| Zenair CH 640 EXPERIMENTAL |
| >> PRESTAZIONI |
PERFORMANCE
Lycoming O-360, 180-hp
|
Load: 518 Lbs
Take-Off Weight: 1,718 Lbs.
|
Gross Weight
2,200 Lbs.
|
MAX LEVEL SPEED
|
167
MPH
|
267
km/h
|
157
MPH
|
251
km/h
|
CRUISE SPEED
(75% power @ 7,000 Ft.)
|
154
MPH
|
246
km/h
|
150
MPH
|
240
km/h
|
STALL SPEED (Flaps Down)
|
40
MPH
|
65
km/h
|
47
MPH
|
76
km/h
|
STALL SPEED (Flaps Up)
|
50
MPH
|
81
km/h
|
58
MPH
|
93
km/h
|
RATE OF CLIMB
|
1,400
FPM
|
7.0
m/s
|
950
FPM
|
4.8
m/s
|
SERVICE CEILING
|
16,000+
Ft.
|
4880+
m.
|
12,800
Ft.
|
3,900
m.
|
ENDURANCE (Standard)
|
3
Hrs. 45 min.
|
3
Hrs. 45 min.
|
RANGE (Standard)
|
525
Miles
|
845
km.
|
510
Miles
|
820
km.
|
TAKE-OFF ROLL
|
950
Ft.
|
260
m.
|
990
Ft.
|
300
m.
|
LANDING ROLL
|
800
Ft.
|
244
m.
|
1,150
Ft.
|
350
m.
|
|
Above performance figures
with the Lycoming O-360 engine (180 BHP: 390 lbs. with accessories and
fixed-pitch Sensenich 76-EM8-0-63 metal propeller).
Standard atmosphere, sea level, no wind. All technical data, specification
and performance figures subject to change without notice. Endurance and range
figures without fuel reserve.
Performance flight test
results: The following performance
figures are based on prototype flight tests (4/15/02). Aircraft as
tested: Empty weight: 1,200 lbs. with advanced avionics installed.
Basic equipped aircraft empty weight: 1,147 lbs.
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