Summary Aircraft Data 2009 Cirrus (SR20) N511RT
Cirrus SR20 G3 · Systems Description
Overview
This document provides a comprehensive systems description for the 2009 Cirrus SR20 G3, specifically for aircraft N511RT. It includes critical specifications such as weight limits, fuel capacity, and engine details. The document is intended for pilots and aviation enthusiasts who require detailed knowledge of the aircraft's systems and performance characteristics. Key information includes the electrical system specifications, avionics suite, and various performance speeds essential for safe operation. The document serves as a reference for understanding the aircraft's capabilities and limitations, ensuring pilots can operate the SR20 G3 effectively and safely.
- Empty Weight: 1048.23 lbs
- Max T/O Weight: 3050 lbs
- Useful Load: 1000 lbs
- Fuel Capacity: 58.5 gallons (usable: 56 gallons)
- Max Crosswind Component: 20 knots at 90 degrees
- Minimum CAPS Deployment Altitude: 600 feet AGL
- VNE: 200 KIAS, VNO: 163 KIAS, VY: 96 KIAS
Document
Source
Originally published by rochesterair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Systems Description
- Year
- 2009
- Pages
- 1
- File size
- 636 KB
- Publisher
- rochesterair.com
Common. Rarer than 17% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cirrus SR20 G3.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Aircraft Specifications
The 2009 Cirrus SR20 G3 has an empty weight of 1048.23 lbs, a maximum takeoff weight of 3050 lbs, and a useful load of 1000 lbs. It has a fuel capacity of 58.5 gallons, with 56 gallons being usable.
Electrical System
The aircraft features two alternators: the first is a 28 V 75 amp alternator, and the second is a 28 V 40 amp alternator. The battery specifications include a 24 V 10 amp hour battery and a 12 V 7 amp hour battery.
Performance Speeds
The document lists various V-speeds for the Cirrus SR20 G3: VNE is 200 KIAS, VNO is 163 KIAS, and VY is 96 KIAS. The maximum crosswind component is 20 knots at 90 degrees to the runway.
CAPS Deployment
The minimum altitude for CAPS deployment is 600 feet AGL, with a maximum deployment speed of 133 KIAS.
Go-Around Procedure
In the event of a go-around, the procedure is to apply full power, pitch for a normal climb, reduce flaps to 50%, and once a positive rate of climb is established, retract flaps.
Safety notes
- Ensure oil level is between 6 and 8 quarts before flight.
- Monitor engine during soft field takeoff.
Full document text
Summary Aircraft Data 2009 Cirrus (SR20) N511RT Empty Weight (lbs) Max T/O Weight (lbs) Useful Load (lbs) Fuel Capacity (gals) Useable Fuel (gals) 1048.23 3050 1000 58.5 56 Electrical System Engine Oil Alternator 1 28 V 75 amp 200HP Min level = 6 qts Alternator 2 28V 40 amp IO-360-ES Max level = 8 qts Battery 1 24 V 10 amp hr. Battery 2 12 V 7 amp hr. Normal Category Load Factor: Flaps up 3.8g, -1.9g, Flaps 50% 1.9g,0g, and Flaps 100% 1.9g,0g Avionics Suite: Garmin G1000 with Perspective Package V – Speeds KIAS: Standard Traffic Pattern VNE = 200 VNO = 163 Vfe= 50% flaps 119 100% 104 VA (max T/O weight) = 120 VY = 96 VX = 83 VG = 99 VR = 70 VS1 = 69 V0= 130 Minimum CAPS Deployment Altitude: 600’ AGL Max CAPS Deployment Speed: Vpd= 133 Maximum Crosswind Component = 20 knots @ 90 deg to runway. GO-AROUND: Full Power, pitch for normal climb, reduce flaps to 50% and once positive rate of climb established retract flaps. Commercial Maneuvers Speeds Short field Takeoff Rotate at 65. Initial climb 77. With obstacle pitch for obstacle clearance speed. Without obstacle pitch for VX or VY as appropriate. Soft Field Takeoff Keep the stick back, full power, and monitor engine. Rotate at slowest speed practical. Release back pressure and climb out at 85 kts. % Power KIAS Flaps Trim Downwind 40% 100 NONE As Req Abeam Touchdown Pt. 25% 100 50% As Reg Base 25% 90 50% - 100% As Req Final As Req. 78 100% As Req Maneuver Entry Speed KIAS Chandelle 130 Lazy Eight 130 Steep Turn (45 – 50 deg bank) 130