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LAA Specification Sheet Pazmany PL2 Type No. 069 Plans built Aircraft Number of seats Two Construction All metal Engine 135 – 150 hp Length 19ft 4 in Span 25 ft Wing Area 116 sq ft Max Weight 1700 lbs Rate of Climb 1700 ft/min Cruise 132 mph Vendor Pazmany Aircraft Corporation P.O. Box 80051 San Diego, CA 92138 USA www.pazmany.com Other links
The ICAO (International Civil Aviation Organization) Doc 8643 document contains designators for those aircraft types which are most commonly provided with air traffic service (ATS)
11 mar 2010 · PAZMANY PL-2 STANDARD DATA: Gross wt. 1,416. Empty wt. 875. Fuel capacity 25. Wingspan 28′. Length 19’4″. Engine 100-hp Lycoming. PERFORMANCE: Top mph 138. Cruise mph 119. Stall mph 52. Climb rate…
Pazmany PL-2. Venerable side-by-side low wing monoplane, sheet metal construction
Sri Lanka Air Force PL-2 program started in 1977; First maiden test flight on April 11, 1980; Pazmany PL-2 aircraft was built by the Aircraft Engineering Wing of the Sri Lanka Air Force, under the personal supervision of Wing Commander N. Gunarathnam; This was the first instance in the history that an aircraft has been completely built in Sri Lanka
8 maj 2019 · The PL-2 was a side-by-side two-seat, dual control, aircraft with a fixed tricycle undercarriage. The fuselage was built up of conventional pressed metal frames, longerons and skins. The all-flying tail was equipped with an anti-servo tab for trimming and providing adequate stick forces.
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