Piper 28T Arrow 4

Piston • single engine • Low Wing • Retractable gear

Range Visualization

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Payload vs. Range

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Avg. pax weight (lbs)

Default: 190 lbs (FAA standard)

Luggage per pax (lbs)

Default: 30 lbs

Passengers

lbs @ lbs / pax

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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

172

KTAS

Cruise Speed

Occupants

695

Max Range

805

lbs

Wet Payload

Estimated Ownership Costs

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About the Piper 28T Arrow 4

The Piper PA-28RT-201 Turbo Arrow IV is a T-tail, four-seat, single-engine turbocharged piston aircraft introduced in 1979. Powered by a 200 hp Continental TSIO-360-FB engine, it features retractable landing gear and a three-blade constant-speed propeller. With a normal cruise speed of 172 KTAS, a rate of climb of 940 fpm, and a service ceiling of 20,000 ft, it offers excellent high-altitude performance. Fuel capacity is 72 US gallons, giving a range of approximately 695 NM, and a useful load of about 1,237 lb. The Turbo Arrow IV was produced until 1986 and is valued for its combination of speed and utility.

Technical Specifications

Dimensions

Wingspan: 35.4 ft
Length: 27.33 ft
Height: 8.25 ft

Weights

Max Takeoff Weight: 2,900 lbs
Max Landing Weight: 2,900 lbs
Useful Load: 1,237 lbs
Fuel Capacity: 72 gal

Performance

Cruise Speed: 172 KTAS
Range: 695 NM
Service Ceiling: 20,000 ft
Rate of Climb: 940 fpm

Engines

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