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MICRO MONG
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Single-engine, single-seat aircraft, intended for sport-recreational and tourist flying with limitations for non-acrobatic operation, category special. Biplane with struts and reinforcing cables with engine in towing configuration and fibreglass ground adjustable propeller. The cabin is open with access from the top. The landing gear is of the classic stern type. The entire structure is a combination of chrome-molybdenum thin-walled tubes, canvas and duralumin wing spars.
Advertisement type:
Offer
Manufacturer:
Plučinsky
Type:
Micro Mong
Date of manufacture:
1998
MTOW:
up to 450 kg
Airframe HOBBS:
500
Engine HOBBS:
5
Propeller HOBBS:
100
Engine:
Rotax 532
Power:
47 kW
Fuel tank capacity:
35 L
Consumption (LPH):
15
Propeller:
ground adjustable
Flaps:
N/A
Cruise speed:
140 km/hod.
Never exceed speed (Vne):
160 km/hod.
Landing gear:
fidex
COM radio:
N/A
Transponder (XPDR):
N/A
ELT:
No
Rescue system:
No
Construction:
steel
Instruments:
Basic
Owners count:
1
Other equipment:
aircraft flight log book, engine log book, fuel valve, mechanic brakes