PZL-105 Flaming
| PZL-105 Flaming | |
|---|---|
| |
| PZL-105 at the Polish Aviation Museum | |
| Role | Utility aircraft |
| Manufacturer | PZL Warszawa-Okęcie |
| First flight | 9 November 1989 |
| Status | Prototype |
| Primary user | Polish civilian aviation |
| Number built | 2 (prototypes) |
PZL-105 Flaming (Template:Lang-en) is a Polish short-takeoff-and-landing (STOL) utility aircraft designed by PZL "Warszawa-Okęcie". It remained a prototype.
Development
The PZL-105 was designed as a successor to the successful utility aircraft PZL-104 Wilga, being more modern and economical and offering increased transport capacity. The design was initially called Wilga 88. It retained the high-wing layout of the PZL-104 and the upward-opening side doors, but it was a completely new aircraft. Compared with the Wilga, it has a six-seat cabin instead of four seats and the wings are supported by single struts instead of a cantilever design. The plane was intended for a variety of purposes, like glider towing, parachute training, transport, air ambulance, patrolling and crop dusting (with 500 kg of chemicals). Also, a seaplane variant was intended.
The first prototype, powered by a 265 kW (360 hp) Russian M-14P radial engine, was first flown on 9 November 1989 (markings SP-PRC). An intended designation of a serial variant was PZL-105M. The second prototype, designated PZL-105L, was fitted with a flat engine 298 kW (400 hp) Lycoming IO-720. It was flown on 27 July 1991 (markings SP-PRD). There was also made one prototype for static trials.
Problems with funding at the outbreak of the 1980s and 1990s, connected with a change of political system in Poland, and the priority of the PZL-130 Orlik trainer program, had caused the Flaming program to be suspended, and production of the type has yet to have started. The company developed a new variant of the PZL-104, the Wilga 2000 with Lycoming I0-540 flat engine instead.
Design
Metal construction braced high-wing monoplane, conventional in layout, duralumin covered. Semi-monocoque fuselage. Rectangular single-spar wings, fitted with Fowler flaps and slotted flaperons. Six-seat cabin with three rows of seats, with large side doors opening upwards. Conventional fixed landing gear with tail wheel, the main gear is made of composite spring legs. Two-blade or three-blade (PZL-105L) metal propeller. Fuel tanks in wings (270 l).
Survivors
The first prototype and the second prototype airframe (lacking engine) are in a collection of the Polish Aviation Museum in Kraków.
Specifications (PZL-105L)
Data from Jane's All The World's Aircraft 1993-94[1]
General characteristics
- Crew: 1 pilot
- Capacity: 5Fuel: 270 L (71.3 US Gallons)
Performance
See also
Related development
References
- ^ Lambert 1993, pp. 241–242.
- Andrzej Glass: Samoloty '94, Grupa IMAGE, Warsaw 1994, ISBN 83-85461-19-1
- Lambert, Mark (ed.). Jane's All The World's Aircraft 1993-94. Coulsdon, UK: Jane's Data Division, 1993. ISBN 0-7106-1066-1.
External links
