| Wing Span .................. 19.00 ft. |
Range ............................ 120 sm |
|
Wing Area ................... 140.0 sq. ft. |
Takeoff Dist . ................. 200 ft. |
|
Length ......................... 15.80 ft. |
Landing Dist . ................ 275 ft. |
|
Max Gross Wt . ............ 700 lbs. |
VNE ............................. 80 mph |
|
Empty Wt . .................... 495 lbs. |
Cruise............................ 68 mph |
|
Payload (full fuel) ...... 205 lbs. |
Stall.................. ............ 35 mph |
|
Fuel Capacity ............. 12 gal. |
Climb Rate @msI............ 850 fpm |
|
Seats ...........................1 |
Service Ceiling ............ 9,000 ft. |
|
Cabin Width ................ 21 in. |
|
|
Engine 40-95 hp |
Construction: Aluminium tube, Fabric |
|
Plans
$250.00 |
Est. Bldg. Time 800 hrs. |
|
Bi-plane designed by Bert Howland
using a TIG welded fuselage frame of 3/4" square
aluminium 6061-T6 tubing,
instead of gussets and rivets. Plans are 40 engineering drawings in
17"x 11" format and construction notes. |
|
CLASSIC AERO ENTERPRISES
343 Wrexham Ct.,
Hampton VA 23669
Tel. 757-851-2856
|
