PL-1
| Photo courtesy of EAA Sport Aviation: "L. Pazmany with first prize for Original Design won at EAA Fly-In at Corona Airport, October 7, 1962" |
| NOTES: By using the Continental C90-12F engine, the PL-1 meets FAA Light-Sport Aircraft category. |
| Engine | Continental C90-12F (Actual Measured Performance) |
Lycoming 0-290-D2b (Estimated Performance) |
| Gross Weight (lb) | 1,320 | 1,407 |
| Wing Area (sq. ft) | 116 | 116 |
| Wing Loading (lb/sq. ft) | 11.4 | 12.1 |
| Power, T.O. (hp) | 95 | 140 |
| Power, Rated RPM (hp) | 90 | 135 |
| Rated Power Loading (lb/hp) | 14.7 | 10.4 |
| Empty Weight (lb) | 800 | 881 |
| Span (ft) | 28 | 28 |
| Length (ft) | 18'11" | 18'11" |
| Fuel Capacity (gal) | 25 | 25 |
| Max Speed SL (mph) | 120 | 160 |
| Cruise Speed SL (mph) | 115 | 155 |
| Landing Speed SL, 37 deg Flap - 1.1VS (mph) | 56 | 59 |
| Stall Speed SL, 37 deg Flap (mph) | 51 | 54 |
| Rate of Climb SL (fpm) | 1,000 | 1,600 |
| Usable Service Ceiling (ft) | 18,000 | 22,000 |
| Normal Range SL (mi) | 500 | 450 |
| Take-Off Distance/50 ft, 15 deg Flap (ft) | 784 | 560 |
The following articles about the PL-1 are provided as a courtesy of EAA Sport Aviation Magazine, Air Progress Magazine, and the Union Tribune (PDF format). These articles were written after the first flights, in a Q-and-A format, where Mr. Pazmany answered many typical questions people had about the PL-1.
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