Piper Aircraft
PA-38-112 Tomahawk
Single-engine piston · Primary trainer · Pre-1980 classic
discontinued
- Power
- 112 hp
- Cruise
- 110 kt
- MTOW
- 1,670 lb
- Range
- 460 nm
- Fuel
- 100LL avgas
🇺🇸Specs shown in Imperial.
Performance
- Cruise speed (Vc)110 kt
- Never-exceed speed (Vne)138 kt
- Stall (landing config) (Vs0)47 kt
- Climb rate718 fpm
- Service ceiling13,000 ft
- Range460 nm
- Endurance4 h
- Takeoff roll1,460 ft
- Landing roll635 ft
Weights
- MTOW1,670 lb
- Empty weight1,109 lb
- Useful load561 lb
- Baggage capacity100 lb
Dimensions
- Wingspan34 ft
- Length23.2 ft
- Height9.1 ft
- Cabin width42 in
Powerplant
- EngineLycoming O-235-L2C — 112 hp · 100LL · 6 gph
- Total horsepower112 hp
- Primary fuel100LL avgas
- Unleaded pathLeaded only — needs G100UL or engine swap
Cockpit & avionics
- Cockpit typeanalog
- Autopilot commonly availableNo
- Typical packages
- Six-pack analog with single nav/com— as-delivered
- Garmin G5 / GFC 500 retrofits— modern retrofit on active fleets
Certification
- RegulatoryFAR Part 23 (CAR 3 origin)
- Certified rolesNormal category · Utility category
- IFRNo
- Spin approvedYes
- Aerobatic-categoryNo
- TailwheelNo
- Complex (FAR 61.31)No
- High-performance (FAR 61.31)No
Why is the PA-38-112 Tomahawk popular?
Structured popularity-driver evidence. Each axis below carries one factual statement; we don't grade, the facts speak.
Pedagogy and handling
Designed in consultation with active CFIs with deliberately sharper stall and spin behaviour than a Cessna 152 so student recognition of departures from controlled flight would be unambiguous; the type retains a niche role at schools that specifically value that pedagogy.
Operating economics
Acquisition cost between $22,000 and $60,000 and Lycoming O-235-L2C fuel burn around 6 gph keep the Tomahawk among the cheapest two-seat trainers available to flying clubs that retain the type.
Production volume
Approximately 2,497 airframes were built before production ended in 1982 — substantially smaller fleet than the Cessna 152, with corresponding parts-availability constraints driven by type-club support rather than factory channels.
Parts and MRO ecosystem
Out-of-production since 1982 with no factory support; parts are sourced through type-club networks (notably Piper Owner Society) and salvage. Common consumables (Lycoming O-235 cylinders, sparks, magnetos) remain widely available because the engine is still produced for other airframes, but PA-38-specific airframe items (T-tail attach hardware, control surfaces) are increasingly difficult to source new and frequently rely on overhaul of existing stock.
Regulatory fit
FAA TCDS A11SO certifies the PA-38-112 in both Normal and Utility categories with intentional spin certification — relevant for CFI / commercial pilot spin-training requirements under FAR 61.183(i). Not LSA-eligible (1,670 lb MTOW exceeds the LSA limit) and not approved for IFR in the original certification, though many active airframes carry post-certification IFR-capable retrofits.
Fuel future-proofing
100LL-only without a documented G100UL pathway as of the FAA EAGLE programme's 2026 status. The Lycoming O-235-L2C is on the manufacturer's broader unleaded-fuel evaluation track but not on a published G100UL STC list specific to the PA-38 airframe — meaning Tomahawk operators face the same lead-fuel transition risk as other discontinued 100LL trainers without an explicit fleet pathway.
Before you buy more aircraft
The next airframe is rarely the highest-leverage move.
Flight school revenue is a function of three things — utilisation, dispatch reliability, and student progression — that multiply rather than add. Most schools running below 850 hours per aircraft per year have hidden capacity worth more than the next purchase, already paid for and sitting on the ramp.
Read: Why buying more aircraft probably won't grow your schoolHow flight schools track this aircraft in Aviatize
Schools that retain Tomahawks typically configure them in Aviatize as a low-cost ab-initio / spin-training airframe. Engine reserves track against the Lycoming O-235-L2C 2,400-hour TBO. The PA-38 wing-rigging service-bulletin compliance cycle is commonly tracked as a recurring inspection in the maintenance module.
Editorial confidence
1 primary source cited. Spec data is partially attributed; some operating details are editorial synthesis pending additional research.
Sources
Primary sources are POH / TCDS / manufacturer pages; derived sources record where Aviatize editorial synthesis is layered on top.
- Primary sourceFAA TCDS·Retrieved 2026-05-05
Federal Aviation Administration (FAA)
https://drs.faa.gov/browse/excelExternalWindow/A11SOFAA TCDS A11SO covers the PA-38-112.
- Editorial synthesisAviatize-internal·Retrieved 2026-05-05
Aviatize editorial
Entry authored by Aviatize from accumulated industry knowledge cross-referenced against the primary sources cited above. Specific fleet figures, fleet wins, and recent production status changes are research-backlog candidates and should be verified against primary sources before flipping verified: true.