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Two - Seat side-by-side
all metal motor gilder |
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Suitable for school,
training and touring purposes |
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Utility category aircraft,
including : |
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ROTAX 912 A3 engine |
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HO-V352F-S1 / S1 70FQ Hoffmann variable
pitch, “constant speed ” propeller |
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Main landing gear damped and semi-retractable
and steerable tail wheel |
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wheel brake for left
pilot |
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Safety harnesses |
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4 flaps positions control |
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elevator connection-
automatic type |
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external paint, as per
BUYER’s choice |
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rubber pedals |
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Standard panel instrument
: Oil temperature indicator, oil pressure gauge,
engine r.p.m. indicator, cylinder head temperature
indicator, air-speed indicator, altimeter, variometer,
compass, voltammeter. |
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Batch 1/1 |
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Type Certificates :
Romanian and German (LBA) , as per JAR- 22 |
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Performances |
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Var.Pitch Propeller |
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HO n-V352F - SI/S170FQ |
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Power Plant |
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ROTAX 912A3 |
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Max.Continuous Power
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81 HP |
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Climbing Speed at Sea
Level |
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3.2 m/s |
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Max.Cruising Speed (at
1,000 m ) |
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200Km/ h |
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Economical Cruising
Speed ( at 1,000m) |
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155 km/ h |
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Take -Off Distance (15
m obstacle, grassy ground, at 560 m ) |
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490 m |
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Service Ceilling |
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6,200 m |
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Never Exceed Speed |
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220 km/ h |
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Sink Speed at 80 km/
h |
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1/15m/ s |
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Range (no fuel reserve) |
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700 Km |
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Load Factors |
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+5.3g; -2.65g |
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Fuel Tank Capacity |
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551 |
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