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1974 Piper Pathfinder N57347
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| Engine make/model: | Lycoming O-540-B4B5 | |
| Horsepower@altitude: | 235@SL | |
| Horsepower for takeoff: | 235 | |
| TBO hrs.: | 2000 | |
| Fuel type: | 100/100LL | |
| Propeller type/diameter: | Hartzell CS | |
| Landing gear type: | Tri/Fixed | |
| Max ramp weight (lbs.): | 3000 | |
| Gross weight (lbs.): | 3000 | |
| Landing weight (lbs.): | 3000 | |
| Empty weight, std. (lbs.): | 1550 | |
| Useful load, std. (lbs.): | 1450 | |
| Payload, full std. fuel (lbs.): | 958 | |
| Usable fuel (gals.): | 82 | |
| Oil capacity (qts.): | 12 | |
| Wingspan: | 32 ft. | |
| Overall length: | 24 ft. | |
| Height: | 7 ft. 10 in. | |
| Wing area (sq. ft.): | 170 | |
| Wing loading (lbs./sq. ft.): | 17.6 | |
| Power loading (lbs./hp.): | 12.8 | |
| Wheel size (in.): | 6.00 x 6 | |
| Seating capacity: | 4 | |
| Cabin doors: | 1 | |
| Cabin width (in.): | 44 | |
| Cabin height (in.): | 47 | |
| Baggage capacity (lbs.): | 200 | |
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PERFORMANCE
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| Cruise speed (kts.): | ||
| 75% power: | 133 | |
| 65% power: | 127* | |
| 55% power: | 122* | |
| Max range (w/ reserve) (nm): | ||
| 75% power: | 718** | |
| 65% power: | 813** | |
| 55% power: | 939** | |
| Fuel consumption (gph): | ||
| 75% power: | 12.8** | |
| 65% power: | 11.1** | |
| 55% power: | 9.4** | |
| Estimated endurance (65%) (hrs): | 6.4** | |
| Vs (kts.): | 57 | |
| Vso (kts.): | 52 | |
| Best rate of climb (SL fpm): | 800 | |
| Best rate of climb, 8000 ft. (fpm): | 400* | |
| Service ceiling (ft.): | 13,550 | |
| Takeoff ground roll (ft.): | 850 | |
| Takeoff over 50-ft. obstacle (ft.): | 1410 | |
| Landing ground roll (ft.): | 1040 | |
| Landing over 50-ft. obstacle (ft.): | 1740 | |
| *estimated | ||
| **calculated | ||
| Sources: Aircraft Bluebook Price Digest, Jane’s All The World’s Aircraft | ||
