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Base price:
| $970,000 |
| Engine make/model: | Lycoming TIO-540-AE2A
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| Horsepower@altitude: | 350 hp to 17,000
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| Horsepower for takeoff: | 350 |
TBO hrs.:
| 2000 |
| Fuel type: | 100/100LL
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Propeller type/diameter:
| Hartzell three -blade/80
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Landing gear type:
| Tri./Retr.
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| Max ramp weight (lbs.): | 4340
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| Gross weight (lbs.): | 4340 |
| Landing weight (lbs.): | 4100
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| Empty weight, std. (lbs.): | 3100
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| Useful load, std. (lbs.): | 1240
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Payload, full std. fuel (lbs.):
| 520
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| Usable fuel, std. (gals.): | 120 |
| Oil capacity (qts.): | 12
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| Wingspan: | 43 ft. |
| Overall length: | 28 ft. 6 in. |
| Height: | 11 ft. 5 in. |
| Wing area (sq. ft.): | 175 |
Wing loading (lbs./sq. ft.):
| 24.8
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Power loading (lbs./hp.):
| 12.4
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Wheel size (in.):
| 6.00 x 6
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| Seating capacity: | 6
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Cabin doors:
| 1
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| Cabin width (in.): | 49 |
| Cabin height (in.): | 47 |
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PERFORMANCE |
| Cruise speed (kts.): | |
| 75% power: | 213 |
| 65% power: | 199 |
55% power:
| 166 |
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Fuel consumption (gph):
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| 75% power: | 20.0 |
| 65% power: | 18.0 |
55% power:
| 15.0
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| Range, 55% power (nm): | 1055 |
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| Best rate of climb (SL fpm): | 1225 |
Best rate of climb, 8,000 ft (fpm):
| 1100*
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| Max operating altitude (ft.): | 25,000 |
Vso (kts):
| 58
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| Takeoff ground roll (ft.): | 1090 |
| Takeoff over 50-ft. obstacle (ft.): | 2090
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| Landing ground roll (ft.): | 1020 |
Landing over 50-ft. obstacle (ft.):
| 1960
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*estimated
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Sources: Aircraft flight manual and New Piper Website
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