Piper Cherokee Warrior II: Difference between revisions

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→‎Performance: Numbers were for a PA-28-140, which is an older, slower aircraft with slightly different fuselage and wings.
(→‎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==
* Maximum speed: 123 knots (142 mph, 230 km/h)
* Cruise speed (TAS):
* Cruise speed: 108 knots (124 mph (200 km/h), 201 km/h)
** 75% power, 8,000 ft, ROP, wheel fairings installed: 127 knots (146 mph 235 km/h)
* Stall speed: 47 knots (54 mph, 87 km/h)
* Stall speed (IAS):
* Range: 465 nm (535 sm, 867 km)
** 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: 660 ft/min (3.4 m/s)
* Rate of climb:
* Wing loading: 13.4 lb/sq ft (64.4 kg/sq m)
** sea level, 2335 lb: 710 ft/min (3.6 m/s)
* Power/mass: 14.3 lb/hp (0.116 kW/kg)


<i>Source: Piper Aircraft: Cherokee 140 PA-28-140 Owner's Handbook. Piper Aircraft Corporation publication 753 584, February 1964, Revised May 27, 1977 via [http://en.wikipedia.org/wiki/Piper_Cherokee Wikipedia]</i>
<i>Source: Piper Cherokee Warrior II Information Manual, 1981</i>


== Development status/Issues/Todo ==
== Development status/Issues/Todo ==
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