PZL I-22 Iryda
The PZL I-22 Iryda, otherwise known as the PZL M93 Iryda and PZL M96 Iryda, was a twin-engine, two-seat Polish military jet trainer aircraft developed and produced by Polish aviation company PZL Mielec.
|PZL I-22 M93K|
|First flight||3 March 1985|
|Introduction||22 December 1992|
|Primary user||Polish Air Force|
|Number built||17 including prototypes|
Work started on what would become the Iryda during 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 during May 1995. However, aircraft deliveries were complicated due to 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 1996, an agreement was struck to upgrade the existing aircraft to a new standard, flight testing of which commenced during the following year. However, relations between PZL Mielec and the Polish Defense Ministry became so poor over the programme that legal action was initiated while the Iryda itself languished. During the late 1990s, Polish Government support for the programme was withdrawn, and the handful of delivered aircraft were stored. Despite attempts to revive the programme by PZL Mielec, no orders have been forthcoming.
In 1976, the Warsaw Institute of Aeronautics (Polish: Instytut Lotnictwa) initiated work on a program to develop a new jet-powered trainer aircraft; this was primarily envisioned to replace the Polish Air Force's existing TS-11 Iskra fleet, an indigenously-developed first generation jet trainer aircraft. A key feature of the new type would be its PZL K-15 turbojet engines, which were also locally designed by the Warsaw Institute of Aeronautics. Subsequently dubbed Iryda, the aircraft was designed by PZL Mielec (then WSK-Mielec).
On 3 March 1985, the first prototype conducted the type's maiden flight. Early examples of the type were powered by a pair of PZL-5s, an older generation turbojet engine; these were considered to be underpowered and were only intended as a temporary measure while issues with the newer K-15 were being resolved. Following the Revolutions of 1989, Poland soon gained greater accessibility to international markets; this had an impact upon the fledgling Iryda. It was chosen to adopt a British-developed Martin-Baker Mk.10 ejection seat; consideration was reportedly given to the incorporation of foreign-sourced avionics from French aeronautics company SAGEM.
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. 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.
While the Polish Armed Forces were heavily impacted by curtailed budgets during the 1990s, the service intended to take delivery of five M-93K aircraft by the end of 1995, while plans for purchasing an additional six-to-eight Irydas were publicly mooted. At the time, there was an acknowledged desire for "around 40" jet trainers; the Polish Navy had also sought new trainer aircraft at this time.
On 1 December 1995, the Polish Government announced that the Polish Air Force would purchase no further aircraft due to it being too costly to continue. The Iryda's chief designer, Marek Potapowicz, openly stated that the programme's loss could lead to the collapse of PZL Mielec. That same month, a rival plan to procure second-hand Dassault/Dornier Alpha Jets for the Polish Air Force was officially suspended; the negative impact on Polish industry was apparently a major contributing factor to this decision. Nevertheless, competing trainers, including the Alpha Jet, Saab 105, and Aero L-39 Albatros, were demonstrated to Polish officials. PZL Mielec offered several improvements for the Iryda, including various aerodynamic improvements, such as leading-edge root extensions and trailing edge flaps, along with a costly SAGEM-sourced avionics suite.
During January 1996, funding was redirected by the Polish Government to support the Iryda programme; this was to not only to acquire additional aircraft but to finance upgrades to both the avionics and the engines. The prior month's decision to terminate the programme's backing had reportedly been overruled by Prime Minister Jozef Oleksy. According to aerospace industry periodical Flight International, Polish Air Force officials at one point were claiming the Iryda fleet to have achieved the highest serviceability statistics in the air force's inventory. However, Colonel Janusz Karpowicz of the Deblin pilot-training school criticised the Iryda for possessing longitudinally "heavy" controls, a relatively high approach speed, and the capability of its avionics.
In February 1996, the Polish Air Force grounded its Iryda fleet and froze its orders for the type following a fatal accident on 24 January of that year. The accident, which was reportedly the result of a trim-related issue, and its investigation became highly politicised. During March 1996, the Warsaw Institute of Aeronautics abandoned development of its new D-18A engine, which was intended to power future combat-orientated versions of the Iryda, reportedly due to market viability concerns. In April 1996, the programme was officially resumed in response to a fresh order from the Polish Air Force, which involved the purchase of six new-build aircraft and the retrofitting of 11 existing aircraft in air force service with improved engines, avionics and wings by 1998.
During October 1996, PZL-Mielec stated that it aimed for an upgraded prototype to be flown prior to the end of the year; the company also had ambitions to secure a follow-on order in the coming year, as well as for an modified maritime reconnaissance/strike version that were envisioned to replace the Polish Navy's fleet of MiG-21bis fighters. In June 1997, an Iryda flew for the first time with both the upgraded avionics package and the aerodynamic improvements. Full-scale flight testing of the upgraded aircraft was reportedly set to commence during August of that year; it was anticipated that the upgrade would be certified during 1998, after which the Polish Air Force would commence operational use of the type.
Relations between PZL-Meilec and the Polish Defense Ministry broke down during the latter half of 1997, cumulating in the company opting to file a law suit against the ministry over its alleged failure to honour the terms of a contract pertaining to the Iryda. While PZL-Meilec claimed that the Defense Ministry had demanded additional unfunded factory testing, the ministry accused the company of "negligence", and that the aircraft lacked necessary quality-control certification to be deemed safe for test flights. The prototype was grounded while legal action ensured.
The Polish Air Force's procurement of the Iryda was formally cancelled during 1998, allegedly in response to the development difficulties experienced as well as the protracted shortage of funding that was common around this period; a key event that had reportedly contributing to its cancellation was the fatal crash in 1996. During the summer of 2002, PZL-Mielec relaunched development of the type, resuming flights of the Iryda on 22 July of that year, while attempting to gain interest and secure orders. Dubbed Iskra 2, it received a new Thales-supplied avionics suite and featured underwing hard points to enable the carriage of armaments, external fuel tanks, and other equipment.
- 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)
- Empty weight: 4,600 kg (10,141 lb)
- Gross weight: 6,650 kg (14,661 lb)
- Max takeoff weight: 7,500 kg (16,535 lb)
- Powerplant: 2 × PZL K-15 turbojet engines, 14.7 kN (3,300 lbf) thrust each
- 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
Aircraft of comparable role, configuration and era
- Dassault-Breguet/Dornier Alpha Jet
- Aero L-39 Albatros
- BAE Hawk
- Soko G-4 Super Galeb
- FMA IA 63 Pampa
- Kawasaki T-4
|Wikimedia Commons has media related to PZL I-22 Iryda.|
- Jeziorski, Andrzej (17 May 1995). "Mielec delivers first K-15 Irydas". Flight International.
- Jeziorski, Andrzej (13 December 1995). "Poland puts brakes on Alpha Jet deal". Flight International.
- "Poland resurrects support for Iryda". Flight International. 3 January 1996.
- Jeziorski, Andrzej (28 February 1996). "Poles freeze Iryda orders after crash". Flight International.
- Jeziorski, Andrzej (13 March 1996). "IL abandons D-18A engine". Flight International.
- Jeziorski, Andrzej (24 April 1996). "Polish air force revives troubled Iryda". Flight International.
- Jeziorski, Andrzej (30 October 1996). "PZL-Mielec aims to fly modified Iryda I-22 'by the end of year'". Flight International.
- "System installed". Flight International. 17 June 1997.
- "PZL will test upgraded Iryda in August". Flight International. 23 July 1997.
- Jeziorski, Andrzej (28 January 1998). "Iryda teeters as Mielec decides to sue Polish defence ministry". Flight International.
- Jaxa-Malachowski, Ryszard (30 July 2002). "Poland's Iryda flies again, but now renamed Iskra 2". Flight International.
- Instytut Lotnictwa (12 July 2006). "Samolot szkolno-bojowy I-22 Iryda". Nasze osiągniecia. Archived from the original on 15 July 2006. Retrieved 12 July 2006.