Single Engine • Piper • PA-38-112, PA-38-125, PA-38-160
| Manufacturer | Piper |
| Model | PA-38 Tomahawk |
| Category | Single Engine |
| Variants | PA-38-112, PA-38-125, PA-38-160 |
| Production Years | 1978 – 1989 |
| Seating | 2 seats |
| Typical TTAF | 4,200 hours |
| Markets | United States, Canada, United Kingdom, Australia, Germany |
| Price Range | $35K – $95K |
The Piper PA-38 Tomahawk is a two-seat, single-engine aircraft designed primarily for flight training and personal transportation. Introduced in the late 1970s, it represents Piper's answer to the training market with an emphasis on affordability and simplicity. The aircraft features a high-wing configuration, fixed landing gear, and a Lycoming O-235 engine, making it economical to operate. The Tomahawk became popular among flight schools worldwide due to its robust construction, forgiving handling characteristics, and low acquisition and maintenance costs. Its spacious cabin and good visibility make it suitable for primary flight training, recreational flying, and personal use. The aircraft's straightforward systems and durable design have allowed many examples to remain in active service for over four decades. The Tomahawk is known for its reliability and ease of maintenance, though some pilots note its relatively modest performance compared to contemporary competitors. Today, the type remains a common sight at general aviation airports and continues to serve as an entry-level platform for pilots pursuing their licenses.
Maximum Speed: 115 knots
Cruise Speed: 105 knots
Range: 510 nautical miles
Service Ceiling: 12,200 feet
Engine: Lycoming O-235-C2C (112 hp)
Maximum Takeoff Weight: 1,670 pounds
Empty Weight: 1,080 pounds
Fuel Capacity: 40 gallons
Wing Span: 32 feet