DINO

GANZAVIA GAK-22 Dino

Aircraft
Name
GAK-22 Dino
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufactured as
GANZAVIA GAK-22 Dino
GANZAVIA Dino

DINO

The Ganzavia GAK-22 Dino was an unusual light utility aircraft built in Hungary in the early 1990s. In configuration, it was a biplane with cantilever wings and a very pronounced negative stagger, making it almost a tandem wing design. The pilot and a single passenger sat side by side under an expansive bubble canopy, and it had fixed tricycle undercarriage. The fuselage was of welded steel tube construction, and the wings of duralumin, with the whole aircraft skinned in fabric, other than the forward fuselage which had aluminium skin.

Technical Data
Wing span (metric)
7.60 m
Length (metric)
6.20 m
Height (metric)
2.80 m
Powerplant

1 x Lycoming O-235-H2C four-cylinder horizontally opposed aircooled piston engine, 86 kW (115 hp)

Engine Model(s)
Lycoming O-235
Indicative Performance Data
Take-Off
V2
n/a
Distance
235 m
MTOW
700 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
94 kts
MACH
n/a
Ceiling
105
Range
370 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a

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