Piper PA-31T3-500 T-1040

Turboprop • twin 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
  • Multi-Engine
236
KTAS
Cruise Speed
11
Occupants
950
nm
Max Range
2058
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper PA-31T3-500 T-1040

Overview

The Piper PA-31T3-500 T-1040 is a rare commuter turboprop developed in the early 1980s by mating the unpressurized fuselage of the Chieftain with the wings, tail, and PT6A-11 engines of the Cheyenne I. Piper certified the type in 1982 and built only 24 airframes through 1984, targeting the third-level commuter airline market that needed turbine reliability without the cost or complexity of a pressurized cabin.

The design rationale was specific: short-haul feeder routes typically run under 200 miles, where pressurization adds weight and cost without operational benefit. The result is an 11-passenger turboprop with a useful load above 3,800 lbs, capable of operating from 3,000 ft strips and burning Jet A. Most units served regional carriers like Bar Harbor Airlines and Sunbird Airlines before the deregulation era reshaped commuter aviation.

Key Features for GA Buyers

  • Payload Utility: Without pressurization equipment, the T-1040 carries an exceptional useful load (3,800 lbs+), making it well suited to cargo, jump operations, or high-density passenger configurations.
  • Turbine Reliability: Pratt & Whitney Canada PT6A-11 engines deliver 500 shp per side with 3,600 hr standard TBO, significantly more reliable and longer-running than the piston Chieftain’s Lycoming TIO-540s.
  • Cabin Volume: The stretched Chieftain fuselage seats up to 11 in commuter configuration, or holds substantial cargo with seats removed and an optional belly pod fitted.
  • Short-Field Capability: Wing loading and engine power yield landing distances under 2,200 ft, opening regional fields that jet operators cannot serve.

Trade-offs

  • Unpressurized: Service ceiling is 24,000 ft but most operations run between 10,000 and 14,000 ft, leaving the aircraft below most weather rather than above it.
  • Rarity: With only 24 built, type-specific parts and experienced maintenance are increasingly difficult to source. Many components are shared with the Cheyenne I and Chieftain, but unique hybrid items have no aftermarket.
  • Fuel Burn: Cruise burn near 66 GPH is roughly double that of a piston Chieftain, eroding the economic case for low-utilization private operators.
  • Limited Resale Market: The combination of small fleet size, commuter-spec interiors, and aging avionics keeps the secondary market narrow.

See Also

Technical Specifications

Dimensions

Wingspan
41.1 ft
Length
36.67 ft
Height
12.75 ft
Parking area (ft2)
2129.34 ft2

Weights

Max Takeoff Weight
9,000 lbs
Max Landing Weight
9,000 lbs
Useful Load
3,800 lbs
Fuel Capacity
260 gal

Performance

Cruise Speed
236 KTAS
Never-Exceed (Vne)
246 KIAS
Max Structural Cruise (Vno)
190 KIAS
Approach Speed
90 KIAS
Stall, Clean (Vs1)
86 KIAS
Range
950 NM
Service Ceiling
24,000 ft
Rate of Climb
1600 fpm
Takeoff over 50 ft obstacle
2,650 ft
Landing ground roll
2,150 ft

Engines

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