Sling TSi

Piston • single engine • Low Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

MOSAIC Eligibile Sport Pilot-flyable
155
KTAS
Cruise Speed
4
Occupants
1000
nm
Max Range
703
lbs
Wet Payload

Estimated Ownership Costs

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About the Sling TSi

Sling TSi

The Sling TSi is a high-performance, four-seat experimental homebuilt aircraft developed by Sling Aircraft. Designed as a development of the Sling 4, it is specifically optimized for the Rotax 915 iS or 916 iS turbocharged engines, offering impressive high-altitude performance and efficiency. It has become a favorite in the GA community for pilots who want modern, glass-cockpit capabilities and long-range cross-country utility without the price tag of certified competitors like the Cirrus SR series.

Key Features for GA Buyers

  • Turbocharged Performance: Maintains sea-level power up to 15,000 ft, allowing for efficient cruising at higher altitudes to find better winds and cooler air.
  • Modern Avionics: Typically equipped with the Garmin G3X Touch suite, providing full IFR capability and integrated engine monitoring.
  • Efficiency: Consumes only 7-8 gallons per hour of MOGAS or Avgas while cruising at 155 KTAS.
  • Payload Utility: A true four-adult aircraft with a useful load exceeding 1,000 lbs, making it practical for family trips.

Trade-offs

  • Experimental Category: As an E-AB aircraft, it requires significant builder time (approx. 900-1,400 hours) or purchasing a pre-owned experimental, which carries different maintenance and insurance considerations than certified aircraft.
  • Fixed Gear: While simplifying maintenance and reducing insurance premiums, the fixed gear limits the top-end speed compared to retractable-gear high-performance singles.
  • Flap Speeds: Relatively low flap extension speed (VFE of 85 KIAS) requires careful energy management during the transition from cruise to the terminal environment.

Technical Specifications

Dimensions

Wingspan
31.3 ft
Length
23.54 ft
Height
8.0 ft
Parking area (ft2)
1178.7 ft2

Weights

Max Takeoff Weight
2,094 lbs
Max Landing Weight
2,094 lbs
Useful Load
1,015 lbs
Fuel Capacity
52 gal

Performance

Cruise Speed
155 KTAS
Never-Exceed (Vne)
155 KIAS
Max Structural Cruise (Vno)
125 KIAS
Approach Speed
62 KIAS
Stall, Clean (Vs1)
56 KIAS
Range
1000 NM
Service Ceiling
23,000 ft
Rate of Climb
1200 fpm
Takeoff over 50 ft obstacle
820 ft
Landing ground roll
750 ft

Engine

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