PZL I-22 Iryda

· PZL Mielec · 2 × PZL K-15

Airplanes

Length

13.22 m

Flat Wing Span

9.6 m

Height

4.3 m

Flat Wing Area

19.92 m²

Max Speed

940 km/h

Max Mach

0.82 Mach

Max Ceiling

13700 m

Number of Engines

Aircraft Engine

First Flight

1985-03-03

Entry Into service

1992-12-22

Number Built

Maximum Take-Off Weight

7.5 t (paragliders: kg)

Maximum Range

1200 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
PZL I-22 Iryda	7.5	1200

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Dassault/Dornier Alpha Jet	SNECMA Turbomeca Larzac	13.23	9.11	Compare
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All data (27 fields)

Name: PZL I-22 Iryda
Manufacturer: PZL Mielec
Description: 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.
ICAO Code: I22
First Flight: 1985-03-03
Entry Into service: 1992-12-22
Service End: 1996-01-01
Designer: PZL Mielec
Type: Jet trainer
Length (m): 13.22
Height (m): 4.3
Cockpit Crew: 2
Max Speed (km/h): 940
Max Ceiling (m): 13700
Rate of Climb (m/s): 40.6
Armament: 1 × 23 mm GSh-23L cannon with 200 rounds; ; FAB-250; FAB-500; ; 57 mm S-5; ; R-60; 4 × under-wing
Max Mach (Mach): 0.82
Number Built: 17
Powerplant Description: 2 × PZL K-15 turbojet engines, 14.7 kN thrust each
Primary Users: Polish Air Force
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/PZL_I-22_Iryda
Flat Wing Span (m): 9.6
Flat Wing Area (m²): 19.92
Wake Category: M
Aircraft Engine: PZL K-15
Number of Engines: 2