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Piper Cherokee Arrow III - AeroClub


![]() Climb Chart |
![]() Descent Chart |
Lycoming engines
465 nm range
3 pax, 200 lbs cargo capacity
465 nm range
3 pax, 200 lbs cargo capacity
The original PA-28R-180 Cherokee Arrow was a relatively simple adaptation of the existing PA-28-180 Cherokee D, but incorporated electro-hydraulically operated retractable undercarriage (complete with a self lowering system that safeguarded against the pilot failing to do so, automatically lowering when airspeed reached 91kt and a certain engine manifold pressure), a fuel injected version of the PA-28-180s O-360, a constant speed propeller and an increased max takeoff weight.
The PA-28R-201 Arrow III first flew in September 1975, and was introduced from 1976. The major change (also introduced on the fixed undercarriage PA-28s at that time) was a new longer tapered span wing, while the maximum takeoff weight was increased.
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Length | 7.38 m |
Wingspan | 9.14 m |
Height | 2.44 m |
Engine | IO-360-C1C6 |
Cruise Speed | 138 kts |
Service Ceiling | 16,200 ft |
Gross Weight | 1.25 t |
Capacity | 3 pax | 200 lbs |
Crew | 1 pilot |
Price | 0.3M EUR |
Manufacturer | PIPER |
Pictures | Airliners.net |
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OEW | 1,637 lbs |
MTOW | 2,750 lbs |
Fuel Capacity | 72 gal |
Fuel Weight | 504 lbs |
Long Range Altitude | 15000 FT |
Long Range Speed | 143 kts |
Max Speed | 149 kts |
Range (MLoad...MFuel) | 465... 695 |
Engine Thrust | 1 x 200 HP |
Takeoff RWY Length (Min) | 1,025 ft |
Takeoff RWY Length (Max) | 1,600 ft |
Landing RWY Length | 615 ft |
V Rotate / Flaps | 75kts / 15 deg |
V Approach / Flaps | 71kts / FULL |
Max climb rate | 1700 ft/min |
Max descent rate | -1500 ft/min |