Cirrus Vision Jet SF50

TCDS: A00017AC Max Weight: 6,000 lbs

Cirrus Aircraft

Certification
Normal

Aircraft Overview

Official TCDS specifications for Cirrus Vision Jet SF50 per Type Certificate A00017AC

⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate A00017AC. Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
6,000 lbs
Max Landing
5,550 lbs
Typical Empty
3,550 lbs
Max Baggage
300 lbs
Useful Load
2,450 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tank 115.0 in Standard loading position
Pilot Seat 100.0 in Standard loading position
Baggage Area 190.0 in Primary baggage compartment
Front Passenger 100.0 in Standard loading position
Rear Passengers 150.0 in Standard loading position

Center of Gravity Envelope

CG must remain within these limits throughout all phases of flight.

📊 aft limit Category
📊 forward limit Category
🔧 Engine Specifications
Engine Model
Williams FJ33-5A
Power Output
N/A
Fuel Type
Jet A
Oil Capacity
3 qt
📋 Key Specifications
TCDS Number A00017AC
Max Weight 6,000 lbs
Engine Williams FJ33-5A
Power N/A
Category Normal
🏁 Speed Limits
VNE (Never Exceed) 311 KIAS
VNO (Normal) 250 KIAS
VFE (Flaps) 173 KIAS
VS (Stall Clean) 92 KIAS
VS0 (Stall Landing) 83 KIAS
📈 Performance Notes

The Cirrus Vision Jet SF50 delivers single-engine jet performance with 311 KTAS cruise speed, CAPS parachute system, and pioneering personal jet design.

⚠️ Important Disclaimers

Verification Required

Always verify against current aircraft records and equipment list before flight operations.

TCDS Reference

This summarizes TCDS A00017AC but does not replace the official document.

Regulatory Compliance

Calculations must comply with 14 CFR Part 23 and applicable airworthiness directives.

Data Accuracy

Specifications may vary by serial number and modifications. Verify with aircraft documentation.