Aircraft model
PIPER PA22-20-135
Everything here is true of every aircraft of the type, not of any one aircraft.
The PA22-20-135 designation records a Tri-Pacer converted to conventional landing gear -- the so-called PA-22/20, in which the nosewheel airframe is put back on the tailwheel legs the Pacer was built with. It is one of the most common modifications in light aviation and it is done for two reasons: the Tri-Pacer's nosegear is the part owners complain about, and the conversion turns a cheap four-seater into a cheap four-seat taildragger.
Ownership is steel tube and fabric ownership. The recover is the periodic bill that dwarfs everything else, corrosion in the tubing under the fabric is what ends these airframes, and the lift strut inspection requirement is a real one. Against that, the engines are among the cheapest four-cylinder Lycomings to overhaul and the parts trade for the type is unusually good, because Univair and others still make almost everything. A converted aircraft needs its paperwork read: which approval was used, whether the flight manual supplement is aboard, and whether the work was done properly at the gear attachment fittings. Insurance will treat it as a taildragger and so should the pilot, because the conversion does nothing to soften the short-coupled ground handling the Pacer was always known for.
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Put PIPER PA22-20-135 side by side with up to two other models.
- PIPER PA22-20-135
What it is
| Seats | 4 |
|---|---|
| Landing gear | taildragger |
| Engines | 1 |
| Engine | Lycoming O-290-D2 |
| Horsepower | 135 hp |
| Fuel | 100LL |
| Certification basis | CAR3 |
| Production start | 1952 |
| Production end | 1960 |
| Endorsements required | tailwheel |
Performance
| Cruise speed | 111 KTAS |
|---|---|
| Range | 450 nm |
| Service ceiling | 16,500 ft |
| Climb rate | 755 ft/min |
| Stall speed (Vso) | 43 KCAS |
| Takeoff over 50 ft | 1,600 ft |
| Landing over 50 ft | 1,280 ft |
Load and fuel
| Seats | 4 |
|---|---|
| Useful load | 955 lb |
| Full-fuel payload | 739 lb |
| Max takeoff weight | 1,950 lb |
| Empty weight | 995 lb |
| Usable fuel | 36 gal |
| Fuel burn at cruise | 7.6 gal/h |
Cost of ownership
| Price, low | $45,000 |
|---|---|
| Price, high | $110,000 |
| Prices as of | 2026 |
| Engine TBO | 1,800 h |
| Overhaul cost, low | $26,000 |
| Overhaul cost, high | $36,000 |
The fleet and its record
| Registered, all time | 1 |
|---|---|
| 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, 3-4 seats |
|---|---|
| Accident record | —1 |
| Severity | —2 |
| Access | —3 |
| Support | 0.2 of 104 |
| Liquidity | —5 |
- Accident record: class median 28.36 · 202 models in class.
- Severity: class median 11.65.
- Access: class median 767.75.
- Support: class median 141.5.
- Liquidity: class median 19.57.
- 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.