Piper 32T Turbo Lance 2

Piston • single engine • Low Wing • Retractable 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

175
KTAS
Cruise Speed
6
Occupants
865
nm
Max Range
971
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper 32T Turbo Lance 2

Key Features for GA Buyers

The Piper PA-32RT-300T Turbo Lance II is a high-performance, single-engine aircraft that serves as a logical step-up for pilots graduating from the PA-28 Archer/Arrow series. It is essentially a retractable-gear version of the Cherokee Six, retaining that airframe’s legendary load-hauling capability and spacious six-seat cabin.

  • Heavy Hauler: Known as the “Suburban of the Sky,” it offers a substantial useful load (often over 1,500 lbs), allowing for full fuel and a reasonable passenger load.
  • Turbo Performance: The turbocharged Lycoming TIO-540 engine allows for cruising at altitudes up to 20,000 ft, maintaining true airspeeds of ~175 kts above the weather.
  • Club Seating: Features a comfortable club seating arrangement with a wide center aisle and dual cargo doors, making loading passengers and luggage exceptionally easy.
  • T-Tail Configuration: Distinguishes the “Lance II” from earlier Lances and later Saratogas. The T-tail places the horizontal stabilizer out of the propwash, designed to reduce vibration.

Trade-offs

  • Handling Characteristics: The T-tail design results in less elevator authority at low speeds compared to the conventional tail, requiring a specific takeoff technique (allowing speed to build before rotation) to avoid abrupt pitch-up.
  • Maintenance: The turbocharging system adds complexity and maintenance costs compared to naturally aspirated models. The engine runs hotter and requires careful management to reach TBO.
  • Fuel Burn: Expect a fuel burn of 18-20 gallons per hour at cruise, which is higher than smaller retractables like the Mooney M20 or Piper Arrow.

Technical Specifications

Dimensions

Wingspan
32.83 ft
Length
27.75 ft
Height
9.5 ft

Weights

Max Takeoff Weight
3,600 lbs
Max Landing Weight
3,600 lbs
Useful Load
1,535 lbs
Fuel Capacity
94 gal

Performance

Cruise Speed
175 KTAS
Range
865 NM
Service Ceiling
20,000 ft
Rate of Climb
1050 fpm

Engines

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