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General Info

PZL Mielec
PZL I-22 Iryda M93K

Role Jet Trainer
Manufacturer PZL Mielec
First flight 3 March 1985
Introduction 22 December 1992
Retired 1996
Status Retired
Primary user Polish Air Force
Number built 17 including prototypes

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History WSK "PZL-Mielec  
PZL Mielec PZL I-22 Iryda M93K



The PZL I-22 Iryda, otherwise known as the PZL M93 Iryda and PZL M96 Iryda, was a twin-engine, two-seat military jet trainer aircraft developed and produced by Polish aviation company PZL Mielec.

Work started on what would become the Iryda in 1976 as a successor to the indigenously-developed TS-11 Iskra jet trainer. First flying on 3 March 1985, the type would have a protracted development, partly due to the initial unavailability of its PZL K-15 turbojet engines. The Polish Air Force received the first K-15-powered Irydras in May 1995. However, aircraft deliveries were complicated by disputes over cost and performance, leading to multiple announcements, policy reversals, and groundings of the type. A fatal accident involving the type on 24 January 1996 fuelled criticism and undermined support for the programme.

During May 1995, the first pair of M-93K Irydas were delivered to the Polish Air Force; these were intended to be the production-standard version of the type.[1] Unlike the five preceding units of the type that had been previously handed over, the M-93K model was powered by the PZL K-15 engines instead of the older PZL-5 units which had been adopted as an interim powerplant. Amongst other benefits, the more powerful K-15 engines almost doubled the Iryda's payload capacity. The K-15 engine was not considered to be a likely candidate for export sales of the Iryda; British engine manufacturer Rolls-Royce was at one stage working with PZL to certify its Viper engine to power the type.

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WSK "PZL-Mielec" Now Sikorsky

WSK "PZL-Mielec" Now Sikorsky
PZL I-22 Iryda

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General Info

  • Crew: 2
  • Length: 13.22 m (43 ft 4 in)
  • Wingspan: 9.6 m (31 ft 6 in)
  • Height: 4.3 m (14 ft 1 in)
  • Wing area: 19.92 m2 (214.4 sq ft))
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Powerplant

  • Empty weight: 4,600 kg (10,141 lb)
  • Gross weight: 6,650 kg (14,661 lb)
  • Max takeoff weight: 7,500 kg 
  • Powerplant: 2 × PZL K-15 turbojet engines, 14.7 kN (3,300 lbf) thrust each
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Specifications

  • Maximum speed: 940 km/h (580 mph, 510 kn) at 5,000 m (16,404 ft)
  • Maximum speed: Mach 0.82
  • Range: 1,200 km (750 mi, 650 nmi)
  • Service ceiling: 13,700 m (44,900 ft)
  • Rate of climb: 40.6 m/s (7,990 ft/min)
  • Thrust/weight: 0.4
Special Links WSK "PZL-Mielec" Now Sikorsky; PZL I-22 Iryda

Links to Youtube & Others

PZL Mielec (Polskie Zakłady Lotnicze - Polish Aviation Works)

PZL I-22 Iryda

PZL Mielec (Polskie Zakłady Lotnicze - Polish Aviation Works)

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Youtube Link

PZL Mielec (Polskie Zakłady Lotnicze - Polish Aviation Works)

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Aircrafttotal : WSK "PZL-Mielec" Now Sikorsky

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