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Data from Piper PA-22-160 pilot's operating handbook, issued January 1960 General characteristics Crew: one Capacity: three passengers Length: 20 ft 6 in (6.25 m) Wingspan: 29 ft 3 in (8.92 m) Height: 8 ft 4 in (2.54 m) Wing area: 147.5 sq ft (13.70 m 2) Empty weight: 1,110 lb (503 kg) Gross weight: 2,000 lb (907 kg) Fuel capacity: 36 US gal (140 L; 30 imp gal) Powerplant: 1 × Lycoming O-320 ...
Initial designation for military version of the PA-18, reverted to PA-18 designation after three built PA-20 Pacer: 1950 1,121 Re-designed PA-16 PA-21 0 Proposed production version of the Baumann Brigadier: PA-22 Tri-Pacer: 1951 9,490 Updated version of the PA-20 with nose wheel PA-23 Apache: 1954 2,047 Twin-engined low-wing cabin monoplane PA ...
Print/export Download as PDF; Printable version; In other projects Wikimedia Commons; ... Piper PA-22-160 Tri-Pacer [19] Piper PA-23-250 Aztec [20]
On 22 September 1953, a British European Airways Douglas C-47 Skytrain (registration: G-AGIZ) crashed into a hedge on landing at Guernsey Airport, no injuries. On 15 September 1954, a Royal Air Force Short Sunderland MR.5 (serial: PP122) hit a submerged rock on landing causing a rupture in the hull.
Learn how to download and install or uninstall the Desktop Gold software and if your computer meets the system requirements.
The PA-22 had a three-bladed rotor with a diameter of 32 ft (9.8 m), pylon-mounted over the cockpit. It was connected via a clutch to the nose-mounted, 85 hp (63 kW) Pobjoy Cataract engine to spin it up, with rotor blades latched at a low angle of incidence , then unlatched for take-off.
Some troops leave the battlefield injured. Others return from war with mental wounds. Yet many of the 2 million Iraq and Afghanistan veterans suffer from a condition the Defense Department refuses to acknowledge: Moral injury.
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