| 词条 | Zlín Z 526 | ||||||||||||||||||
| 释义 |
The Zlin Z-526 Akrobat is a Czech sports plane used in aerobatics. HistoryThe Z-526 was originally designed by Zlin Aircraft in 1959. Its two-seat version is called the Trener-Master The Z 526's layout was organized with the pilot in the rear, and the student in front. The aircraft could be equipped also with tip tanks and a constant speed propeller. The Z-526F was introduced in 1968 and was equipped with a 135 kW (180 hp) Avia M 137A engine, the export version Z-526L differing by being equipped with a 150 kW (200 hp) Lycoming AEIO-360 flat-four. Single-seat versions included the Z-526A, Z-526AS, and the Z-526AFS. The Z-526 AFM was built between 1981 and 1984 and was powered by a 155 kW (210 hp) Avia M337 engine, had tip tanks and a lengthened fuselage. The aircraft was later developed into the Zlin Z-726. More than 1,400 Z-526s were manufactured, many for military and private flying schools. Variants
Two-seat version
Single-seat version
Single-seat version
Single-seat version
powered by an Avia M337 inverted six-cylinder engine giving 210hp(157kW) Aircraft On Display
A Zlin Z-526M is on display. Specifications (Z-526F){{Aircraft specifications|plane or copter?= |jet or prop?= |ref= |crew=one or two |capacity= |payload main= |payload alt= |length main= 8.00 m |length alt=26 ft 3 in |span main=10.60 m |span alt=34 ft 9 in |height main=2.06 m |height alt=6 ft 9 in |area main= 15.5 m² |area alt= 166.3 ft² |airfoil= |empty weight main= 665 kg |empty weight alt= 1,465 lb |loaded weight main= |loaded weight alt= |useful load main= |useful load alt= |max takeoff weight main= 975 kg |max takeoff weight alt= 2,150 lb |more general= |engine (prop)=Avia M 137 A |type of prop=inverted inline engine |number of props=1 |power main= 135 kW |power alt= 180 hp |power original= |max speed main= 244 km/h |max speed alt= 132 knots |cruise speed main= 210 km/h |cruise speed alt= 113 knots |stall speed main= |stall speed alt= |never exceed speed main= |never exceed speed alt= |range main= 475 km |range alt= 256 nm |ceiling main= 5,200 m |ceiling alt= 17,060 ft |climb rate main= 5.99 m/s |climb rate alt= 1,180 ft/min |loading main= |loading alt= |thrust/weight= |power/mass main= |power/mass alt= |more performance= |avionics= }} External links{{commons category|Zlin Z-526}}
5 : Czechoslovakian sport aircraft 1960–1969|Single-engined tractor aircraft|Zlín aircraft|Low-wing aircraft|Aircraft first flown in 1959 |
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