The PIK-19 Muhinu was a light aircraft developed in Finland in the early 1970s for use as a glider tug and flight trainer. [1] It was a low-wing cantilever monoplane of conventional configuration, with an enclosed cockpit and fixed, tricycle undercarriage. [1] Its construction was of composite materials throughout, [2] a novel approach at the ...

PIK-19 Muhinu (lyhenne sanoista Muovihinauskone) oli suomalainen Teknillisen korkeakoulun lentotekniikan laboratorion suunnittelema ja valmistama komposiittirakenteinen yksimoottorinen purjelentokoneiden hinauskone.

The PIK-19 Muhinu was a light aircraft developed in Finland in the early 1970s for use as a glider tug and flight trainer. It was a low-wing cantilever monoplan...

PIK-19 ”Muhinu” (M) Muhinu oli ensimmäinen TKK:n uudenuutukaisessa kevytrakennetekniikan laboratoriossa suunniteltu ja rakennettu lentokone. Suunnittelusta vastasivat pääasiassa Jukka Tervamäki, Ilkka Rantasalo ja Pekka Tammi. Suunnittelu alkoi v. 1969 ja ensilento oli 26.3.1972.

2023年11月13日 · The PIK-19 Muhinu was a light aircraft developed in Finland in the early 1970s for use as a glider tug and flight trainer. It was a low-wing cantilever monoplane of conventional configuration, with an enclosed cockpit and fixed, tricycle undercarriage.

The PIK-19 Muhinu was a light aircraft developed in Finland in the early 1970s for use as a glider tug and flight trainer. It was a low-wing cantilever monoplane of conventional configuration with an enclosed cockpit and fixed tricycle undercarriage.

Two seat glider towplane, Finnish design. Manufactured 1972, destroyed 1993. [Nikkormat FTn] - Photo taken at Helsinki - Malmi (HEM / EFHF) in Finland on April 25, 1974.

The ICAO (International Civil Aviation Organization) Doc 8643 document contains designators for those aircraft types which are most commonly provided with air traffic service (ATS)

Two seat glider towplane, Finnish design. Manufactured 1972, destroyed 1993. [Smena 8]

Specifications. Data from Jane's All the World's Aircraft 1974-75. General characteristics. Crew: Two Length: 6.90 m (22 ft 8 in) Wingspan: 10.00 m (32 ft 10 in) Height: 2.60 m (8 ft 6 in) Wing area: 14.00 m2 (150.7 sq ft) Aspect ratio: 7.14 Airfoil: NACA 63 2 415 Empty weight: 560 kg (1,235 lb) equipped Max takeoff weight: 840 kg (1,852 lb) Fuel capacity: 150 L …