482
edits
Piper Cherokee Warrior II: Difference between revisions
Jump to navigation
Jump to search
→Aircraft help: added gen. characteristics & performance sections
m (→Aircraft help) |
(→Aircraft help: added gen. characteristics & performance sections) |
||
| Line 83: | Line 83: | ||
===Landing=== | ===Landing=== | ||
Landing check list on panel. | Landing check list on panel. | ||
==General Characteristics== | |||
* Crew: one pilot | |||
* Capacity: three passengers | |||
* Length: 23.3 feet (7.16 m) | |||
* Wingspan: 30.0 feet (9.2 m) | |||
* Height: 7.3 feet (2.25 m) | |||
* Wing area: 160 sq ft (15.14 m²) | |||
* Airfoil: NACA 652-415 | |||
* Empty weight: 1201 lb (544 kg) | |||
* Loaded weight: 2150 lb (975 kg) | |||
* Useful load: 949 lb (430 kg) | |||
* Max takeoff weight: 2150 lb (975 kg) | |||
* Powerplant: 1× Lycoming O-320-E2A Sensenich M74DM, 150 hp (113 kW) | |||
* Propeller diameter: 74 inches (1.9 m) | |||
==Performance== | |||
* Maximum speed: 123 knots (142 mph, 230 km/h) | |||
* Cruise speed: 108 knots (124 mph (200 km/h), 201 km/h) | |||
* Stall speed: 47 knots (54 mph, 87 km/h) | |||
* Range: 465 nm (535 sm, 867 km) | |||
* Service ceiling: 14,300 feet (4400 m) | |||
* Rate of climb: 660 ft/min (3.4 m/s) | |||
* Wing loading: 13.4 lb/sq ft (64.4 kg/sq m) | |||
* 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 <a href="http://en.wikipedia.org/wiki/Piper_Cherokee">Wikipedia</a></i> | |||
== Development status/Issues/Todo == | == Development status/Issues/Todo == | ||