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AAFC SR20 Quick Reference Sheet

Cirrus SR20 G7 · V Speeds Reference

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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

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

Copy found at aeroatlanta.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
V Speeds Reference
Pages
·
3
File size
·
114 KB
Copy found at
·
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
About this document
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.

How rare is it?
2,207Cirrus SR20 G7 registered worldwide · 2,198 active

Common. More common than 98% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the Cirrus SR20 G7.

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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.

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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.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

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

All Cirrus SR20 G7 v speeds reference