Initial Operational Capability (IOC):
Also Known As: L-29A, L-29R and Maya
AERO Vodochody a.s.
Parent System: L-29 Delfin
Initial Operational Capability (IOC): 1963
Total Production: 3,600
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Description: Czech Republic's Aero L-29 Delfin is a single-engine, two-seat turbojet trainer developed for the Soviet Union. Entered service in the early 1960s. It was sold as an advanced trainer to Warsaw Pact nations, except Poland, and other international customers. L-29A was a single-seat version and L-29R a dedicated ground attack variant. NATO dubbed L-29 as 'Maya'.
L-29 Delfin Specifications
Number of Engines: 1
Height: 4.70 meter (15.4 foot)
Length: 12.1 meter (39.7 foot)
Wingspan: 9.60 meter (31.5 foot)
Ceiling: 11,000 meter (36,089 foot)
Max Range: 1,750 kilometer (945 nautical mile)
Cruise Speed: 170 mps (612 kph)
Top Speed at High Altitude: 209 mps (753 kph)
Max Takeoff Thrust: 3,800 pound (1,724 kilogram)
Max Takeoff Weight: 3,500 kilogram (7,716 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
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