Aircraft model
PIPER PA-28-140FL
Everything here is true of every aircraft of the type, not of any one aircraft.
The Cherokee 140, Piper's low-wing answer to the Cessna 150 and 172, built from 1964 to 1977. Despite the name it had 150 hp from 1964 onward. Piper sold it as a two-seat trainer with an optional rear bench, and that optional bench is why it appears as a four-seater — in practice it is a two-plus-two, because loading four adults and useful fuel puts it over gross. The first aircraft were certified as two-seaters at 1,950 lb; the four-seat version at 2,150 lb was approved in June 1965, so a 1964 aircraft may be a genuine two-seater and the paperwork of any individual aeroplane decides which it is. Piper never changed the engine or the constant-chord wing during the run; the later aircraft differ in trim and in name — the Flite Liner trainer from 1971 and the Cruiser 2+2, shortened to Cruiser in 1974 — rather than in what they can do. It was used to train enormous numbers of pilots and many are still doing that work.
The low wing is the main difference in character from a Cessna: you climb onto the wing to get in through one door on the right, visibility in a turn is better below and worse above, and it sits lower and feels more stable in turbulence. It also has 50 usable gallons, which is generous for its size and gives it genuinely long legs. The weaknesses are a cramped rear seat, only one cabin door, modest climb performance on a warm day, and the Piper wing spar corrosion and fatigue inspection requirements that now apply to high-time PA-28 airframes. Running costs are low and every mechanic knows the type.
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Put PIPER PA-28-140FL side by side with up to two other models.
- PIPER PA-28-140FL
What it is
| Seats | 4 |
|---|---|
| Landing gear | tricycle |
| Engines | 1 |
| Engine | Lycoming O-320-E2A |
| Horsepower | 150 hp |
| Fuel | 100LL |
| Certification basis | CAR3 |
| Production start | 1964 |
| Production end | 1977 |
| Endorsements required | — |
Performance
| Cruise speed | 108 KTAS |
|---|---|
| Range | 600 nm |
| Service ceiling | 14,300 ft |
| Climb rate | 660 ft/min |
| Stall speed (Vso) | 47 KCAS |
| Takeoff over 50 ft | 1,700 ft |
| Landing over 50 ft | 1,000 ft |
Load and fuel
| Seats | 4 |
|---|---|
| Useful load | 945 lb |
| Full-fuel payload | 645 lb |
| Max takeoff weight | 2,150 lb |
| Empty weight | 1,205 lb |
| Usable fuel | 50 gal |
| Fuel burn at cruise | 8.4 gal/h |
Cost of ownership
| Price, low | $36,000 |
|---|---|
| Price, high | $125,000 |
| Prices as of | 2026 |
| Engine TBO | 2,000 h |
| Overhaul cost, low | $28,000 |
| Overhaul cost, high | $40,000 |
The fleet and its record
| Registered, all time | 2 |
|---|---|
| Active fleet | 0 |
| Median year built | — |
| NTSB events, last 10 years | 0 |
| Fatal events, last 10 years | 0 |
| Events per 1,000 active, last 10 years | — |
| Personal-flying events per 1,000 active | — |
| Ownership transfers, last 24 months | 0 |
| Transfers per 100 active | — |
| Airworthiness directives | 0 |
| Directives, last 5 years | 0 |
| Rate confidence | none |
Peer scores6
| Peer class | Fixed wing single-engine, piston, 1 engine, 1-2 seats |
|---|---|
| Accident record | —1 |
| Severity | —2 |
| Access | —3 |
| Support | 0.2 of 104 |
| Liquidity | —5 |
- Accident record: class median 29.1 · 174 models in class.
- Severity: class median 9.09.
- Access: class median 974.
- Support: class median 81.
- Liquidity: class median 20.47.
- Each of the five categories places the model within its peer class, from 0 (the worst of the class) to 10 (the best): a position among comparable models, not a grade. The overall score is the sum of the categories shown that are scored, out of 10 for each (50 when all five are); it is given only when at least 4 of the five are scored, and it can be set against another model's only when both are in the same peer class and scored on the same categories.