Piper PA-38 Tomahawk

Piper PA-38 Tomahawk

The Piper PA-38 Tomahawk is a light aircraft that was introduced by Piper Aircraft in the late 1970s as a primary trainer and recreational plane. Designed to be a simple, cost-effective solution for flight training, the Tomahawk features a high-wing configuration and a stable, forgiving flight characteristic ideal for novice pilots. Its construction focuses on ease of maintenance and operation, making it a popular choice among flight schools and private owners looking for an economical way to gain flying experience.

Equipped with a 115-horsepower Lycoming O-235 engine, the PA-38 Tomahawk offers a cruising speed of approximately 100 knots and a range of around 400 nautical miles. Its low operating costs and straightforward systems contribute to its affordability, making it an attractive option for training purposes. The aircraft’s design includes a spacious, well-placed cockpit that enhances visibility and comfort for both the pilot and a student or co-pilot.

One of the key features of the Tomahawk is its stable flight characteristics, which are achieved through its design elements like the low stall speed and good control responsiveness. These attributes help new pilots develop their skills with confidence while also ensuring safety during flight training. The Tomahawk’s reputation for being forgiving during stalls and its manageable handling make it an effective tool for teaching fundamental flying techniques.

Despite its many advantages, the Piper PA-38 Tomahawk has faced some criticisms over the years, particularly concerning its performance in certain aerodynamic conditions. Nonetheless, it remains a valuable asset in the aviation community for its intended role as a training aircraft. The Tomahawk’s legacy is reflected in its continued use in flight schools and by private pilots who appreciate its simplicity and practicality.

Piper PA-38 Tomahawk parameters

Here are the key parameters for the Piper PA-38 Tomahawk:

1. Dimensions:
   • Wingspan: Approximately 32 feet 10 inches (10.01 meters)
   • Length: About 22 feet 10 inches (6.96 meters)
   • Height: Roughly 8 feet 6 inches (2.59 meters)
   • Wing Area: Approximately 177 square feet (16.5 square meters)
2. Performance:
   • Maximum Speed: Around 125 knots (230 km/h, 143 mph)
   • Cruise Speed: Approximately 100 knots (185 km/h, 115 mph)
   • Stall Speed: About 50 knots (93 km/h, 58 mph)
   • Range: Roughly 400 nautical miles (740 km, 460 miles)
   • Service Ceiling: Around 13,000 feet (3,960 meters)
3. Engine and Power:
   • Engine Type: Lycoming O-235-L2C
   • Horsepower: 115 horsepower (86 kW)
   • Propeller: Fixed-pitch, two-blade
4. Weights:
   • Maximum Takeoff Weight: Approximately 1,950 pounds (884 kg)
   • Empty Weight: About 1,230 pounds (559 kg)
   • Useful Load: Approximately 720 pounds (327 kg)

These parameters highlight the Piper PA-38 Tomahawk’s suitability as a training aircraft with manageable performance characteristics and operational efficiency.