AAFC SR22T Quick Reference Sheet
Cirrus SR22T G7 · V Speeds Reference
Overview
The AAFC SR22T Quick Reference Sheet provides essential operational and performance information for the Cirrus SR22T G7 aircraft. This document is designed for pilots and aviation enthusiasts, offering quick access to critical data such as engine specifications, fuel management, maneuver configurations, and V-speeds. It serves as a handy reference for both pre-flight planning and in-flight operations, ensuring that pilots can operate the aircraft safely and efficiently. The sheet includes specific performance metrics, operational limits, and procedural guidelines that are vital for effective flight management.
- Engine: Continental TSIO-550-K, 315 HP, oil capacity 8 quarts.
- Maximum Gross Takeoff Weight: 3600 lbs; Maximum Baggage Loading: 130 lbs.
- Usable Fuel Capacity: 92 gallons; switch tanks every 20-25 minutes to avoid imbalance.
- VSO: 64 KIAS, VR: 77-80 KIAS, VY: 103 KIAS, VNO: 150-176 KIAS, Crosswind Limit: 21 KTS.
- Use electric fuel pump during critical phases: priming, takeoff, landing, and switching tanks.
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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.
Document details
- Type ·
- V Speeds Reference
- Pages ·
- 3
- File size ·
- 120 KB
- Copy found at ·
- aeroatlanta.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp) ·
- 315
- Engine model ·
- Continental TSIO-550-K
- Fuel capacity (gal) ·
- 92
- Max takeoff weight (lb) ·
- 3,600
Performance
- Max crosswind (kt) ·
- 21
- Stall speed clean (kt) ·
- 74
- Stall speed landing (kt) ·
- 64
V-speeds
- VR ·
- 80
- VX ·
- 88
- VY ·
- 103
- VFE ·
- 150
- VNE ·
- 205
- VNO ·
- 176
- VS1 ·
- 74
- VSO ·
- 64
Weight & balance
- Baggage allowance (lb) ·
- 130
- Max takeoff weight (lb) ·
- 3,600
What is the AAFC SR22T Quick Reference Sheet?
The AAFC SR22T Quick Reference Sheet is a v speeds reference for the Cirrus SR22T G7.
How many pages is the AAFC SR22T Quick Reference Sheet?
The copy of the AAFC SR22T Quick Reference Sheet on file runs 3 pages.
Common. More common than 99% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cirrus SR22T G7.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Engine Information
The Cirrus SR22T G7 is powered by a Continental TSIO-550-K engine, which is a turbocharged, fuel-injected, horizontally opposed, air-cooled engine producing 315 horsepower. Pilots should maintain cylinder head temperatures (CHTs) between 240°F and 420°F. The oil capacity of the engine is 8 quarts, and the maximum gross takeoff weight is 3600 lbs, with a maximum baggage compartment loading of 130 lbs.
Operational Specifications
The aircraft has a usable fuel capacity of 92 gallons, with a total capacity of 94.5 gallons. Pilots must switch fuel tanks approximately every 20-25 minutes to avoid imbalance, which triggers a CAS message at a 10-gallon difference. The SR22T G7 can use 100LL and 100 octane fuel. It features two fuel pumps: an engine-driven pump and an auxiliary electric pump, which should be used during priming, takeoff, landing, and other critical phases.
V-Speeds
The V-speeds for the Cirrus SR22T G7 are crucial for safe operation. Vso is 64 KIAS, Vs is 74 KIAS, VR ranges from 77 to 80 KIAS, VX is 88 KIAS, and VY is 103 KIAS. The maximum flap extension speed (VFE) is 150 KIAS for full flaps and 110 KIAS for 50% flaps. Other important speeds include VNO at 150-176 KIAS, VNE at 175-205 KIAS, and VPD at 140 KIAS. The aircraft has a crosswind limit of 21 knots.
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Safety notes
- Maintain CHTs between 240°F and 420°F at all times.
- Lean the mixture to max RPM for ground operations before taxi and after landing.
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Full document text
AAFC SR22T Quick Reference Sheet Engine Information • Continental TSIO-550-K o (Keep CHTs between 240F and 420F at all times) • Fuel Injected, Horizontally Opposed, Air Cooled, Turbocharged, Direct Drive, 315 HP • Oil Capacity – 8 quarts • Maximum Gross Takeoff Weight – 3600 lbs • Maximum Baggage Compartment Loading – 130 lbs Operational Specifications • 92 Gallons Usable Fuel (94.5 Total) o Tabs – 60 gallons • Must switch fuel tanks – expect a fuel tank switch every 20-25 minutes o CAS message triggered at 10 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 (high boost), takeoff, landing, switching tanks, maneuvering, climbing, & descending Leave electric pump on at cruise for at least 30 minutes **Before taxi and after landing you should lean the mixture to max RPM for ground operation. Maneuver Configurations • Steep Turns: 50% Power – 120 KIAS • Ground Reference Maneuvers: 40% Power – 100 KIAS • Slow Flight/Power Off Stalls: 30% Power – <100 KIAS • Power On Stalls: 30% Power – >65% Power • Downwind: 40% Power • Abeam Touchdown: 30% Power – 12” MP – 50% Flaps – 100 KIAS • Base: 12” MP – 100% Flaps – 90 KIAS • Final: 12” MP – 100% Flaps – 80-85 KIAS Instrument Procedures • Cleared IAF: Power as required – 120 KIAS • FAF Inbound: 30% Power – 100 KIAS • ½ Scale below Glide Slope or 2NM prior to FAF on non-precision appr. – 40% Power – 50% Flaps V-Speeds & KIAS V-Speed KIAS Vso 64 V s 74 V R 77-80 V X 88 V Y 103 V FE 150 V FE 110 V O 140 V NO 150-176 V NE 175-205 V G 92 V PD 140 Crosswind Limit – 21 KTS