRUS ECTION IMITATIONS SR20 IRSPEED NDICATOR ARKINGS 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.
Page 32: Powerplant Limitations
2: L ECTION IMITATIONS IRRUS SR20 OWERPLANT IMITATIONS Powerplant Limitations Engine Lycoming Engines................. IO-390-C3B6 Power Rating ..............215 HP @ 2700 RPM Maximum RPM ..................2700 RPM • N • 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.
Page 33 2: L IRRUS ECTION IMITATIONS SR20 OWERPLANT IMITATIONS 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.
Page 34: Propeller
2: L ECTION IMITATIONS IRRUS SR20 OWERPLANT IMITATIONS 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 FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 35: Engine Instrument Markings & Annunciations
2: L IRRUS ECTION IMITATIONS SR20 OWERPLANT IMITATIONS Engine Instrument Markings & Annunciations The following describes the engine instrument markings. Powerplant Yellow Green Yellow Arc/Bar Arc/Bar Arc/Bar Arc/Bar Arc/Bar Instrument Lower Min. Max. Upper (Range & Units) Normal Warning Caution...
Page 36: Fuel
2: L ECTION IMITATIONS IRRUS SR20 OWERPLANT IMITATIONS Fuel Yellow Green Yellow Arc/Bar Arc/Bar Arc/Bar Arc/Bar Arc/Bar Instrument Minimum Maximum (Range & Units) Normal Minimum Caution Caution Maximum Range Range Range Fuel Flow –– –– –– –– 0 to 21 (0 to 25 U.S.
Page 37: Weight Limits
2: L IRRUS ECTION IMITATIONS SR20 EIGHT IMITS 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...
Page 38 2: L ECTION IMITATIONS IRRUS SR20 ENTER OF RAVITY IMITS Figure 2-1: Center of Gravity Envelope 3200 3100 FS 141.1 FS 148.1 3150 lb 3150 lb 3000 2900 2800 2700 FS 139.1 2700 lb 2600 2500 2400 2300 2200 FS 148.1 FS 137.8...
Page 39: Maneuver Limits
This airplane is certified in the Normal category. • N • 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.
Page 40 2: L ECTION IMITATIONS IRRUS SR20 INDS OF PERATION Kinds of Operation System, Instrument Remarks, Notes, and/or Equipment and/or Exceptions Night Night PLACARDS AND MARKINGS Airplane Flight Manual Garmin Cockpit Reference Guide COMMUNICATIONS VHF COM ELECTRICAL POWER Battery 1 Battery 2...
Page 41 2: L IRRUS ECTION IMITATIONS SR20 INDS OF PERATION Kinds of Operation System, Instrument Remarks, Notes, and/or Equipment and/or Exceptions Night Night Pitch Trim Indicator Pitch Trim System Roll Trim Indicator Roll Trim System Stall Warning System Stick Shaker FUEL...
Page 42 2: L ECTION IMITATIONS IRRUS SR20 INDS OF PERATION Kinds of Operation System, Instrument Remarks, Notes, and/or Equipment and/or Exceptions Night Night Flash Light Ice Inspection Light NAVIGATION & PITOT STATIC Primary ADAHRS Standby ADARS Magnetic Compass Pitot System Static System, Normal...
Page 43: Maximum Operating Altitude Limits
2: L IRRUS ECTION IMITATIONS SR20 AXIMUM PERATING LTITUDE IMITS Kinds of Operation System, Instrument Remarks, Notes, and/or Equipment and/or Exceptions Night Night Oil Temperature Engine Speed SPECIAL EQUIPMENT Cirrus Airframe Parachute (CAPS) Maximum Operating Altitude Limits Maximum Airport Elevation ............10,000 ft MSL Maximum Operating Altitude............
Page 44: Maximum Occupancy
2: L ECTION IMITATIONS IRRUS SR20 AXIMUM CCUPANCY 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.
Page 45: Child Restraint System Limits
2: L IRRUS ECTION IMITATIONS SR20 AXIMUM CCUPANCY Child Restraint System Limits 1. Rear seat configuration for LATCH / ISOFIX compliant child seat is limited to the Observer’s Seat. Figure 2-3: Observer’s Seat Arrangement SR20_FM02_5320 Serials w/o 2+1 Rear Seat or Observer’s Seat 1.
Page 46: Systems And Equipment Limits
IMITS Systems and Equipment Limits The appropriate revision of the Cirrus Perspective Touch+ Cockpit Refer- ence Guide (P/N 190-02954-XX, where X can be any digit from 0 to 9) must be immediately available to the pilot during flight. The system software version stated in the reference guide must be appropriate for the system software version displayed on the equipment.
Page 47: Engagement Limits
VNAV will be disabled at the beginning of the teardrop. Navigation and Communication Equipment Attitude and Heading Reference System (AHRS) Navigation using the Cirrus Perspective Touch+ Integrated Avionics System is prohibited in the following geographic areas. Magnetic Cut-out Regions Latitude...
Page 48: Cirrus Perspective Touch+ Integrated Avionics System
RNAV approaches must be conducted utilizing the GPS sensor. g) The Cirrus Perspective Touch+ Integrated Avionics System is compliant with AC 90-100A. As such, the Cirrus Perspective Touch+ system is eligible to fly RNAV 'Q' or 'T' routes, RNAV SID/STAR/ODPs and eligible to use RNAV substitution or RNAV alternate means of navigation (US Only).
Page 49 TSOC145d (Sensors) and (Display Units) for Class 3 system. i) The Cirrus Perspective Touch+ Integrated Avionics System has been installed in accordance with AC 20-138A and is approved for navi- gation using GPS and SBAS (within the coverage of a Satellite Based Augmentation System complying with ICAO annex 10) for IFR enroute, terminal and approach operations.
Page 50: Traffic Advisory System (Tas)
2: L ECTION IMITATIONS IRRUS SR20 YSTEMS AND QUIPMENT IMITS 4. FIS-B Receiver Equipment, including GTX 345 Mode S UAT in Tran- sponder (optional): a) Flight Information Services - Broadcast (FIS-B) information is intended to enhance pilot awareness of weather and airspace condi- tions.
Page 51: Synthetic Vision System (Svs)
2: L IRRUS ECTION IMITATIONS SR20 YSTEMS AND QUIPMENT IMITS Synthetic Vision System (SVS) Use of the Synthetic Vision System (SVS) for flight guidance, navigation, traffic avoidance, or terrain avoidance is prohibited. Maneuvering the airplane in any phase of flight such as taxi, takeoff, approach, landing, or roll out should not be predicated on SVS imagery.
Page 52: Air Conditioning System
Air Conditioning System The use of Recirculation Mode during flight is prohibited. Inflatable Restraint System Use of a child safety seat with inflatable restraint system is prohibited. Cirrus Airframe Parachute System (CAPS) Maximum Demonstrated Deployment Speed ......133 KIAS • N •...
Page 53: Placards
2: L IRRUS ECTION IMITATIONS SR20 LACARDS Placards Exterior Placards Figure 2-4: Placards (1 of 5) Engine compartment, inside oil filler access: CAPACITY: 7 U.S. QUARTS (6.6 LITERS) AFTER BREAK-IN: USE ASHLESS DISPERSANT OIL SAE 15W50 OR SAE 20W50 ACCEPTABLE FOR ALL TEMPERATURES...
Page 54 2: L ECTION IMITATIONS IRRUS SR20 LACARDS Figure 2-4: Placards (2 of 5) Left fuselage, on external power supply door: EXTERNAL POWER 28 V DC Doors, adjacent to latch: OPEN SR20_FM02_5411A 2-28 FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 55: Interior Placards
2: L IRRUS ECTION IMITATIONS SR20 LACARDS Interior Placards Figure 2-4: Placards (3 of 5) Engine control panel: RICH IDLE CUTOFF LIFT BUTTON FOR OFF POSITION SR20_FM02_5679 P/N 44763-001 FAA APPROVED 2-29 Original Issue 01 Aug 2023...
Page 56 2: L ECTION IMITATIONS IRRUS SR20 LACARDS Figure 2-4: Placards (4 of 5) Baggage Compartment, aft edge: ELT LOCATED BEHIND BULKHEAD REMOVE CARPET AND ACCESS PANEL Cabin Door Window, lower edge, centered, applied upside down: RESCUE: FRACTURE AND REMOVE WINDOW...
Page 57 3: E IRRUS ECTION MERGENCY ROCEDURES SR20 Section 3: Emergency Procedures Table of Contents Introduction..................3 Crew Alert System (CAS) Messaging ..........3 Warnings ..................3 CAPS Guidance ................3 Preflight Planning ................4 Preflight Inspections/Maintenance ............ 4 Methodology..................4 Maintain Aircraft Control ..............
Page 58 3: E ECTION MERGENCY ROCEDURES IRRUS SR20 Engine Fire In Flight ................ 18 Engine Partial Power Loss .............. 19 Inadvertent Spin Entry ..............21 Landing Without Elevator Control............ 22 Power Lever Linkage Failure............23 Propeller Governor Failure .............. 24 Rejected Takeoff ................24 Smoke and Fume Elimination............
Page 59: Section 3: Emergency Procedures
CAPS Guidance All Cirrus aircraft are equipped with a pilot or passenger activated ballistic airframe parachute system. The system is capable of lowering the aircraft and occupants safely to the ground for life threatening emergencies. CAPS provides pilots and passengers an alternative means of handling various life threatening emergency situations.
Page 60: Preflight Planning
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 NTRODUCTION Preflight Planning Enroute emergencies caused by weather can be minimized or eliminated by careful flight planning and good judgment when unexpected weather is encountered. Preflight Inspections/Maintenance In-flight mechanical problems in the aircraft will be extremely rare if proper preflight inspections and maintenance are practiced.
Page 61: Land As Soon As Conditions Permit
ECTION MERGENCY ROCEDURES SR20 NTRODUCTION The Cirrus Airframe Parachute System (CAPS) should be activated in the event of a life-threatening emergency where CAPS deployment is deter- mined to be safer than continued flight and landing. • N • Refer to Section 10, Cirrus Airframe Parachute System (CAPS) CAPS deployment information and landing considerations.
Page 62: Procedure Division Symbols
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 NTRODUCTION Procedure Division Symbols For procedures requiring pilot decision, conditional steps are indented with a symbol to designate sub-sections within the procedure. On condi- tion, the pilot makes a decision to identify the applicable sub-section.
Page 63: Airspeeds For Emergency Operations
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 IRSPEEDS FOR MERGENCY PERATIONS Airspeeds for Emergency Operations Maneuvering Speed 3150 lb (1429 kg) ..................133 KIAS 2700 lb (1225 kg) ..................123 KIAS 2300 lb (1043 kg) ..................114 KIAS Best Glide (Flaps: UP) 3150 lb (1429 kg) ..................100 KIAS 2600 lb (1179 kg) ..................92 KIAS...
Page 64: Glide
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 LIDE Glide Conditions Example Power Altitude 8,000 ft. AGL Propeller Windmilling Airspeed Best Glide Flaps 0% (UP) Glide Distance 12 NM Wind Zero Best Glide Speed 3150 lb (1429 kg).................. 100 KIAS 2600 lb (1179 kg)..................92 KIAS...
Page 65: Emergency Procedures
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 MERGENCY ROCEDURES Emergency Procedures Automatic Flight Control Malfunction (Autopilot, ESP, Trim, Flaps) 1. AP DISC Button............PRESS AND HOLD 2. AP SERVO (A1), PITCH TRIM (B1), ROLL TRIM (B2), FLAPS (D3) CBs................PULL, AS REQUIRED 3.
Page 66 3: E ECTION MERGENCY ROCEDURES IRRUS SR20 MERGENCY ROCEDURES (Continued) • N • If the airplane is in IMC conditions, turn ALT 1, ALT 2, and BAT 1 switches OFF. Power from battery 2 will keep the Primary Flight Display operational for approximately 30 minutes. If airplane is in day VFR conditions and turning off the BAT/ALT switches elim- inated the fire situation, leave the BAT/ALT switches OFF.
Page 67: Caps Deployment
Procedure Complete • N • The Cirrus Airframe Parachute System (CAPS) should be acti- vated immediately in the event of a spin. It should also be used in other life threatening emergencies where CAPS deployment is determined to be safer than continued flight and landing.
Page 68: Ditching
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 MERGENCY ROCEDURES (Continued) • CAUTION • CAPS deployment will likely result in damage or loss to the airframe. • N • Several possible scenarios in which the activation of the CAPS would be appropriate are discussed in...
Page 69: Emergency Descent
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 MERGENCY ROCEDURES Emergency Descent 1. AP DISC Button............PRESS AND RELEASE 2. Power Lever .................... IDLE 3. Mixture................RICH (AS REQ’D) 4. Airspeed ................INCREASE TO V Procedure Complete • CAUTION • If significant turbulence is expected, do not descend at indicated...
Page 70: Emergency Ground Egress
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 MERGENCY ROCEDURES Emergency Ground Egress 1. Mixture .....................CUTOFF 2. Fuel Pump ....................OFF 3. BAT 1 and BAT 2 Switches..............OFF 4. Parking Brake.................... SET 5. Egress aircraft. Procedure Complete • WARNING • While exiting the airplane, make sure evacuation path is clear of other aircraft, spinning propellers, and other hazards.
Page 71: Emergency Landing W/O Power
• WARNING • If a safe landing is not assured, consider CAPS Deployment. Refer to Section 10, for CAPS deploy- Cirrus Airframe Parachute System (CAPS) ment scenarios and landing considerations. After landing: d. BAT 1 and BAT 2 Switches ..............OFF e.
Page 72: Engine Failure In Flight
If altitude or terrain does not permit a safe landing, CAPS deployment may be required. Refer to Section 10, Cirrus Airframe Parachute System (CAPS) CAPS deployment scenarios and landing considerations 3-16...
Page 73: Engine Failure On Takeoff - Low Altitude
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 MERGENCY ROCEDURES Engine Failure On Takeoff - Low Altitude 1. Best Glide or Landing Speed ............ESTABLISH 2. Fuel Selector....................OFF 3. Flaps ..................AS REQUIRED 4. Land straight ahead. ◆ If time permits: a. Power Lever ..................IDLE b.
Page 74: Engine Fire During Start
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 MERGENCY ROCEDURES Engine Fire During Start 1. Mixture .....................CUTOFF 2. Fuel Pump ....................OFF 3. Fuel Selector ....................OFF 4. Power Lever................. FORWARD 5. Starter....................ENGAGE ◆ If flames persist: a. Evacuate aircraft. Procedure Complete •...
Page 75: Engine Partial Power Loss
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 MERGENCY ROCEDURES Engine Partial Power Loss 1. Air Conditioner (if installed) ..............OFF 2. Fuel Pump....................ON 3. Fuel Selector..............SWITCH TANKS 4. Mixture....CHECK APPROPRIATE FOR FLIGHT CONDITIONS 5. Power Lever ..................SWEEP 6. Alternate Induction Air ................ON 7.
Page 76 3: E ECTION MERGENCY ROCEDURES IRRUS SR20 MERGENCY ROCEDURES (Continued) • N • Low oil pressure may be indicative of an imminent engine failure. OIL PRESSURE Warning Checklist in this Section for special procedures with low oil pressure. A damaged (out-of-balance) propeller may cause extremely rough operation.
Page 77: Inadvertent Spin Entry
The aircraft is not approved for spins, and has not been certified for traditional spin recovery characteristics. The only approved and demonstrated method of spin recovery is activation of the Cirrus Airframe Parachute System (see CAPS Deployment Checklist, this section). Because of this, if the aircraft enters a spin, CAPS must be deployed immediately.
Page 78: Landing Without Elevator Control
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 MERGENCY ROCEDURES Landing Without Elevator Control 1. Flaps ......................50% 2. Trim ....................80 KIAS 3. Power ..........AS REQUIRED FOR GLIDE ANGLE Procedure Complete • CAUTION • The pitch trim spring cartridge is attached directly to the elevator and provides a backup should you lose the primary elevator control system.
Page 79: Power Lever Linkage Failure
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 MERGENCY ROCEDURES Power Lever Linkage Failure 1. Power Lever Movement ..............VERIFY 2. Power ..................SET IF ABLE 3. Flaps ..................SET IF NEEDED 4. Mixture ........AS REQUIRED (FULL RICH TO CUTOFF) 5. Land as soon as possible.
Page 80: Propeller Governor Failure
3: E ECTION MERGENCY ROCEDURES IRRUS SR20 MERGENCY ROCEDURES Propeller Governor Failure 1. Power Lever...... REDUCE TO MINIMUM NECESSARY FOR SUSTAINED FLIGHT 2. Airspeed............... REDUCE TO 85-90 KIAS 3. Land as soon as practicable. Procedure Complete • N • An in-flight governor failure will likely result in a large exceedance (3000 RPM or more), as propeller blade angle will go to fine pitch.
Page 81: Smoke And Fume Elimination
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 MERGENCY ROCEDURES Smoke and Fume Elimination 1. Air Conditioner............RECIRC DISABLED 2. Temperature Selector ................COLD 3. Vent Selector............FEET/PANEL/DEFROST 4. Airflow Selector................MAXIMUM 5. Fuel Selector..............MANUAL MODE ◆ If source of smoke and fume is firewall forward: a.
Page 82: Emergency Cas Procedures
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SR20 MERGENCY ROCEDURES Emergency CAS Procedures APPROACH SPEED Warning APPROACH SPEED Approach speed is too high. 1. Approach................GO-AROUND Procedure Complete 3-26 FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 83: Auto Descent Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 CAS P MERGENCY ROCEDURES AUTO DESCENT Warning AUTO DESCENT Automatic descent to 14,000FT in 60 seconds. Aircraft descending to 14,000FT. Aircraft descending to 12,500FT. Aircraft descended due to pilot incapacitation. 1. Situation ....................ASSESS •...
Page 84: Cht Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SR20 MERGENCY ROCEDURES CHT Warning Cylinder head temperature is high. ◆ If on ground: a. Power Lever .............REDUCE TO IDLE b. Mixture .................FULL RICH c. Annunciations and Engine Temperatures .......MONITOR ❍ If Warning annunciation is still illuminated, and temperatures not decreasing: (1)Shutdown engine.
Page 85: Co Level High Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 CAS P MERGENCY ROCEDURES CO LEVEL HIGH Warning CO LEVEL HIGH Carbon monoxide level is too high. 1. Air Conditioner............RECIRC DISABLED 2. Temperature Selector ................COLD 3. Vent Selector............FEET/PANEL/DEFROST 4. Airflow Selector................MAXIMUM 5.
Page 86: Essential Bus Volts Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SR20 MERGENCY ROCEDURES ESSENTIAL BUS VOLTS Warning ESSENTIAL BUS VOLTS Check essential power bus voltage. 1. Essential Bus Voltage (ESS Bus V)..........CHECK ◆ If Essential Bus Voltage is greater than 32 Volts: a.
Page 87: Fuel Imbalance Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 CAS P MERGENCY ROCEDURES FUEL IMBALANCE Warning FUEL IMBALANCE Fuel quantity imbalance has been detected. 1. Fuel Quantity Gauges............... CHECK 2. Fuel Selector............SELECT FULLER TANK Procedure Complete • N • Fuel level imbalance (between left and right) is greater than 9.5 gallons.
Page 88: Fuel Low Total Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SR20 MERGENCY ROCEDURES FUEL LOW TOTAL Warning FUEL LOW TOTAL Total fuel quantity is low. 1. Fuel Quantity Gauges ...............CHECK 2. Totalized Fuel Quantity..............CHECK ◆ If totalized fuel quantity differs significantly from sensed quantity: a.
Page 89: Main Bus 2 Volts Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 CAS P MERGENCY ROCEDURES MAIN BUS 2 VOLTS Warning MAIN BUS 2 VOLTS Check voltage on main power bus 2. ◆ If Main Bus 1 VOLTS Warning is also asserted: a. Perform MAIN BUS 1 VOLTS Warning Checklist.
Page 90: Oil Pressure Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SR20 MERGENCY ROCEDURES OIL PRESSURE Warning OIL PRESSURE Oil pressure is out of range. 1. Oil Pressure Gauge................CHECK ◆ If pressure low / high: a. Power ..REDUCE TO MINIMUM FOR SUSTAINED FLIGHT b.
Page 91: Rpm Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 CAS P MERGENCY ROCEDURES RPM Warning Check engine RPM. 1. Tachometer..................CHECK ◆ If engine speed normal: a. If on ground........CORRECT PRIOR TO FLIGHT b. If in flight ............CONTINUE, MONITOR Procedure Complete ◆...
Page 92: Spin Spin Spin Warning
The aircraft is not approved for spins, and has not been certified for traditional spin recovery characteristics. The only approved and demonstrated method of spin recovery is activation of the Cirrus Airframe Parachute System (see CAPS Deployment Checklist, this section). Because of this, if the aircraft enters a spin, CAPS must be deployed immediately.
Page 93: Stall Warning
3: E IRRUS ECTION MERGENCY ROCEDURES SR20 CAS P MERGENCY ROCEDURES STALL Warning STALL Stall imminent. 1. Angle of Attack................REDUCE 2. Power Lever ..............FULL FORWARD Procedure Complete STALL WARNING FAIL Warning STALL WARNING FAIL Stall warning is inoperative. 1. Airspeed ............MAINTAIN ABOVE 1.3 V 2.
Page 94: Starter Engaged Warning
3: E ECTION MERGENCY ROCEDURES IRRUS CAS P SR20 MERGENCY ROCEDURES STARTER ENGAGED Warning STARTER ENGAGED Starter is engaged. ◆ If on ground: a. Starter Button ................RELEASE ❍ If starter does not disengage (stuck button, relay, or solenoid failure): (1) Wait 1 minute before next start attempt.
Page 95 3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 Section 3A: Abnormal Procedures Table of Contents Introduction..................3 Crew Alert System (CAS) Messaging ..........3 Cautions ..................3 Advisories ..................3 Abnormal Procedures Guidance ............3 Circuit Breakers................. 4 Procedure Division Symbols ............. 4 Landing Guidance ................
Page 96 3A: A ECTION BNORMAL ROCEDURES IRRUS SR20 FUEL IMBALANCE Advisory............18 FUEL IMBALANCE Caution ............18 FUEL LOW TOTAL Caution ............19 FUEL PUMP OFF Caution .............. 19 FUEL QTY MISCOMPARE Caution ..........19 FUEL VALVE AUTO FAIL Caution..........20 FUEL VALVE OFF Advisory............
Page 97 3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 BNORMAL ROCEDURES Abnormal Procedures Fuel Valve Malfunction ◆ If manual fuel selector operation is difficult: a. FUEL VALVE Circuit Breaker (C3) ........... PULL b. Fuel Selector ........LEFT OR RIGHT (AS REQ’D) ❍ If difficult operation persists: (1)Fuel Selector........
Page 98 3A: A ECTION BNORMAL ROCEDURES IRRUS SR20 BNORMAL ROCEDURES Intentionally Left Blank 6 of 8 FAA APPROVED TAFM 24-01 Original Issue 15 Jul 2024...
Page 99: Introduction
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 NTRODUCTION Introduction This section provides procedures for handling abnormal system and/or flight conditions which, if followed, will maintain an acceptable level of airworthiness or reduce operational risk. The guidelines described in this section are to be used when an abnormal condition exists, and should be considered and applied as necessary.
Page 100: Circuit Breakers
ECTION BNORMAL ROCEDURES IRRUS SR20 NTRODUCTION Sound judgment as well as thorough knowledge of the aircraft, its charac- teristics, and the flight manual procedures are essential in the handling of any abnormal system and/or flight condition. In addition to the outlined...
Page 101: Landing Guidance
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 NTRODUCTION Landing Guidance Land as Soon as Practicable The pilot may consider the convenience of future maintenance when selecting an airport to land as soon as practicable. Pilots must not overfly a suitable and practicable airport for other ground conveniences.
Page 102: Abnormal Procedures
3A: A ECTION BNORMAL ROCEDURES IRRUS SR20 BNORMAL ROCEDURES Abnormal Procedures Brake Failure During Taxi 1. Engine Power ................AS REQUIRED 2. Directional Control........MAINTAIN WITH RUDDER 3. Brake Pedal(s) ..................PUMP ◆ If directional control cannot be maintained: a. Engine Knob ..................OFF Procedure Complete •...
Page 103: Door Open
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 BNORMAL ROCEDURES Door Open ◆ If during takeoff roll: a. Takeoff ..................ABORT Procedure Complete ◆ If in flight: a. Airplane Control..............MAINTAIN b. Land as soon as practicable. Procedure Complete • N • The doors on the airplane will remain 1-3 inches open in flight if not latched.
Page 104: Inadvertent Icing Encounter
3A: A ECTION BNORMAL ROCEDURES IRRUS SR20 BNORMAL ROCEDURES Inadvertent Icing Encounter 1. Probe Heat....................ON 2. Exit icing conditions. Turn back or change altitude. 3. Temperature Selector................HOT 4. Vent Selector..................DEFROST 5. Airflow Selector ................. MAXIMUM 6. Panel Vents ..................CLOSED 7.
Page 105: Landing With Failed Brakes
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 BNORMAL ROCEDURES Landing With Failed Brakes ◆ One brake inoperative: a. Land on the side of runway corresponding to the inoperative brake. b. Maintain directional control using rudder and working brake. Procedure Complete ◆...
Page 106: Loss Of All Flight Displays
3A: A ECTION BNORMAL ROCEDURES IRRUS SR20 BNORMAL ROCEDURES Loss of All Flight Displays 1. BAT 1 and BAT 2 Switches............VERIFY ON 2. ALT 1 and ALT 2 Switches ............VERIFY ON 3. Land as soon as possible. Procedure Complete Loss of Reliable Airspeed Indication 1.
Page 107: Afcs Alerts
BNORMAL ROCEDURES SR20 AFCS A LERTS AFCS Alerts For more information on AFCS alerts, refer to SR20 Garmin Cockpit Refer- ence Guide. Abnormal CAS Procedures ALTERNATOR 1 CURRENT Caution ALTERNATOR 1 CURRENT Check Alternator 1 current. 1. ALT 1 (D11) Circuit Breaker ..............SET 2.
Page 108: Alternator 2 Current Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES ALTERNATOR 2 CURRENT Caution ALTERNATOR 2 CURRENT Check Alternator 2 current. 1. ALT 2 (B5) Circuit Breaker..............SET 2. ALT 2 Switch..................CYCLE ◆ If alternator does not reset: a.
Page 109: Battery 1 Fail Caution
Continue flight. ◆ If message persists or reoccurs: a. BAT 1 switch ..................OFF b. Exit IMC as soon as practicable. c. Land as soon as practicable. 2. Contact Cirrus for corrective action. Procedure Complete P/N 44763-001 FAA APPROVED 3A-13 Original Issue...
Page 110: Battery 1 Low Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES BATTERY 1 LOW Caution BATTERY 1 LOW Battery 1 state of charge is low. ◆ If on ground, prior to engine start: a. External Power ..............CONNECT Procedure Complete ◆...
Page 111: Cht Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES CHT Caution Cylinder head temperature is high. ◆ If on ground: a. Power Lever ................REDUCE b. Annunciations and Engine Temperatures ....... MONITOR ❍ If message persists: (1)Power Lever ..........MINIMUM REQUIRED (2)Do not dispatch.
Page 112: Flaps Airspeed Inhibit Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES FLAPS AIRSPEED INHIBIT Caution FLAPS AIRSPEED INHIBIT Flaps motion inhibited. 1. Airspeed......... INCREASE OR REDUCE, AS REQUIRED 2. Flaps ..........RETURN TO PREVIOUS POSITION Procedure Complete • N • The flaps will extend or retract to the commanded position as soon as FLAPS AIRSPEED INHIBIT caution extinguishes.
Page 113: Flaps Disagree Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES FLAPS DISAGREE Caution FLAPS DISAGREE Flaps are not within commanded position. 1. Flaps ..........CYCLE TO ACTUAL FLAP POSITION ◆ If message extinguishes: a. Flaps...........SELECT DESIRED FLAP POSITION b. Continue flight.
Page 114: Flaps Selector Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES FLAPS SELECTOR FAIL Caution FLAPS SELECTOR FAIL Flaps not in commanded position. 1. Perform landing with flaps at current position. Procedure Complete FUEL IMBALANCE Advisory FUEL IMBALANCE Fuel quantity imbalance has been detected.
Page 115: Fuel Low Total Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES FUEL LOW TOTAL Caution FUEL LOW TOTAL Total fuel quantity is low. 1. Fuel Quantity Gauges............... CHECK 2. Totalized Fuel Quantity..............CHECK ◆ If totalized value differs significantly from sensed quantity: a.
Page 116: Fuel Valve Auto Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES FUEL VALVE AUTO FAIL Caution FUEL VALVE AUTO FAIL Automatic fuel tank selection is unavailable. 1. FUEL VALVE (C3) Circuit Breaker ........... PULL 2. Fuel Selector ..........LEFT OR RIGHT (AS REQ'D) Procedure Complete •...
Page 117: Main Bus 1 Volts Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES MAIN BUS 1 VOLTS Caution MAIN BUS 1 VOLTS Check voltage on Main Bus 1. 1. ALT 1 (D11) Circuit Breaker ..............SET 2. ALT 1 Switch ..................CYCLE ◆...
Page 118: Main Bus 2 Volts Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES MAIN BUS 2 VOLTS Caution MAIN BUS 2 VOLTS Check voltage on Main Bus 2. 1. ALT 2 (B5) Circuit Breaker..............SET 2. ALT 2 Switch..................CYCLE ◆ If alternator does not reset: a.
Page 119: Oil Temp Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES OIL TEMP Caution OIL TEMP Oil temperature is high. 1. Power ..........REDUCE AS MUCH AS PRACTICAL 2. Airspeed ..................INCREASE 3. Mixture ..........ADJUST TO TOP OF GREEN ARC 4.
Page 120: Probe Heat Fail Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES PROBE HEAT FAIL Caution PROBE HEAT FAIL Probe heat failure. 1. Probe Heat Circuit Breaker............... CYCLE 2. Probe Heat................CYCLE OFF, ON ◆ If inadvertent icing encountered, perform Inadvertent Icing Encounter Checklist and: a.
Page 121: Sfd Alt Miscompare Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES SFD ALT MISCOMPARE Caution SFD ALT MISCOMPARE SFD altitude miscompare. 1. DISPLAY BACKUP Button ............... PRESS 2. Altitude..........CROSS-CHECK SFD WITH PFD 3. Altitude........ CROSS-CHECK PFD ADC 1 WITH ADC 2 •...
Page 122: Sfd Ias Miscompare Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES SFD IAS MISCOMPARE Caution SFD IAS MISCOMPARE SFD airspeed miscompare. 1. DISPLAY BACKUP Button..............PRESS 2. Airspeed..........CROSS-CHECK SFD WITH PFD 3. Airspeed.......CROSS-CHECK PFD ADC 1 WITH ADC 2 • N •...
Page 123: Sfd Pitch Miscompare Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES SFD PITCH MISCOMPARE Caution SFD PITCH MISCOMPARE SFD pitch miscompare. 1. DISPLAY BACKUP Button ............... PRESS 2. Attitude ..........CROSS-CHECK SFD WITH PFD 3. Attitude ......CROSS-CHECK PFD AHRS 1 WITH AHRS 2 •...
Page 124: Sfd Roll Miscompare Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS CAS P SR20 BNORMAL ROCEDURES SFD ROLL MISCOMPARE Caution SFD ROLL MISCOMPARE SFD roll miscompare. 1. DISPLAY BACKUP Button..............PRESS 2. Attitude..........CROSS-CHECK SFD WITH PFD 3. Attitude......CROSS-CHECK PFD AHRS 1 WITH AHRS 2 • N •...
Page 125: Starter Engaged Caution
3A: A IRRUS ECTION BNORMAL ROCEDURES SR20 CAS P BNORMAL ROCEDURES STARTER ENGAGED Caution STARTER ENGAGED Starter is engaged. ◆ If on ground: a. Starter Button................RELEASE ❍ If starter does not disengage (stuck button, relay, or solenoid failure): (1)Wait 20 seconds before next start attempt.
Page 126: Takeoff Flaps Caution
3A: A ECTION BNORMAL ROCEDURES IRRUS SR20 THER YSTEM ESSAGES TAKEOFF FLAPS Caution TAKEOFF FLAPS Flaps not in takeoff configuration. 1. Takeoff ....................ABORT 2. Flaps ......................50% Procedure Complete Other System Messages MFD FAN FAIL Advisory MFD FAN FAIL MFD cooling fan failure.
Page 127 4: N IRRUS ECTION ORMAL ROCEDURES SR20 Section 4: Normal Procedures Table of Contents Introduction..................3 Airspeeds for Normal Operation............3 Normal Procedures ................4 Preflight Inspection................4 Before Engine Start ................9 Engine Start..................10 Before Taxi ..................12 Before Takeoff.................
Page 128 4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES Normal Procedures Landing • CAUTION • Landings should be made with full flaps. Landings with less than full flaps are recommended only if the flaps fail to deploy or to extend the aircraft’s glide distance due to engine malfunction.
Page 129 4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES Intentionally Left Blank TAFM 24-01 FAA APPROVED 8 of 8 15 Jul 2024 Original Issue...
Page 130 4: N ECTION ORMAL ROCEDURES IRRUS SR20 Intentionally Left Blank FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 131: Introduction
Normal Procedures. Normal operating procedures for the Garmin TAWS and GFC 700 Automatic Flight Control System are described in the Cirrus Perspective+ Integrated Flight Deck Pilot’s Guide. Airspeeds for Normal Operation Unless otherwise noted, the following speeds are based on a maximum weight of 3150 lb.
Page 132: Normal Procedures
4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES Normal Procedures Preflight Inspection • WARNING • Before carrying out preflight inspections, ensure that all required main- tenance has been accomplished. Review your flight plan and compute weight and balance and performance requirements. Throughout the walk-around: check all hinges, hinge pins, and bolts for security;...
Page 133 4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES (Continued) 1. Cabin a. Required Documents ..............CHECK b. BAT 2 Switch..................ON (1) Verify PFD, GTC 1, and GTC 2 power on. (2) Verify MFD does not power on. c. Essential Bus Voltage ............23-25 VOLTS d.
Page 134 4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES (Continued) q. Emergency Egress Hammer ..........STOWED r. STARTER DISABLE Switch............ ENABLE 2. Left Fuselage a. Antennae ........CONDITION AND ATTACHMENT b. Wing/Fuselage Fairing ...............CHECK c. Baggage Door ..........CLOSED AND SECURE d.
Page 135 4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES (Continued) • N • Verify bolt located under the inboard edge of aileron is secured with safety wire. e. Aileron Gap Seal ....... CONDITION AND SECURITY f. Hinges, actuation arm, bolts, and cotter pins......SECURE 6.
Page 136 4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES (Continued) 9. Nose Gear, Propeller, and Spinner • WARNING • Keep clear of propeller rotation plane. Do not allow others to approach propeller. a. Tow Bar .............REMOVE AND STOW b. Strut..................CONDITION c.
Page 137: Before Engine Start
4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES (Continued) e. Wing Tip Static Wicks ..... CONDITION AND SECURITY 13.Left Wing Trailing Edge • N • Verify bolt located under the inboard edge of aileron is secured with safety wire.
Page 138: Engine Start
4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES Engine Start If the engine is warm, no priming is required. For the first start of the day and in cold conditions, prime will be necessary. Weak intermittent firing followed by puffs of black smoke from the exhaust stack indicates over-priming or flooding.
Page 139 4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES (Continued) 1. ALT 1 and ALT 2 Switches..............OFF 2. CAS Messages..................CHECK 3. Strobe Lights (STRB Switch) ..............ON 4. Power Lever ................OPEN ¼ INCH 5. Mixture..................... CUTOFF 6. Propeller Area..................CLEAR 7.
Page 140: Before Taxi
4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES Before Taxi When taxiing, directional control is accomplished with rudder deflection and intermittent braking (toe taps) as necessary. Proper braking practices are critical to avoid potential damage to the brakes. Pilots unaccustomed to free castering nose wheel steering may be inclined to “ride”...
Page 141: Before Takeoff
4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES Before Takeoff During cold weather operations, the engine should be properly warmed up before takeoff. In most cases this is accomplished when the oil temperature has reached at least 100 °F (38 °C). In warm or hot weather, precautions should be taken to avoid overheating during prolonged ground engine operation.
Page 142 4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES (Continued) 11.Alternator ...................CHECK a. Probe Heat ................... ON b. Landing Light (LAND Switch)............ON 12.Voltage....................CHECK 13.Probe Heat................AS REQUIRED • N • Probe Heat should be turned ON for flight into IMC, flight into visible moisture, or whenever ambient temperatures are 41 °F (5...
Page 143: Maximum Power Fuel Flow
4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES Maximum Power Fuel Flow Target fuel flow is indicated by the top of a dynamically calculated green arc displayed on the fuel flow gauge. Full Power target fuel flow should be maintained at the top of this arc by use of the mixture lever.
Page 144: Normal Takeoff
4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES Maximum demonstrated crosswind is 20 knots. With the ailerons fully deflected into the wind, accelerate the airplane to a speed slightly higher than normal while decreasing the aileron deflection as speed increases then - with authority - rotate to prevent possibly settling back to the runway while drifting.
Page 145: Climb
4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES Climb Normal climbs are performed flaps UP (0%) and full power at speeds 5 to 10 knots higher than best rate-of-climb speeds. These higher speeds give the best combination of performance, visibility and engine cooling.
Page 146: Cruise
4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES Cruise Normal cruising is performed between 55% and 85% power. The engine power setting and corresponding fuel consumption for various altitudes and temperatures can be determined by using the cruise data in Section 5.
Page 147: Cruise Leaning
4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES Cruise Leaning • CAUTION • If moving the mixture control from the full rich position only decreases the EGT from the full rich value, place the mixture control back in the full forward position and have the fuel system serviced.
Page 148: Descent
4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES Descent 1. Altimeter....................SET 2. Landing Lights (LAND Switch) .............. ON 3. Fuel Quantity ..................CHECK 4. Power Lever................AS REQUIRED 5. Mixture ..................AS REQUIRED 6. Seats and Seat Belts ................SECURE 7. Brake Pressure ...................CHECK Before Landing 1.
Page 149: Short Field Landing
4: N IRRUS ECTION ORMAL ROCEDURES SR20 ORMAL ROCEDURES Short Field Landing 1. Flaps ......................100% 2. Airspeed ..................... 78 KIAS 3. Power Lever ................AS REQUIRED After clear of obstacles: 4. Power Lever ..............REDUCE TO IDLE After touchdown: 5.
Page 150: After Landing
4: N ECTION ORMAL ROCEDURES IRRUS SR20 ORMAL ROCEDURES After Landing 1. Fuel Pump ....................OFF 2. Mixture ......LEAN TO OBTAIN MAXIMUM IDLE RPM 3. Flaps ......................UP 4. Lights..................AS REQUIRED 5. Probe Heat....................OFF • N • As the airplane slows, the rudder becomes less effective and taxiing is accomplished using differential braking.
Page 151: Stalls
4: N IRRUS ECTION ORMAL ROCEDURES SR20 TALLS Stalls Aircraft stall characteristics are conventional. Power-off stalls may be accompanied by a slight nose bobbing if full aft stick is held. Power-on stalls are marked by a high sink rate at full aft stick. Power-off stall speeds at...
Page 152: Environmental Conditions
4: N ECTION ORMAL ROCEDURES IRRUS SR20 NVIRONMENTAL ONDITIONS Environmental Conditions Cold Weather Operation • CAUTION • An engine that has been superficially warmed, may start and appear to run satisfactorily, but can be damaged from lack of lubrication due to the congealed oil blocking proper oil flow through the engine.
Page 153 4: N IRRUS ECTION ORMAL ROCEDURES SR20 NVIRONMENTAL ONDITIONS (Continued) 5. Power Lever ................OPEN ¼ INCH 6. Mixture..................... CUTOFF 7. Propeller Area..................CLEAR 8. Fuel Pump....................ON 9. Mixture..............ADVANCE TO RICH UNTIL STABLE FUEL FLOW IS INDICATED (3-5 SECONDS) •...
Page 154: Hot Weather Operation
4: N ECTION ORMAL ROCEDURES IRRUS SR20 NVIRONMENTAL ONDITIONS Hot Weather Operation Avoid prolonged engine operation on the ground. Fuel Pump must be ON for engine start and takeoff, and should be ON during climb for vapor suppression which could occur under hot ambient conditions or after extended idle.
Page 155: Noise Abatement
4: N IRRUS ECTION ORMAL ROCEDURES SR20 OISE BATEMENT Noise Abatement The following suggested procedures minimize environmental noise when operating the aircraft. • N • Do not follow these noise abatement procedures where they conflict with Air Traffic Control clearances or instructions, weather considerations, or wherever they would reduce safety.
Page 156 4: N ECTION ORMAL ROCEDURES IRRUS SR20 OISE BATEMENT Intentionally Left Blank 4-28 FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 157 5: P IRRUS ECTION ERFORMANCE SR20 Section 5: Performance Data Table of Contents Introduction..................3 Standard Charts .................. 3 Associated Conditions Affecting Performance ........3 Temperature Conversion..............4 OAT for International Standard Atmosphere (ISA) Condition.... 5 Pressure Conversion - Inches of Mercury to Millibars ....... 6 Fuel Quantity Conversion - U.S.
Page 158 5: P ECTION ERFORMANCE IRRUS SR20 Landing Distance - 100% Flaps............35 Landing Distance Table - Flaps 100%..........36 Landing Distance - 50% Flaps............37 Landing Distance Table - Flaps 50%..........38 Landing Distance - 0% Flaps............39 Landing Distance Table - Flaps 0%..........40...
Page 159: Introduction
5: P IRRUS ECTION ERFORMANCE SR20 NTRODUCTION Introduction Performance data in this section are presented for operational planning so that you will know what performance to expect from the airplane under various ambient and field conditions. Performance data are presented for takeoff, climb, and cruise (including range &...
Page 160: Temperature Conversion
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Temperature Conversion Temp to Convert Temp to Convert Temp to Convert °C or °F °C or °F °C or °F °C < > °F °C < > °F °C < > °F...
Page 161: Oat For International Standard Atmosphere (Isa) Condition
5: P IRRUS ECTION ERFORMANCE SR20 TANDARD HARTS OAT for International Standard Atmosphere (ISA) Condition Press -30 °C -15 °C +15 °C +30 °C °C °F °C °F °C °F °C °F °C °F 1000 2000 3000 4000 5000 -25 -13 -10...
Page 162: Pressure Conversion - Inches Of Mercury To Millibars
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Pressure Conversion - Inches of Mercury to Millibars Inches Of Inches Of Millibars Millibars Mercury Mercury 28.0 29.6 1002 28.1 29.7 1006 28.2 29.8 1009 28.3 29.9 1012 28.4 30.0 1016 28.5 30.1...
Page 163: Fuel Quantity Conversion - U.s. Gallons To Liters
5: P IRRUS ECTION ERFORMANCE SR20 TANDARD HARTS Fuel Quantity Conversion - U.S. Gallons to Liters • N • Fuel mass provided for reference assuming nominal 6.0 lb/gallon at 59 °F (15 °C). U.S. U.S. Gallons Lb (Kg) Gallons Lb (Kg)
Page 164: Weight Conversion - Pounds To Kilograms
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Weight Conversion - Pounds to Kilograms Pounds Kilograms Pounds Kilograms 2000 907.2 2700 1224.7 2100 952.5 2800 1270.1 2200 998.0 2900 1315.4 2300 1043.3 3000 1360.1 2400 1088.6 3100 1406.1 2500 1134.0 3150 1428.8...
Page 165: Distance Conversion: Feet To Meters
5: P IRRUS ECTION ERFORMANCE SR20 TANDARD HARTS Distance Conversion: Feet to Meters Feet Meters Feet Meters 1000 2000 3000 4000 1219 5000 1524 6000 1829 7000 2134 8000 2438 9000 2743 10,000 3048 P/N 44763-001 FAA APPROVED Original Issue...
Page 166: Length Conversion: Inches To Centimeters
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Length Conversion: Inches to Centimeters Inches Centimeters Inches Centimeters 2.54 50.8 5.08 76.2 7.62 101.6 10.16 12.70 142.4 15.24 177.8 17.78 203.2 20.32 228.6 22.86 25.40 27.94 30.48 5-10 FAA APPROVED P/N 44763-001...
Page 167: Airspeed Calibration
5: P IRRUS ECTION ERFORMANCE SR20 TANDARD HARTS Airspeed Calibration Normal Static Source Conditions: • Power for level flight or maximum continuous, whichever is less. • N • Indicated airspeed values assume zero instrument error. KCAS Flap Deflection KIAS Flaps 0%...
Page 168: Alternate Static Source
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Alternate Static Source Conditions: • Power for level flight or maximum continuous, whichever is less. • Heater, Defroster & Vents ..............ON • N • Indicated airspeed values assume zero instrument error. KCAS...
Page 169: Altitude Correction
5: P IRRUS ECTION ERFORMANCE SR20 TANDARD HARTS Altitude Correction Normal Static Source: Primary Flight Display Conditions: • Power for level flight or maximum continuous, whichever is less. • 3150 LB • N • Add correction to desired altitude to obtain indicated altitude to fly.
Page 170: Normal Static Source: Standby Altimeter
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Normal Static Source: Standby Altimeter Conditions: • Power for level flight or maximum continuous, whichever is less. • 3150 LB • N • Add correction to desired altitude to obtain indicated altitude to fly.
Page 171: Alternate Static Source: Primary Flight Display
5: P IRRUS ECTION ERFORMANCE SR20 TANDARD HARTS Alternate Static Source: Primary Flight Display Conditions: • Power for level flight or maximum continuous, whichever is less. • Heater, Defroster & Vents..............ON • N • Add correction to desired altitude to obtain indicated altitude to fly.
Page 172: Alternate Static Source: Standby Altimeter
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Alternate Static Source: Standby Altimeter Conditions: • Power for level flight or maximum continuous, whichever is less. • Heater, Defroster & Vents ..............ON • N • Add correction to desired altitude to obtain indicated altitude to fly.
Page 173: Stall Speeds
5: P IRRUS ECTION ERFORMANCE SR20 TANDARD HARTS Stall Speeds • N • KIAS values may not be accurate at stall. STALL SPEEDS AT IDLE Bank Angle Flaps UP Flaps 50% Flaps 100% KIAS KCAS KIAS KCAS KIAS KCAS 3150 lb - Most FWD C.G.
Page 174: Wind Components
5: P ECTION ERFORMANCE IRRUS SR20 TANDARD HARTS Wind Components Example: Runway Heading..................... 10° Wind Direction ....................60° Wind Velocity ..................15 Knots • N • The maximum demonstrated crosswind is 20 knots. Figure 5-1: Wind Components 0° 10° 20°...
Page 175: Takeoff Distance
5: P IRRUS ECTION ERFORMANCE SR20 AKEOFF ISTANCE Takeoff Distance Takeoff Weight 3150 lb (1429 kg) Conditions: • Winds ..................... Zero • Runway................Dry, Level, Paved • Flaps......................50% • Air Conditioner ..................OFF • Power..................Full Throttle • Speed Over 50 ft Obstacle..............81 KIAS •...
Page 176 5: P ECTION ERFORMANCE IRRUS SR20 AKEOFF ISTANCE Takeoff Weight: 3150 lb (1429 kg) TEMPERATURE ~°C Press Alt Distance Gnd Roll 1503 1623 1748 1877 2011 2150 1685 Total 2273 2443 2618 2799 2986 3179 2530 1000 Gnd Roll 1653...
Page 177: Takeoff Weight: 2600 Lb (1179 Kg)
5: P IRRUS ECTION ERFORMANCE SR20 AKEOFF ISTANCE Takeoff Weight: 2600 lb (1179 kg) Conditions: • Winds ..................... Zero • Runway................Dry, Level, Paved • Flaps......................50% • Air Conditioner ..................OFF • Power..................Full Throttle • Speed Over 50 ft Obstacle..............75 KIAS •...
Page 178 5: P ECTION ERFORMANCE IRRUS SR20 AKEOFF ISTANCE Takeoff Weight: 2600 lb (1179 kg) TEMPERATURE ~°C Press Alt Distance Gnd Roll 1061 1140 1221 1305 1023 Total 1408 1513 1621 1732 1848 1967 1566 1000 Gnd Roll 1004 1083 1166...
Page 179: Takeoff Climb Gradient
5: P IRRUS ECTION ERFORMANCE SR20 AKEOFF ISTANCE Takeoff Climb Gradient Conditions: • Power..................Full Throttle • Mixture........ Set Fuel Flow to Very Top of GREEN ARC • Flaps......................50% CLIMB GRADIENT - Feet per Nautical Mile Weight Press Alt...
Page 180: Takeoff Rate Of Climb
5: P ECTION ERFORMANCE IRRUS SR20 AKEOFF ISTANCE Takeoff Rate of Climb Conditions: • Power ..................Full Throttle • Mixture........Set Fuel Flow to Very Top of GREEN ARC • Flaps ......................50% • N • Aircraft with optional Air Conditioning System: Maximum rate of climb performance is reduced by approximately 75 feet per minute.
Page 181: Enroute Climb
5: P IRRUS ECTION ERFORMANCE SR20 NROUTE LIMB Enroute Climb Climb Gradient Conditions: • Power..................Full Throttle • Mixture........ Set Fuel Flow to Very Top of GREEN ARC • Flaps......................UP Weight Press Alt Climb CLIMB GRADIENT - Feet per Nautical Mile Speed TEMPERATURE ~°C...
Page 182: Enroute Rate Of Climb
5: P ECTION ERFORMANCE IRRUS SR20 NROUTE LIMB Enroute Rate Of Climb Conditions: • Power ..................Full Throttle • Mixture........Set Fuel Flow to Very Top of GREEN ARC • Flaps ......................UP • N • Aircraft with optional Air Conditioning System: Maximum rate of climb performance is reduced by approximately 75 feet per minute if system is ON.
Page 183: Enroute Rate Of Climb Vs Density Altitude
5: P IRRUS ECTION ERFORMANCE SR20 NROUTE LIMB Enroute Rate of Climb Vs Density Altitude Conditions: • Power..................Full Throttle • Mixture........ Set Fuel Flow to Very Top of GREEN ARC • Flaps......................UP Figure 5-2: Enroute Rate of Climb Vs Density Altitude...
Page 184: Time, Fuel, & Distance To Climb
5: P ECTION ERFORMANCE IRRUS , & D SR20 ISTANCE TO LIMB Time, Fuel, & Distance to Climb Conditions: • Power ..................Full Throttle • Mixture........Set Fuel Flow to Very Top of GREEN ARC • Weight ....................3150 LB • Winds .....................Zero •...
Page 185: Cruise Performance
5: P IRRUS ECTION ERFORMANCE SR20 RUISE ERFORMANCE Cruise Performance Conditions: • Mixture................Target Fuel Flow* • Weight....................2600 LB • Winds ..................... Zero • Shaded Cells: Cruise Pwr above 85% not recommended. *For power settings greater than 75% power, Best Power.
Page 186 5: P ECTION ERFORMANCE IRRUS SR20 RUISE ERFORMANCE ISA -30 °C ISA +30 °C Press Alt RPM MAP PWR KTAS GPH PWR KTAS GPH PWR KTAS GPH 6000 2700 23.4 82% 151 14.7 78% 154 14.1 74% 156 11.4 2500 23.4 75% 146 13.5 71% 148 11.7 68% 150 10.4 2500 22.3 70% 142 12.7 66% 144 11.0 63% 145...
Page 187: Range / Endurance Profile
5: P IRRUS ECTION ERFORMANCE SR20 ANGE NDURANCE ROFILE Range / Endurance Profile Conditions: • Weight....................3000 LB • Temperature................Standard Day • Winds ..................... Zero • Mixture..................See Tables • Total Fuel ..................56 Gallons • N • Fuel Remaining For Cruise accounts for 10.1 gallons for 45 minutes IFR reserve fuel at 75% power and fuel burn for descent.
Page 188 5: P ECTION ERFORMANCE IRRUS SR20 ANGE NDURANCE ROFILE 65% POWER Press Climb Fuel Airspeed Fuel Endurance Range Specific Fuel Remaining Flow Range For Cruise KTAS HOURS NM/GAL 47.9 10.9 12.4 2000 47.2 10.7 12.9 4000 46.4 10.5 13.4 6000 45.5...
Page 189: Balked Landing
5: P IRRUS ECTION ERFORMANCE SR20 ALKED ANDING Balked Landing Climb Gradient Conditions: • Power..................Full Throttle • Mixture........ Set Fuel Flow to Very Top of GREEN ARC • Flaps.......................100% • N • This chart is required data for certification. However, significantly...
Page 190: Balked Landing Rate Of Climb
5: P ECTION ERFORMANCE IRRUS SR20 ALKED ANDING Balked Landing Rate of Climb Conditions: • Power ..................Full Throttle • Mixture........Set Fuel Flow to Very Top of GREEN ARC • Flaps .......................100% • N • This chart is required data for certification. However, significantly...
Page 191: Landing Distance
5: P IRRUS ECTION ERFORMANCE SR20 ANDING ISTANCE Landing Distance Landing Distance - 100% Flaps Conditions: • Winds ..................... Zero • Runway................Dry, Level, Paved • Weight................3150 lb (1429 kg) • Power......................Idle • Speed Over Obstacle...............79 KIAS The following factors are to be applied to the computed landing distance for the noted condition.
Page 192: Landing Distance Table - Flaps 100
5: P ECTION ERFORMANCE IRRUS SR20 ANDING ISTANCE Landing Distance Table - Flaps 100% TEMPERATURE ~°C Press Distance Alt FT Gnd Roll Total 2557 2609 2663 2717 2773 2829 2636 1000 Gnd Roll Total 2610 2665 2722 2779 2838 2898...
Page 193 5: P IRRUS ECTION ERFORMANCE SR20 ANDING ISTANCE Landing Distance - 50% Flaps Conditions: • Winds ..................... Zero • Runway................Dry, Level, Paved • Weight................3150 lb (1429 kg) • Power......................Idle • Speed Over Obstacle...............82 KIAS The following factors are to be applied to the computed landing distance for the noted condition.
Page 194 5: P ECTION ERFORMANCE IRRUS SR20 ANDING ISTANCE Landing Distance Table - Flaps 50% TEMPERATURE ~°C Press Distance Alt FT Gnd Roll 1029 1066 1104 1141 1179 1217 1085 Total 2704 2768 2833 2899 2966 3033 2800 1000 Gnd Roll...
Page 195 5: P IRRUS ECTION ERFORMANCE SR20 ANDING ISTANCE Landing Distance - 0% Flaps Conditions: • Winds ..................... Zero • Runway................Dry, Level, Paved • Weight................3150 lb (1429 kg) • Power......................Idle • Speed Over Obstacle...............87 KIAS The following factors are to be applied to the computed landing distance for the noted condition.
Page 196 5: P ECTION ERFORMANCE IRRUS SR20 ANDING ISTANCE Landing Distance Table - Flaps 0% TEMPERATURE ~°C Press Distance Alt FT Gnd Roll 1185 1228 1272 1315 1358 1402 1250 Total 2971 3037 3105 3174 3243 3314 3071 1000 Gnd Roll...
Page 197 6: W IRRUS ECTION EIGHT AND ALANCE SR20 Section 6: Weight and Balance Table of Contents Introduction..................3 Weight and Balance Record..............3 Weight and Balance Data..............3 Loading Instructions ................4 Weight and Balance Loading Form ............. 5 Loading Data ..................6 Moment Values ...................
Page 198 6: W ECTION EIGHT AND ALANCE IRRUS SR20 Intentionally Left Blank FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 199: Introduction
6: W IRRUS ECTION EIGHT AND ALANCE SR20 NTRODUCTION Introduction This section describes the procedure for calculating the weight and moment for various operations. A comprehensive list of all equipment available for this airplane is included at the back of this section.
Page 200: Loading Instructions
6: W ECTION EIGHT AND ALANCE IRRUS SR20 EIGHT AND ALANCE ECORD Loading Instructions It is the responsibility of the pilot to ensure that the airplane is properly loaded and operated within the prescribed weight and center of gravity limits. The following information enables the pilot to calculate the total weight and moment for the loading.
Page 201: Weight And Balance Loading Form
6: W IRRUS ECTION EIGHT AND ALANCE SR20 EIGHT AND ALANCE OADING Weight and Balance Loading Form • N • The Takeoff Condition Weight must not exceed 3150 lb. The Takeoff Condition Moment must be within the Minimum Moment to Maximum Moment range at the Takeoff Condition Weight.
Page 202: Loading Data
6: W ECTION EIGHT AND ALANCE IRRUS SR20 OADING Loading Data Use the following chart or table to determine the moment/1000 for fuel and payload items to complete the Loading Form. Figure 6-3: Loading Chart Fuel Fwd Pass Loading Chart...
Page 203: Moment Values
6: W IRRUS ECTION EIGHT AND ALANCE SR20 OMENT ALUES Moment Values Use the following chart or table to determine if the weight and moment from the completed Weight and Balance Loading Form (Figure 6-2) are within limits. Figure 6-4: Moment Limits Chart...
Page 204: Weight & Balance Record
6: W ECTION EIGHT AND ALANCE IRRUS & B SR20 EIGHT ALANCE ECORD Weight & Balance Record Use this form to maintain a continuous history of changes and modifica- tions to airplane structure or equipment affecting weight and balance: Figure 6-5: Weight & Balance Record Form Serial Num: Reg.
Page 205 7: S IRRUS ECTION YSTEMS ESCRIPTION SR20 Section 7: Systems Description Table of Contents • N • Content for Section 7: Systems Description is located in the Pilot’s Information Manual (PIM). P/N 44763-001 NOT FAA APPROVED Original Issue 01 Aug 2023...
Page 206 7: S ECTION YSTEMS ESCRIPTION IRRUS SR20 Intentionally Left Blank NOT FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 207 Airplane Records and Certificates............4 Airworthiness Directives ..............5 Airplane Inspection Periods..............5 Annual Inspection................5 100-Hour Inspection ................6 Cirrus Progressive Inspection Program..........6 Ground Handling ................. 7 Application of External Power ............7 Towing....................8 Taxiing....................9 Parking .................... 10 Tie Down ..................
Page 208 8: H ECTION ANDLING AND ERVICING IRRUS SR20 Care of Graphics ................25 Cleaning Interior Surfaces ..............29 Interior Windshield and Windows ............ 29 Instrument Panel and Electronic Display Screens......30 Headliner and Trim Panels .............. 30 Leather Upholstery and Seats ............31 Carpets ....................
Page 209: Introduction
This section provides general guidelines for handling, servicing, and maintaining your aircraft. In order to ensure continued safe and efficient operation of your airplane, keep in contact with your Authorized Cirrus Service Center to obtain the latest information pertaining to your aircraft.
Page 210: Obtaining Publications
Service Bulletin. Pay careful attention to the Service Advi- sory information. Obtaining Publications Airplane Flight Manuals and aircraft service publications can be obtained from Cirrus at www.cirrusaircraft.com, or the Cirrus Connection at www.cirrusconnection.com. Airplane Records and Certificates The Federal Aviation Administration (FAA) requires that certain data, certificates, and licenses be displayed or carried aboard the airplane at all times.
Page 211: Airworthiness Directives
ADs are mandatory changes and must be complied with within a time limit set forth in the AD. Operators should periodically check with Cirrus Service Centers or A&P mechanic to verify receipt of the latest issued AD for their airplane.
Page 212: 100-Hour Inspection
Airframe and Powerplant (A&P) mechanic holding an Inspection Authorization (IA). Annual inspections can only be performed by facilities approved by Cirrus. The inspection is listed, in detail, in Chapter 5 of the Airplane Maintenance Manual.
Page 213: Ground Handling
8: H IRRUS ECTION ANDLING AND ERVICING SR20 ROUND ANDLING Ground Handling Application of External Power An external power receptacle, located just aft of the cowl on the left side of the airplane, permits the use of an external power unit for cold weather starting and maintenance procedures.
Page 214: Towing
8: H ECTION ANDLING AND ERVICING IRRUS SR20 ROUND ANDLING Towing The airplane may be moved on the ground by the use of the nose wheel steering bar that is stowed in the rear baggage compartment or by power equipment that will not damage or excessively strain the nose gear assembly.
Page 215: Taxiing
8: H IRRUS ECTION ANDLING AND ERVICING SR20 ROUND ANDLING Taxiing Before attempting to taxi the airplane, ground personnel should be instructed and authorized by the owner to taxi the airplane. Instruction should include engine starting and shutdown procedures in addition to taxi and steering techniques.
Page 216 8: H ECTION ANDLING AND ERVICING IRRUS SR20 ROUND ANDLING If the airplane will be parked for 30 days or more, pull the CONV SYS 1 and CONV SYS 2 circuit breaker to prevent excessive discharge from battery 1. To Park Airplane Position airplane on level surface and headed into the wind.
Page 217: Tie Down
8: H IRRUS ECTION ANDLING AND ERVICING SR20 ROUND ANDLING Tie Down The airplane should be moored for immovability, security, and protection. FAA Advisory Circular AC 20-35C, Tie-down Sense, contains additional information regarding preparation for severe weather, tie down, and related information.
Page 218: Servicing
8: H ECTION ANDLING AND ERVICING IRRUS SR20 ERVICING Servicing Landing Gear Servicing The main landing gear wheel assemblies use 15 x 6.00 x 6 tubeless tires. The nose wheel assembly uses a 5.00 x 5 tubeless tire. Always keep tires inflated to the rated pressure to obtain optimum perfor- mance and maximum service.
Page 219: Tire Inflation
8: H IRRUS ECTION ANDLING AND ERVICING SR20 ERVICING Tire Inflation For maximum service from the tires, keep them inflated to the proper pres- sure. When checking tire pressure, examine the tires for wear, cuts, nicks, bruises and excessive wear.
Page 220 8: H ECTION ANDLING AND ERVICING IRRUS SR20 ERVICING It is recommended that the oil be changed every 50 hours, or every four months, whichever occurs first, and sooner under unfavorable operating conditions. Refer to Section 2, Powerplant Limitations, for approved oil grades.
Page 221: Fuel System Servicing
8: H IRRUS ECTION ANDLING AND ERVICING SR20 ERVICING Fuel System Servicing Observe all safety precautions required when handling gasoline. Fuel fillers are located on the forward slope of the wing. Each wing holds a maximum of 29.3 U.S. gallons. When using less than the standard 58.5 gallon capacity, fuel should be distributed equally between each side.
Page 222 8: H ECTION ANDLING AND ERVICING IRRUS SR20 ERVICING To Refuel Airplane • CAUTION • Aviation grade 100 LL (blue) or 100 (green) fuel is the minimum octane approved for use in this airplane. Place fire extinguisher near fuel tank being filled.
Page 223: Fuel Contamination And Sampling
8: H IRRUS ECTION ANDLING AND ERVICING SR20 ERVICING Fuel Contamination and Sampling Typically, fuel contamination results from foreign material such as water, dirt, rust, and fungal or bacterial growth. Additionally, chemicals and addi- tives that are incompatible with fuel or fuel system components are also a source of fuel contamination.
Page 224: Battery Service
8: H ECTION ANDLING AND ERVICING IRRUS SR20 ERVICING Battery Service The aircraft is delivered with a maintenance-free, rechargeable, sealed, lithium-ion primary battery. Battery #1 is mounted to the bottom right side of the instrument panel and access is gained by removing the lower kick panel.
Page 225: Elt Servicing
8: H IRRUS ECTION ANDLING AND ERVICING SR20 ERVICING ELT Servicing The ELT batteries must be inspected in accordance with the Airplane Maintenance Manual, 5-20 - Scheduled Maintenance Checks. The ELT batteries must be replaced upon reaching the date stamped on the batteries, after an inadvertent activation of unknown duration, or when- ever the batteries have been in use for one cumulative hour.
Page 226 8: H ECTION ANDLING AND ERVICING IRRUS SR20 ERVICING multiple flashes separated by 1-second periods, will begin to display after approximately 1 second. Flash Codes displayed with the associated conditions are as follows: 1-Flash: Indicates that the system is operational and that no error conditions were found.
Page 227: Cleaning Exterior Surfaces
8: H IRRUS ECTION ANDLING AND ERVICING SR20 LEANING XTERIOR URFACES Cleaning Exterior Surfaces • CAUTION • Prior to cleaning, place the airplane in a shaded area to allow the surfaces to cool. The airplane should be washed with a mild soap and water. Harsh abrasives or alkaline soaps or detergents could make scratches on painted or plastic surfaces or could cause corrosion of metal.
Page 228: Enhanced Vision System Sensor Lenses (Optional)
8: H ECTION ANDLING AND ERVICING IRRUS SR20 LEANING XTERIOR URFACES To Clean Exterior Windshield and Windows Remove grease or oil using a soft cloth saturated with kerosene then rinse with clean, fresh water. • N • Wiping with a circular motion can cause glare rings. Use an up and down wiping motion on the windshield in the direction of the airflow to prevent this.
Page 229: Landing Gear
8: H IRRUS ECTION ANDLING AND ERVICING SR20 LEANING XTERIOR URFACES cially heavy dirt and grease deposits, it may be necessary to brush areas that were sprayed. • CAUTION • Do not spray solvent into the alternator, vacuum pump, starter, or induction air intakes.
Page 230: Recommended Exterior Cleaning Products
8: H ECTION ANDLING AND ERVICING IRRUS SR20 LEANING XTERIOR URFACES Recommended Exterior Cleaning Products Cleaning Application Cleaning Product Supplier Painted Exterior Pure Carnauba Wax Any Source Mothers California Gold Mothers Polish Pure Carnauba Wax RejeX High Gloss Corrosion Protective Finish...
Page 231: Care Of Graphics
8: H IRRUS ECTION ANDLING AND ERVICING SR20 LEANING XTERIOR URFACES Care of Graphics Graphics require care similar to any fine paint finish. Use high quality products designed specifically for use on automobile finishes. Use products in accordance with the manufacturer’s instructions.
Page 232 8: H ECTION ANDLING AND ERVICING IRRUS SR20 LEANING XTERIOR URFACES To Spot Clean Difficult Contaminants Difficult contaminants such as bugs, bird droppings, or tree sap may require spot cleaning. • CAUTION • To prevent scratching the graphic, refrain from rough scrubbing and the use of abrasive tools.
Page 233 8: H IRRUS ECTION ANDLING AND ERVICING SR20 LEANING XTERIOR URFACES Graphic Restoration If typical cleaning methods fail to produce satisfactory results, refer to the recommended restoration products and mixtures below to help preserve the condition of the graphics on your aircraft.
Page 234 8: H ECTION ANDLING AND ERVICING IRRUS SR20 LEANING XTERIOR URFACES Recommended Graphic Restoration Products and Mixtures Film or Finish Type Cleaning Product or Mixture Supplier Smooth Gloss 3M™ Perfect-it™ Show Car Paste 3M Company Wax 39526 Meguiar's Gold Class™ Carnuaba...
Page 235: Cleaning Interior Surfaces
8: H IRRUS ECTION ANDLING AND ERVICING SR20 LEANING NTERIOR URFACES Cleaning Interior Surfaces Seats, carpet, upholstery panels, and headliners should be vacuumed at regular intervals to remove surface dirt and dust. While vacuuming, use a fine bristle nylon brush to help loosen particles.
Page 236: Instrument Panel And Electronic Display Screens
8: H ECTION ANDLING AND ERVICING IRRUS SR20 LEANING NTERIOR URFACES Instrument Panel and Electronic Display Screens The instrument panel, control knobs, and plastic trim need only to be wiped clean with a soft, damp cloth. The multifunction display, primary...
Page 237: Leather Upholstery And Seats
For deeper cleaning, start with mix of mild detergent and water and, if necessary, work your way up to the products available from Cirrus for more stubborn marks and stains. Do not use soaps as they contain alka- line which will alter the leather’s pH balance and cause the leather to age...
Page 238 8: H ECTION ANDLING AND ERVICING IRRUS SR20 LEANING NTERIOR URFACES Recommended Interior Cleaning Products Cleaning Application Cleaning Product Supplier Interior Windshield Plastic and Glass Prist Aerospace and Windows Cleaner Display Screens Optimax PhotoDon Cabin Interior Mild Dishwasher Any Source...
Page 239 9: L IRRUS ECTION OG OF UPPLEMENTS SR20 Section 9: Log of Supplements Table of Contents As Required P/N 44763-001 NOT FAA APPROVED Original Issue 01 Aug 2023...
Page 240 This Log of Supplements shows all Cirrus Supplements available for the aircraft at the corresponding date of the revision level shown in the lower left corner.
Page 241 NFORMATION SR20 Section 10: Safety Information Table of Contents Introduction..................3 Cirrus Airframe Parachute System (CAPS)......... 3 Deployment Scenarios ..............4 Mid-Air Collision ................4 Structural Failure ................4 Loss of Control ................4 Landing Required in Terrain not Permitting a Safe Landing.... 5 Pilot Incapacitation ................
Page 242 10: S ECTION AFETY NFORMATION IRRUS SR20 Intentionally Left Blank 10-2 NOT FAA APPROVED P/N 44763-001 01 Aug 2023 Original Issue...
Page 243: Introduction
Cirrus also recommends that pilots discuss CAPS deployment scenarios with instructors as well as fellow pilots through forums such as the Cirrus Owners and Pilots Association. In the event of a spin or loss of aircraft control, immediate CAPS activation is required. (See Section 3) In other situations, CAPS activation is at the informed discretion of the pilot in command.
Page 244: Deployment Scenarios
10: S ECTION AFETY NFORMATION IRRUS (CAPS) SR20 IRRUS IRFRAME ARACHUTE YSTEM CAPS. It is also important to note that CAPS has been activated by pilots at speeds in excess of 180 knots on multiple occasions with successful outcomes. While the best speed to activate CAPS is below 133 knots indi- cated airspeed, a timely activation is most important for loss of control situ- ations.
Page 245: Landing Required In Terrain Not Permitting A Safe Landing
CAPS activation is strongly recommended. Numerous fatalities that have occurred in Cirrus aircraft accidents likely could have been avoided if pilots had made the timely decision to deploy CAPS.
Page 246: Deployment Attitude
10: S ECTION AFETY NFORMATION IRRUS (CAPS) SR20 IRRUS IRFRAME ARACHUTE YSTEM feet AGL. A low altitude deployment leaves little or no time for the aircraft to stabilize under the canopy or for the cabin to be secured and increases the risk of injury or death.
Page 247: Door Position
10: S IRRUS ECTION AFETY NFORMATION SR20 (CAPS) IRRUS IRFRAME ARACHUTE YSTEM Door Position For most situations, it is best to leave the doors latched and use the time available to transmit emergency calls, shut down systems, and get into the Emergency Landing Body Position well before impact.
Page 248: Post-Impact Fire
10: S ECTION AFETY NFORMATION IRRUS (CAPS) SR20 IRRUS IRFRAME ARACHUTE YSTEM Post-Impact Fire If there is no fire prior to touchdown and the pilot is able to shut down the engine, fuel, and electrical systems, there is less chance of a post impact fire.

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