Cirrus SR 20

Number of Active Aircraft: 786 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1875 lbs
Max Weight 3000 lbs
Useful Load: 1125 lbs
Engine Name
Engine Number 1
Horsepower 200 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 17500 ft
Max Fuel 60 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 156 kts
GPH (75% BHP): 11
MPG (75% BHP) 14.2
Range (75% BHP): 745 nm
Fuel Cost Per Seat Mile 0.11 $
Fuel Cost Per Hour 66 $
MPG per 1000 lbs of Payload 15.95
F-T (Speed^2/FuelBurn) 22.1 HP
F-T Payload 24.9 kts
MPH To HP: 7.8 kts
T/O Roll - T/O over 50 FT OBST 1940 ft / 2734 ft

SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00143BO Installation of Avidyne Corporation model 700-00004-XXX-( ) multi-function display. Amended 6/25/2002
SA00152BO Installation of Avidyne Engine Instrument Sensor Interface Unit part number 200-00031-000. Issued 6/25/2002
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00166BO Installation of Avidyne Corporation primary flight display p/n 700-00006-000 and Magnetometer/OAT sensor p/n 700-00011-000. Issued 2/21/2003
SA00199BO Installation of Aerox Oxygen System in accordance with Aviation Oxygen Systems Inc. Drawing No. 4110-100 Rev. A dated June 19 2004 or later FAA-approved revisions.  Amended 1/10/2006
SA00243BO (1 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00269BO (2 OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00282BO Installation of Avidyne Corporation Entegra Integrated Flight Display System Amended 4/4/2013
SA00290BO (PAGE 1 ) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010
SA00296BO Installation of:  Amended 6/27/2013
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00780SE (PAGE 3) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00954SE (2 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA01009SE Installation of modified landing and taxi light system. Manufactured in accordance with Manufacturing Drawing List #1 Revision 1 dated August 27 2001 or later FAA approved revision. Installed and maintained in accordance with Installation Data List #1 Revision 1 dated August 27 2001 or later FAA approved revision. Issued 10/24/2001
SA01016SE Installation of an engine control lever friction bolt retainer Issued 11/14/2001
SA01040SE Installation of EMM-35 engine monitoring system installed using Arnav document Engine Monitoring Accessing Kit p/n 570-1210 Rev D dtd 10/18/02 or later rev. EMM-35 must be manufactured using TSO authorization for TSO C113. Amended 7/18/2002
SA01071SE Installation of vacuum pump and battery cooling system. Installed and maintained in accordance with Installation Data List #1 Revision 0 dated February 10 2002 or later FAA approved revision. Issued 4/4/2002
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01170LA : Installation of Sandel Avionics SN3308 Navigation Display Unit in accordance with FAA Approved Sandel Avionics Master Drawing List Document No. ST8691LA-A-01 Revision B Reissued 11/10/2011
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01232SE Installation of a Semi-Portable Oxygen System. Amended 5/7/2007
SA01234WI-D Installation of Bendix/King KMH 880 Multi-Hazard Awareness System or Bendix/King KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS). Issued 4/16/2004
SA01240SE (3 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006
SA01285SE The manufacture of a Cirrus sunvisor system Issued 10/27/2003
SA01304WI Installation of the Concorde CB24-11M or CB24-11MXC Lead Acid Battery or RG24-11M or RG24-15M VRSLA Battery. Amended 11/1/2012
SA01355WI-D Installation of the Bendix/King KR 87 ADB and/or the KN 62A DME. Reissued 4/4/2006
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (2 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01695SE (2 OF 5) Installation of an antenna Amended 2/15/2007
SA01708SE Installation of the fixed oxygen system. Amended 4/13/2010
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01734SE (PG 4) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01800SE (PG 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01861SE (PAGE 2)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01870CH Installation of McCauley Propeller Systems 3-blade propeller model D3A34C443/78CYA-0 with spinner no. D7779-3 assembly. Reissued 7/19/2006
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02033AT (PAGE 6) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008 0:00
SA02110CH (PAGE 2) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02216SE Removal of mechanical link between engine throttle control and propeller RPM control. Installation of a separate RPM control lever linkage between Cirrus RPM cable/cam followers center console to accommodate three-lever configuration new knobs for all levers and new installation hardware (nuts bolts etc). Amended 6/15/2012
SA02217AK (1 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004
SA02247SE Removal of rear seats and installation of cargo shelf and restraint system controlled by Cirrus Master Drawing List (MDL) TAG-CRT-205 Revision B dated October 23 2012 or later Federal Aviation Administration (FAA) approved revision. Reissued 12/21/2012
SA02268CH (PAGE 2) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 3) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02329AK Installation of a fixed-mounted Max-Viz Amended 7/10/2012
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 3) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02558CH Installation of a L-3 Communications Avionics Systems SmartDeck Flight Guidance and Display System Issued 5/21/2008
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 1) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02924CH Installation of M-T Propeller model MTV-14-D/195-30( ) 4 bladed propeller.  Amended 9/27/2013
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA03407AT Installation of Alakai Passive Amended 11/18/2008
SA03962AT Installation of Continental Motors Inc. TSIO-550-N engine on SR22 aircraft previously modified by STC SA10588SC Issued 4/19/2012
SA09541AC-D Installation of S-TEC System 55X Automatic Flight Guidance System Roll Servo  Amended 12/14/2006
SA10195SC Installation of an engine driven vapor cycle air conditioning system Reissued 5/17/2013
SA10236SC (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10532SC Installation of XM Satellite Radio Wireless equipment. Issued 5/15/2006
SA10588SC Installation of modified Teledyne Continental Motors IO-550-N engine equipped with turbonormalizing system. Issued 11/8/2006
SA10675SC Installation of Teledyne Continental Motors IOF-550-N engine. Issued 3/15/2004
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA10925SC Installation of BAR Air LLC supercharged Teledyne Continental Motors IO-550-N Engines in Cirrus Design SR22 aircraft.  Reissued 11/1/2010
SA10980SC Installation of cowl louvers and louver covers Cirrus SR22 aircraft  Issued 8/24/2010
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA2586NM (PAGE 3) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5581SW Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. Amended 9/30/2002
SA593CH (2 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Limitations
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)