Piper PA-34 Seneca

Piston • twin 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

Endorsements & ratings:
  • High-Performance
  • Complex
  • Multi-Engine
200
KTAS
Cruise Speed
6
Occupants
828
nm
Max Range
605
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper PA-34 Seneca

The Piper PA-34 Seneca V (PA-34-220T) is a six-seat, twin-engine touring aircraft often cited as a step-up for pilots graduating from smaller trainers. It is the latest evolution of the Seneca line, featuring turbocharged Continental TSIO-360-RB engines and a re-designed cowling for improved aerodynamics compared to earlier models.

Key Features for GA Buyers

  • Counter-Rotating Propellers: A signature safety feature of the Seneca line, the engines spin in opposite directions, eliminating the “critical engine” factor and significantly simplifying single-engine handling during emergencies.
  • Cabin Comfort: The fuselage is derived from the Cherokee Six/Lance, offering one of the widest cabins in its class with club seating for rear passengers, making it a comfortable platform for family or business travel.
  • High-Altitude Capability: With turbocharged engines and a service ceiling of 25,000 ft, the Seneca V is well-suited for mountain flying and clearing weather systems.

Trade-offs

  • Useful Load: While capable of carrying six seats, the full-fuel useful load (often around 600 lbs) realistically limits the aircraft to 3 adults and bags for maximum range missions.
  • Complexity & Maintenance: The turbocharged engines run hotter and require more disciplined management than naturally aspirated alternatives (like the Seminole), leading to higher potential maintenance costs.
  • Handling: Pilots often describe the control forces as heavier than lighter twins like the Beechcraft Duchess or Piper Seminole.

Featured in our buying guides

Technical Specifications

Dimensions

Wingspan
38.9 ft
Length
28.6 ft
Height
9.9 ft
Parking area (ft2)
1643.04 ft2

Weights

Max Takeoff Weight
4,750 lbs
Max Landing Weight
4,513 lbs
Useful Load
1,337 lbs
Fuel Capacity
122 gal

Performance

Cruise Speed
200 KTAS
Never-Exceed (Vne)
204 KIAS
Max Structural Cruise (Vno)
164 KIAS
Approach Speed
90 KIAS
Stall, Clean (Vs1)
67 KIAS
Range
828 NM
Service Ceiling
25,000 ft
Rate of Climb
253 - 1550 fpm
Takeoff over 50 ft obstacle
1,707 ft
Landing ground roll
2,180 ft

Engines

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