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Price:
| $48,500 (plus mod. cost) |
| Engine make/model: | Lycoming IO-360-C1C
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| Horsepower@rpm@altitude: | 200 @2700 @SL |
| Horsepower for takeoff: | 200 |
TBO hrs.:
| 2000 |
| Fuel type: | 100/100LL
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Propeller type/type:
| Hartzell two-blade CS
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Landing gear type:
| Tri/Retr
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| Max ramp weight (lbs.): | 2650
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| Gross weight (lbs.): | 2650
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| Max landing weight (lbs.): | 2650
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| Empty weight, std. (lbs.): | 1531
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| Useful load, std. (lbs.): | 1119 |
Payload, full std. fuel (lbs.):
| 831
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| Usable fuel (gals.): | 48
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| Oil capacity (qts.): | 8
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| Wingspan: | 32 ft. |
| Overall length: | 24 ft. 6 in.
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| Height: | 8 ft.
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| Wing area (sq. ft.): | 170 |
Wing loading (lbs./sq. ft.):
| 15.6
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Power loading (lbs./hp.):
| 13.3 |
Wheel base:
| 7 ft. 11 in.
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Wheel track:
| 10 ft. 6 in.
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Wheel size (in.):
| 6.00 x 6
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| Seating capacity: | 4
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Cabin doors:
| 1
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| Cabin width (in.): | 42 |
| Cabin height (in.): | 43 |
| Baggage capacity (lbs.): | 200
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PERFORMANCE |
| Cruise speed (kts.): | |
| 75% power @ 7,000 ft.: | 157* |
| 65% power @ 10,000 ft.: | 153* |
55% power @ 12,000 ft.:
| 145* |
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| Max range (w/ reserve) (nm): | |
75% power:
| 518* |
65% power:
| 612* |
55% power:
| 638*
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Fuel consumption (gph):
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| 75% power: | 11.5 |
| 65% power: | 10.5 |
55% power:
| 9.0 |
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| Estimated endurance (65% power w/1 hr reserve) (hrs): | 4.6* |
| Stall speed (flaps up) (knots): | 63 |
| Stall speed (flaps down) (knots): | 56 |
| Best rate of climb (fpm): | 900 |
Best rate of climb (8000 ft - fpm):
| 500
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| Service ceiling (ft.): | 15,000 |
| Takeoff ground roll (ft.): | 770 |
| Takeoff over 50-ft. obstacle (ft.): | 1600
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| Landing ground roll (ft.): | 780 |
Landing over 50-ft. obstacle (ft.):
| 1380
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* as modified
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all specs are standard unless noted otherwise
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Source for Piper specs: 1974 Piper Arrow Information Manual
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