Piper Tomahawk PA38
Piston • single engine • Low Wing • Fixed gear
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About the Piper Tomahawk PA38
Overview
The Piper PA-38 Tomahawk is a two-seat, fixed-gear, low-wing trainer produced from 1978 to 1982, with roughly 2,484 built. Piper designed it from the ground up as a primary trainer, surveying flight instructors on what they wanted in a training aircraft. The result was a low-wing, T-tailed design built around a NASA GA(W)-1 airfoil, with deliberately honest and demanding handling intended to teach airmanship rather than mask it. It competed directly with the Cessna 150 and 152 through the late 1970s and early 1980s.
The Tomahawk uses the same Lycoming O-235-L2C as the Cessna 152, giving it a long 2,400-hour TBO and a modest 6 to 7 GPH fuel burn. Where it differs from the Cessna is philosophy: the low wing and responsive controls give a more aircraft-like feel that many instructors prized, but its stall and spin behaviour is less forgiving than the high-wing Cessnas. That characteristic shaped both its value as a trainer and its reputation.
Key Features for GA Buyers
Genuine training feel. The low-wing layout, responsive ailerons, and honest stall warning were specified by the instructors Piper surveyed. The aircraft rewards correct technique and exposes sloppy technique, which is precisely what a primary trainer is for. Pilots who learned in a Tomahawk tend to transition well to heavier low-wing types.
Low operating cost. The O-235-L2C carries one of the longest TBOs in general aviation at 2,400 hours and burns roughly 6.5 GPH. There is no retractable gear, no turbocharger, and no constant-speed propeller to maintain, which keeps annual inspections straightforward.
MOSAIC sport-pilot eligible. A clean stall speed of approximately 48 KIAS keeps the Tomahawk under the conservative sport-pilot threshold, making it flyable on a sport-pilot certificate under the MOSAIC rule.
Affordable entry. Airworthy examples typically trade in the $20,000 to $35,000 range, among the lowest-cost paths into certificated aircraft ownership.
Trade-offs
- Demanding stall and spin behaviour. The GA(W)-1 airfoil was chosen so that the aircraft requires positive, correct pilot input to recover from a developed spin rather than recovering passively. This makes it an effective spin trainer but unforgiving of mishandling, and the type recorded a higher stall/spin accident rate than the Cessna 150/152. Airworthiness Directive 83-14-08 (September 1983) mandated additional inboard leading-edge stall strips to improve stall progression. The reputation that followed – the nickname “Traumahawk” – is rooted in this behaviour and in training operations that did not always brief it adequately. A buyer should confirm AD compliance and seek type-specific spin and stall instruction.
- Two seats, modest load. Useful load is approximately 542 lbs. With full fuel (30 usable gallons, about 180 lbs) that leaves roughly 362 lbs for two occupants and baggage, so two adults with bags will watch weight and balance carefully.
- Slow cruise. Around 105 KTAS at 75% power (closer to 100 KTAS at economy settings). The Tomahawk is a training and local-flying aircraft, not a cross-country machine.
- Aging fleet. Production ended in 1982, so every Tomahawk in service is more than 40 years old. Corrosion history, stall-strip AD compliance, and high-time training airframes all deserve close scrutiny in a pre-purchase inspection.
- Valve adjustments every 100 hours. Like the Cessna 152, the O-235-L2C uses solid tappets, so valve clearance must be checked and adjusted every 100 hours – a recurring item that catches some owners off-guard.
- Smaller fleet, thinner parts. With about 2,484 built against many thousands of Cessna 150s and 152s, parts support and mechanic familiarity exist but are less ubiquitous than for the Cessna trainers.
See Also
- Cessna 152 – the dominant competing trainer; high-wing, more forgiving stall behaviour, and a far larger support fleet. Compare
- Cessna 150 – the 152’s predecessor and another common primary trainer; lower power and widely available at low prices. Compare
- Cessna Skyhawk 172 – the natural four-seat step-up for pilots outgrowing a two-seat trainer; more useful load and genuine cross-country capability. Compare
Featured in our buying guides
Technical Specifications
Dimensions & Weights
- Length
- 23.1 ft
- Parking area (ft2)
- 1236.4 ft2
- Max Takeoff Weight
- 1,670 lbs
- Max Landing Weight
- 1,670 lbs
- Useful Load
- 542 lbs
- Fuel Capacity
- 30 gal
Performance
- Cruise Speed
- 105 KTAS
- Never-Exceed (Vne)
- 138 KIAS
- Max Structural Cruise (Vno)
- 108 KIAS
- Approach Speed
- 60 KIAS
- Stall, Clean (Vs1)
- 48 KIAS
- Range
- 468 NM
- Service Ceiling
- 13,000 ft
- Rate of Climb
- 718 fpm
Similar to the Piper Tomahawk PA38
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