AAFC SR20 Quick Reference Sheet
Cirrus SR20 G7 · V Speeds Reference
Overview
The AAFC SR20 Quick Reference Sheet provides essential operational and performance information for the Cirrus SR20 G7 aircraft. It is designed for pilots and aviation enthusiasts who require quick access to critical data regarding the aircraft's engine specifications, operational limits, and V-speeds. This document serves as a handy reference for flight planning and in-flight operations, ensuring that pilots can make informed decisions based on accurate and concise information.
- Engine: Lycoming IO-390-C3B6, 215 HP
- Maximum Gross Takeoff Weight: 3150 lbs
- Usable Fuel Capacity: 56 gallons
- Vso: 62 KIAS, Vs: 71 KIAS, VR: 71-75 KIAS
- Crosswind Limit: 20 KTS
Document
Source
Originally published by aeroatlanta.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- V Speeds Reference
- Pages ·
- 3
- File size ·
- 114 KB
- Publisher ·
- aeroatlanta.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp) ·
- 215
- Engine model ·
- Lycoming IO-390-C3B6
- Fuel capacity (gal) ·
- 56
- Max takeoff weight (lb) ·
- 3,150
Performance
- Max crosswind (kt) ·
- 20
V-speeds
- VR ·
- 75
- VX ·
- 81
- VY ·
- 96
- VFE ·
- 150
- VNE ·
- 201
- VNO ·
- 164
- VS1 ·
- 71
- VSO ·
- 62
Weight & balance
- Baggage allowance (lb) ·
- 130
- Max takeoff weight (lb) ·
- 3,150
What is the AAFC SR20 Quick Reference Sheet?
The AAFC SR20 Quick Reference Sheet is a v speeds reference for the Cirrus SR20 G7.
How many pages is the AAFC SR20 Quick Reference Sheet?
The copy of the AAFC SR20 Quick Reference Sheet on file runs 3 pages.
Where does the AAFC SR20 Quick Reference Sheet come from?
This copy of the AAFC SR20 Quick Reference Sheet was originally published by aeroatlanta.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the Cirrus SR20 G7.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Cirrus SR20 G7manuals & documents
- Weight & Balance for Cirrus SR20 G7Weight And Balance
- 2025 SR SERIES G7 / SR20Weight And Balance
- 2025 SR SERIES G7 / SR20Weight And Balance
- BEFA Cirrus SR20 Information Manual and WorkbookPerformance Data
- Cirrus SR20 G7 Weight & BalanceWeight And Balance
- PILOT’S CHECKLIST SR20WITH CIRRUS PERSPECTIVE+ AVIONICSChecklist
- PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for the CIRRUS DESIGN SR20Pilot's Operating Handbook
- CIRRUS SR20 NORMAL CHECKLISTPilot's Operating Handbook
- Cirrus SR20 G7 Systems DescriptionSystems Description
In this document
Engine Information
The Cirrus SR20 G7 is powered by a Lycoming IO-390-C3B6 engine, which is fuel-injected, horizontally opposed, air-cooled, and naturally aspirated. It delivers 215 horsepower and has an oil capacity of 7 quarts. The maximum gross takeoff weight for the aircraft is 3150 lbs, and the maximum baggage compartment loading is 130 lbs.
Operational Specifications
The aircraft has a usable fuel capacity of 56 gallons (58.5 gallons total). Pilots must switch fuel tanks approximately every 20-25 minutes to maintain balance, with a CAS message triggered at a 7.5-gallon imbalance. Acceptable fuel types include 100LL and 100 octane. The aircraft is equipped with two fuel pumps: an engine-driven pump and an auxiliary electric pump, which must be used during critical phases of flight.
V-Speeds
The document lists important V-speeds for the Cirrus SR20 G7, including Vso at 62 KIAS, Vs at 71 KIAS, VR at 71-75 KIAS, VX at 81 KIAS, and VY at 96 KIAS. The maximum flap extended speed (VFE) is 150 KIAS (first notch) and 110 KIAS (second notch). The maximum operating speed (VO) is 133 KIAS, with VNO at 164 KIAS, VNE at 201 KIAS, and VG at 100 KIAS. The crosswind limit for the aircraft is 20 knots.
Safety notes
- Ensure electric fuel pump is on during critical phases of flight such as takeoff and landing.
- Set electric pump off and lean mixture after landing.
Full document text
AAFC SR20 Quick Reference Sheet Engine Information • Lycoming IO-390-C3B6 • Fuel Injected, Horizontally Opposed, Air Cooled, Naturally Aspirated, Direct Drive, 215 HP • Oil Capacity – 7 quarts • Maximum Gross Takeoff Weight – 3150 lbs • Maximum Baggage Compartment Loading – 130 lbs Operational Specifications • 56 Gallons Usable Fuel (58.5 Total) o Tabs – 26 gallons • Must switch fuel tanks – expect a fuel tank switch every 20-25 minutes o CAS message triggered at 7.5 gallon imbalance if tank is not switched • 100LL and 100 are acceptable fuel sources • Two pumps o Engine driven o Auxiliary (electric) – Electric must be used during priming, takeoff, landing, switching tanks, maneuvering, climbing, & descending **The “before landing checklist” should include setting the mixture as required and having the electric pump on. **Before taxi and after landing you should set the electric pump off and lean the mixture to max RPM. Maneuver Configurations • Steep Turns: 60% Power – 120 KIAS • Ground Reference Maneuvers: 50% Power – 100 KIAS • Slow Flight/Stalls: 20-25% Power – 12” MP – <100 KIAS • Downwind: 50% Power • Abeam Touchdown: 25% Power – 50% Flaps – 100 KIAS • Base: Power as required – 100% Flaps – 90 KIAS • Final: Power as required – 100% Flaps – <78 KIAS Instrument Procedures • Cleared IAF: Power as required – 120 KIAS • FAF Inbound: 25% Power – 100 KIAS • ½ Scale below Glide Slope or 2NM prior to FAF on non-precision appr. – 50% Power – 50% Flaps V-Speeds & KIAS V-Speed KIAS Vso 62 V s 71 V R 71-75 V X 81 V Y 96 V FE 150 V FE 110 V O 133 V NO 164 V NE 201 V G 100 V PD 133 Crosswind Limit – 20 KTS