| ………. |  |
A comparison of PL-2, PL-4A and PL-9 by Pazmany Aircraft Corporation:
| PL-2 | PL-4A | PL-9 | |
| Top Speed (mph) | 138 | 120 | 116 |
| Cruise (mph) | 119 | 97 | 104 |
| Stall (mph) | 52 | 46 | 33 |
| Range (mi) | 492 | 280 | 332 |
| Rate of Climb (fpm) | 1200 | 650 | 1400 |
| Take-Off Distance (ft) | 700 | 560 | 250 |
| Landing Distance (ft) | 600 | 440 | 90 |
| Service Ceiling (ft) | 18,000 | 13,000 | 15,000 |
| Engine Used | LYC-235 | VW 1600 c.c. | LYC 0-320 |
| Power Range (hp) | 108-100-150 | 50-90 | 150-160 |
| Fuel Capacity (gal) | 25 | 12 | 30 |
| Empty Weight (lb) | 875 | 578 | 1,132 |
| Gross Weight (lb) | 1,416 | 850 | 1,739 |
| Height (ft) | 7.7 | 5.7 | 7 |
| Length (ft) | 19.3 | 16.5 | 24.3 |
| Wing Span (ft) | 27.8 | 26.7 | 36 |
| Wing Area (sq. ft) | 116 | 89 | 166 |
| Number of Seats | 2 | 1 | 2 |
| Landing Gear | Trigear | Tailwheel | Tailwheel |
| Building Materials | M | M | M. T. F. |
| Building Time (manhours) | 3,500 – 5,000 | 2,000 | 4,000 – 5,000 |
| No. Completed & Flown | ~300 | ~220 | 1 |
| General Characteristics | Side-by-side low-wing monoplane, sheet metal construction |
VW-powered, single seater, T-tail, sheet metal construction |
Replica of the German Fieseler Storch. Tube and fabric fuselage with sheet metal covering on wings and tails |