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(→Related links: checklists) |
(→Performance: Numbers were for a PA-28-140, which is an older, slower aircraft with slightly different fuselage and wings.) |
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==Performance== | ==Performance== | ||
* | * Cruise speed (TAS): | ||
* | ** 75% power, 8,000 ft, ROP, wheel fairings installed: 127 knots (146 mph 235 km/h) | ||
* | * Stall speed (IAS): | ||
* Range: | ** 40° flaps: 44 knots (51 mph, 82 km/h) | ||
** no flaps: 50 knots(58 mph, 93 km/h) | |||
* Range: | |||
** 55% power, 8,000 ft, LOP, no reserve: 695 nm (800 sm, 1,287 km) | |||
** 75% power, 8,000 ft, ROP, no reserve: 580 nm (668 sm, 1,074 km) | |||
* Service ceiling: 14,300 feet (4400 m) | * Service ceiling: 14,300 feet (4400 m) | ||
* Rate of climb: | * Rate of climb: | ||
** sea level, 2335 lb: 710 ft/min (3.6 m/s) | |||
<i>Source: Piper | <i>Source: Piper Cherokee Warrior II Information Manual, 1981</i> | ||
== Development status/Issues/Todo == | == Development status/Issues/Todo == |
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