An-24rb

 

Aircraft description
 The aircraft was developed in mid-sixties. It is equipped with RU-19A300 auxiliary power plant of 800 kgf-thrust mounted in the RH turboprop nacelle. This engine improves the aircraft takeoff performance. Àn-24 "Ñoke" is configured as a cantilever monoplane with high-mounted wing equipped with extended-span Fouler flaps. The double-slotted flaps are externally fitted at the engine nacelle and single-slotted flaps are installed at the root wing. The tail unit has a traditional design, in a seria
Technical characteristics
 FLIGHT PERFORMANCE: Àn-24RV UR-MSI Aircraft Year of manufacture1975ã. Crew5 Maximum takeoff weight, t. 22,5 Maximum payload, kg2720 Maximum passenger capacity, person 48 Maximum range, km1500 Cruising rate, km/h475 Landing rate, km/h180 Climb time 6000 m, min15 Operating ceiling, m8400 Takeoff roll, m 650 Landing run, m 590 Required runway length, m1300   OVERALL DIMENSIONS: Wing span, m29,20 Length, m23,53 Height, m8,32 Wing area, m274,98 Wheel base, m7,85 Passenger cabin:  - width, ì. 2,76 -