Piper Seminole

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:
  • Complex
  • Multi-Engine
162
KTAS
Cruise Speed
4
Occupants
700
nm
Max Range
502
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper Seminole

The Piper PA-44 Seminole is one of the most recognizable multi-engine trainers in the world. Developed from the Piper Arrow, it shares the same T-tail and semi-tapered wing design but adds a second Lycoming O-360 engine. Its reputation is built on docile handling and reliability, making it the standard platform for earning a multi-engine rating.

Key Features for GA Buyers

  • Counter-Rotating Propellers: The right engine rotates counter-clockwise (LIO-360), eliminating the “critical engine” aerodynamic issues found in most twins. This makes single-engine drills significantly safer and easier to master.
  • Simple Systems: Compared to larger twins like the Seneca or Baron, the Seminole uses carbureted engines (on most older models) and simple manual systems, keeping maintenance costs lower.
  • Trainer Pedigree: Because it is the default multi-engine trainer for thousands of flight schools, parts availability and mechanic knowledge are widespread.

Trade-offs

  • Single-Engine Performance: With only 180 hp per side, the single-engine service ceiling is low (approx. 3,800–4,000 ft density altitude), meaning it cannot maintain altitude on one engine over mountainous terrain.
  • Cabin Size: The cabin is essentially a Piper Arrow fuselage; it is tighter than the Seneca or Beechcraft Duchess, making it less ideal for long-distance family touring.
  • T-Tail Handling: The T-tail requires more airflow to become effective, leading to a heavier rotation on takeoff and less elevator authority during the landing flare compared to low-tail aircraft.

Technical Specifications

Dimensions

Wingspan
38.6 ft
Length
27.6 ft
Height
8.5 ft
Parking area (ft2)
1584.36 ft2

Weights

Max Takeoff Weight
3,800 lbs
Max Landing Weight
3,800 lbs
Useful Load
1,150 lbs
Fuel Capacity
108 gal

Performance

Cruise Speed
162 KTAS
Never-Exceed (Vne)
202 KIAS
Max Structural Cruise (Vno)
169 KIAS
Approach Speed
88 KIAS
Stall, Clean (Vs1)
57 KIAS
Range
700 NM
Service Ceiling
15,000 ft
Rate of Climb
212 - 1340 fpm
Takeoff over 50 ft obstacle
1,400 ft
Landing ground roll
1,490 ft

Engines

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