| Zenair CH 640 EXPERIMENTAL |
| >> SPECIFICHE TECNICHE |
SPECIFICATIONS
|
ZODIAC CH 640
|
LENGTH
|
23 Ft.
|
7.01 m.
|
HEIGHT
|
7 Ft. 4 In.
|
2.25 m.
|
WING SPAN
|
31 Ft. 6 In.
|
9.6 m.
|
WING AREA
|
150 SQ.FT.
|
14 m.sq.
|
WING CHORD
|
4 Ft. 9.5 In.
|
1.46 m.
|
HORIZONTAL TAIL SPAN
|
9 Ft. 10 In.
|
3.0 m.
|
HORIZONTAL TAIL AREA
|
30 SQ.FT.
|
2.8 m.sq..
|
EMPTY WEIGHT*
|
1,147 LBS.
|
545 kg.
|
DESIGN GROSS WEIGHT
|
2,200 LBS.
|
1000 kg.
|
USEFUL LOAD
|
1,053 LBS.
|
454 kg.
|
FUEL CAPACITY (Standard)
- Fuel weight (Standard)
|
38 Gal. (2 x
19)
= 230 LBS.
|
144 l. (2 x 72)
= 104 kg.
|
FUEL CAPACITY (Extended Range Option)
- Fuel weight (Extended Range Option)
|
46 Gal. (2 x
23)
= 275 LBS.
|
174 l. (2 x 87)
= 125 kg.
|
DESIGN PAYLOAD
- Occupants + Baggage / Cargo
|
823 LBS.
= 4 X 205 lbs.
|
360 kg.
= 4 X 90 kg.
|
WING LOADING
|
14.6
LBS/FT²
|
71.4 kg/m²
|
POWER LOADING
|
12.2 LBS/BHP
|
5.55 kg/BHP
|
CABIN WIDTH
|
46 INCHES
|
117 cm.
|
CABIN LENGTH (rear seat back to rudder pedals)
|
74 INCHES
|
188 cm.
|
|
| Prototype aircraft equipped with the Lycoming O-360 (with 60 amp alternator,
starter, Gill 35 battery, seats with upholstery, 600 x 6 main wheels with
dual caliper brakes, 500 x 5 nosewheel, metal fixed
pitch propeller, complete night flight package (lighting system), and
instrument gyros. Other installed equipment will effect empty weight of the aircraft. |
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