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THK-5

From Alfawiki
THK (Turkish Aeronautical Association)
IndustryAerospace
Founded1945
Headquarters
Turkey


Template:Infobox aircraft

The THK-5 was a twin-engine airplane created by Stanisław Rogalski and constructed in Turkey in 1945, primarily serving as an air ambulance.[1][2] This aircraft featured a traditional low-wing cantilever monoplane design, with an all-wooden structure. Its tailwheel landing gear had main units that retracted into the engine nacelles mounted on the wings. The THK-5 was capable of accommodating two stretchers along with a medical attendant. Subsequently, a six-seat utility transport variant called the THK-5A entered production,[2] followed by an enhanced model of the 5A, known as the THK-10, of which three units were built.[3] One unit was exported and sold to Denmark.

Following the acquisition of THK by MKEK, this design was chosen for further development. Although it was assigned the designation MKEK-5,[1] no additional progress was made on this project.[3]

Variants

THK-5
Designed as an air ambulance, this model accommodates two stretchers along with a medical attendant.
THK-5A
A utility transport variant with seating capacity for six passengers.
THK-10
An enhanced iteration of the THK-5A, with a total of three units constructed.
MKEK-5
Following the acquisition of THK by Makina ve Kimya Endüstrisi Kurumu (MKEK), the THK-5, THK-5A, and THK-10 were redesignated under this new designation; however, no additional development ensued.

Specifications (THK-5A)

Template:Aircraft specs

References

  1. ↑ 1.0 1.1 Cite error: Invalid <ref> tag; no text was provided for refs named JEA
  2. ↑ 2.0 2.1 Cite error: Invalid <ref> tag; no text was provided for refs named Flight
  3. ↑ 3.0 3.1 Cite error: Invalid <ref> tag; no text was provided for refs named Deniz

Bibliography

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