Allison 36 Turbine Bonanza

Turboprop • single engine • Low Wing • Retractable gear

Range Visualization

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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

Endorsements & ratings:
  • High-Performance
  • Complex
210
KTAS
Cruise Speed
6
Occupants
980
nm
Max Range
577
lbs
Wet Payload

Estimated Ownership Costs

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About the Allison 36 Turbine Bonanza

Overview

The Allison 36 Turbine Bonanza is the original Soloy / Allison turbine conversion of the Beechcraft A36, STC-certified in 1986. The prototype, a 1979 A36, replaced the airframe’s Continental piston engine with a 420 shp Allison 250-B17C free-turbine engine driving a three-blade Hartzell propeller. Tradewind Turbines purchased the STC in 1989 and later upgraded the conversion to the 450 shp Allison 250-B17F/2; Soloy Aviation Solutions reacquired the STC in 2016 and is the current STC holder.

Key Features for GA Buyers

  • Turbine reliability on a familiar airframe. The A36 cabin, panel, and handling are preserved while the firewall-forward replaces piston-engine complexity, mixture management, and 100LL dependence with a single power lever and Jet-A.
  • Performance step over piston A36. The conversion delivers roughly 200 to 215 KTAS in cruise at the mid-teens, against the naturally-aspirated A36’s 169 KTAS, with comparable fuel burn around 24 GPH at altitude.
  • Bonanza ownership profile. Service infrastructure, parts, type-club support, and resale market for the underlying A36 airframe remain among the strongest in general aviation.

Trade-offs

  • Acquisition cost. Turbine conversions carry six-figure premiums over comparable piston A36s; the price differential rarely closes through fuel-cost savings alone at typical owner-operator hours.
  • Unpressurised at turbine altitudes. The conversion does not pressurise the airframe, so high-cruise altitudes still require supplemental oxygen and reduce the practical block-speed advantage on shorter legs.
  • Specialist support. STC support has changed hands twice (Soloy to Tradewind to Soloy); owners depend on a smaller pool of qualified maintenance and a finite installed base for parts knowledge.

See Also

  • Beechcraft A36 – the piston-engined airframe the conversion is built on; same cabin, lower acquisition and complexity. Compare
  • Beechcraft Bonanza B36TC – the turbocharged-piston route to high-altitude performance on the same airframe family. Compare
  • Beechcraft G36 – the modern factory-production Bonanza; current avionics and support, piston powerplant. Compare
  • Piper M500 – pressurised single-engine turbine cross-shop; same Jet-A operating model with higher acquisition cost and more cabin. Compare
  • Socata TBM 700 – pressurised single-engine turbine in the speed step-up; substantially more capable and substantially more expensive. Compare

Technical Specifications

Dimensions

Wingspan
33.5 ft
Length
29.2 ft
Height
8.6 ft
Parking area (ft2)
1487.7 ft2

Weights

Max Takeoff Weight
3,650 lbs
Max Landing Weight
3,650 lbs
Useful Load
1,073 lbs
Fuel Capacity
74 gal

Performance

Cruise Speed
210 KTAS
Never-Exceed (Vne)
205 KIAS
Approach Speed
73 KIAS
Stall, Clean (Vs1)
68 KIAS
Range
980 NM
Service Ceiling
18,500 ft
Rate of Climb
1230 fpm

Engine

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