Piper Aircraft - USA
Australia; Canada; Japan; New Zealand; Scotland; South Africa; United Kingdom; United States
Inherent ability of airframe to take considerable damage.
EXTENDED RANGE PERFORMANCE
Capability to travel considerable distances through onboard fuel stores.
Features partially- or wholly-enclosed crew workspaces.
Features retracting / retractable undercarriage to preserve aerodynamic efficiency.
Maximum Take-Off Weight
monoplane / low-mounted / straight
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Mainplanes are low-mounted along the sides of the fuselage.
The planform involves use of basic, straight mainplane members.
1 x Lycoming IO-540 6-cylinder air-cooled engine developing 260 horsepower driving two-bladed propeller unit at the nose.
(315 kph | 170 knots)
(300 kph | 162 knots)
(+15 kph | 8 knots)
(5,900 m | 4 miles)
(1,970 km | 1,064 nm)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030