Saturday, May 14, 2011

EAA Chapter meeting - June

The meeting in June will be at Russ Roberts Hangar at the Cedar City Airport (KCDC).  Russ has a Zenith STOL CH750 aircraft that meets the LSA category.  The specs for this aircraft are as follows:



(Based on factory prototype, equipped with 100-hp Continental O-200 powerplant)

WING SPAN 29 FT. 10 In. 9.1 m.

HEIGHT (rudder tip) 8 Ft. 8 In. 2.6 m.

WING AREA 144 SQ.FT. 13.4 m.sq.

WING CHORD 4 Ft. 10 In. 1.5 m.

LENGTH 21 Ft. 10 In. 6.7 m.

HORIZONTAL TAIL SPAN 8 Ft. 5 In. 2.6 m.

HORIZONTAL TAIL AREA 22.2 Sq. Ft. 2.0 m.sq.

EMPTY WEIGHT 775 LBS. 350 kg.

DESIGN GROSS WEIGHT (Edition 2) 1,440 LBS. 652 kg.

GROSS WEIGHT (LSA Limit) 1,320 LBS. 600 kg.

USEFUL LOAD (LSA) 545 LBS. 250 kg.

WING LOADING (LSA) 9.15 LBS/FT² 44.8 m²

POWER LOADING (LSA) 13.2 LBS/BHP 6.0 kg/BHP

DESIGN LOAD FACTOR (ultimate) +6 G / -3 G

NEVER EXCEED SPEED (VNE) 125 MPH 200 km/h

CABIN WIDTH 42 INCHES 100 cm.

CABIN WIDTH (bubble doors) 50 INCHES 1.27 m.

FUEL CAPACITY (std., dual wing tanks) 24 US Gallons (2 x 12 gal.)
SUITABLE POWER / Max Engine Weight 80 - 140 hp. / 300 lbs. installed


Look at this video for the amazing take-off and landing capabilities of this aircraft:

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