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RC
Scale Model
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The following
specification figures are based on the prototype ZODIAC XL, and are for the standard kit ('experimental')
model.
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SPECIFICATIONS
ZODIAC CH601 XL |
Jabiru
3300
(110 hp @ 3000 rpm) |
Rotax
912S
(100 hp) |
Lycoming
O-235
(116 hp) |
| WING
SPAN |
27
FT. |
8.23
m. |
27
FT. |
8.23
m. |
27
FT. |
8.23
m. |
| WING
AREA |
132
SQ.
FT. |
12.3
m.sq.
|
132
SQ.
FT. |
12.3
m.sq.
|
132
SQ.
FT. |
12.3
m.sq. |
| LENGTH
|
20
FT. |
6.1
m. |
20
FT. |
6.1
m. |
20
FT. |
6.1
m. |
| HORIZONTAL
TAIL SPAN |
7
FT. 7 IN. |
2.30
m. |
7
FT. 7 IN. |
2.30
m. |
7
FT. 7 IN. |
2.30
m. |
| RUDDER
TIP HEIGHT |
6
FT. 6 IN. |
1.98
m. |
6
FT. 6 IN. |
1.98
m. |
6
FT. 6 IN. |
1.98
m. |
| EMPTY
WEIGHT |
695
LB. |
318
kg. |
690
LB. |
312
kg. |
800
LB. |
362
kg. |
| USEFUL
LOAD |
625
LB. |
282
kg. |
630
LB. |
285
kg. |
520
LB. |
235
kg. |
| GROSS
WEIGHT |
1,320
LB. |
595
kg. |
1,320
LB. |
595
kg. |
1,320
LB. |
595
kg. |
| WING
LOADING |
9.85
psf |
48
kg/sq.m. |
9.85
psf |
48
kg/sq.m. |
9.85
psf |
48
kg/sq.m. |
| FUEL
CAPACITY (wing tanks) |
= 24 Gal. (US) |
2
x 46 l.
= 92 l. |
= 24 Gal. (US) |
2
x 46 l.
= 92 l. |
= 24 Gal. (US) |
2
x 46 l.
= 92 l. |
| POWER
LOADING |
11.8
LB./HP |
5.3
kg/HP |
13
LB./HP |
5.9
kg/HP |
11.2
LB./HP |
5.1
kg/HP |
| CABIN
WIDTH |
44
INCHES |
112
cm. |
44
INCHES |
112
cm. |
44
INCHES |
112
cm. |
| LOAD FACTOR
(G) ultimate |
+/-
6 g |
+/-
6 g |
+/-
6 g |



NOTE:
Specification figures are based on standard factory prototype test results, and are
subject to change and revision without prior notice.
SPORT PILOT
READY* ZODIAC XL: The
standard ZODIAC XL kit aircraft meets the definition of a Light-Sport
Aircraft as defined by "Certification of Aircraft and Airmen for the
Operation of Light-Sport Aircraft" (7/20/04). A Sport Pilot may fly
any aircraft that meets the definition of a Light-Sport Aircraft, and such
aircraft does not need to change its certification category to be operated
by a Sport Pilot. Zenith
Aircraft Company cannot guarantee that the aircraft, as constructed by the
builder, will meet the definition of a Light-Sport Aircraft. Due to the
gross weight and stall speed limitations of the proposed Sport Pilot /
Light-Sport Aircraft category, it is recommended that the aircraft be kept
"as light as possible" if planning to operate the aircraft in
this category. Larger and heavier engines and other installed equipment
will limit the useful load of the aircraft, and may disqualify the
aircraft from meeting the defined category limits.
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