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JUNQUA AIRCRAFT

http://www.junqua-aircraft.com/

Ibis

ibis.jpg (53751 bytes)

 

 

"All wood" construction with additional styrofoam

 

Overall length

4.90 m / 16 ft

Overall wing span

6.30 m / 20.66 ft

Vertical stabilizer height

1.76 m / 5.6 ft

Fuselage width

0.64 m / 26 in

Cabin height

1.04 m / 3.15 ft

Cabin width at pilot elbow

0.64 m / 26 in.

Swep wing rectangular without dihedral

 

Canard wing rectangular and rectilinear

 

Main wing equipped with "flaperons"

 

Dual controls (push-pull tubes)

 

Nose wheel steering coupled to the rudder pedals
(fixed landing gear)

 

Cabin heated, brakes on rear-weels

 

Main landing gear of laminated wood

 

12 V alternator powered electrical system

 

VHF, VOR (or GPS NAV) - transponder

 

Fuel tanks in wing leading edge

60 liters / 16.2 US.G

Electrical contents indication

 

Internal luggage stowage behind passenger head

 

One-piece canopy, opens laterally (special "IBIS" canopy)

 


Max. take-off weight

470 kg (VZ 3.5 m/s) - 1034 lbs

Empty weight with starter equipment

260 kg - 572 lbs

Payload (full fuel)

170 kg - 374 lbs

Front pilot weight limits

65/95 kg - 143/209 lbs

G-loading

+4.5 and -3.0

Max. speed (VMO)

260 km/h (140kts) - 161 mph

Approach speed

120 km/h (65 kts) - 74 mph

Stall speed

95 km/h (52 kts) - 59 mph

Normal cruise

65% 200 km/h (108 kts) - 124 mph

Long range cruise

180 km/h (97 kts) - 112 mph

Max. range

900 km (485 Nms) + VFR reserves - 559 SM

Takeoff distance

1000 ft

Landing distance

1050 ft

Climb rate (VW 1835 CC)

700 fpm at M.T.O. weight.

Service ceiling

depends on the engine power