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Zenair - Zenith, Zenith Aircraft Company
and AMD Aircraft Family
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ZODIAC XL CH 601 |
STOL CH 701 SP |
STOL CH 801 |
ZODIAC CH 640 |
AMD Alarus |
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Ecolight
ready! |
Ecolight
compliant! |
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Certification Matrix
(Switzerland)
| (c) 2003, Sport Aviation LLC |
Experimental Aircraft
Kit |
Ecolight Cat. A
(LTF-UL1) |
Ecolight Cat. B
(LSA2) |
JAR-VLA |
FAR-23/JAR23 |
Seats |
Pilot's License
(Switzerland) |
| Zodiac XL CH 601 |
YES |
YES3,5 |
YES4,6 |
- |
- |
2 |
JAR-PPL
R-PPL |
| Zodiac CH 601 HD8 |
YES |
- |
- |
- |
- |
2 |
JAR-PPL
R-PPL |
| Super Zodiac CH 601 HDS8 |
YES |
- |
- |
- |
- |
2 |
JAR-PPL
R-PPL |
| Zodiac CH 601 UL8 |
YES |
- |
- |
- |
- |
2 |
JAR-PPL
R-PPL |
| CH 701 SP STOL |
YES |
YES3,5,7 |
YES4,6,7 |
- |
- |
2 |
JAR-PPL
R-PPL |
| CH 801 STOL |
YES |
- |
- |
- |
- |
4 |
JAR-PPL
R-PPL |
| Zodiac CH 640 |
YES |
- |
- |
- |
- |
4 |
JAR-PPL
R-PPL |
| AMD Alarus CH 2000 |
NO |
- |
- |
- |
YES/YES |
2 |
JAR-PPL
R-PPL |
| 1 |
LTF-UL |
Lufttüchtigkeitsanforderungen
für aerodynamisch gesteuerte Ultraleichtflugzeuge 30. Jan. 2003 |
| 2 |
LSA |
Light Sport Airplane - Sport Pilot (USA) |
| 2 |
EASA-UL |
EASA Advanced NPA - European Sport/Recreational
Aviation Standard Proposal |
| 2 |
LSA |
U.S. Light Sport Airplane - Sport Pilot - details
still open and unspecified |
| 3 |
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LTF-UL compliant, German LTF-UL certification
pending |
| 4 |
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Sport Pilot ready, Swiss Ecolight Cat. B / U.S.
Light Sport Airplane certification pending |
| 5 |
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Swiss Ecolight Cat. A / LTF-UL certification
pending |
| 6 |
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Swiss Ecolight Cat. B certification pending |
| 7 |
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Actually no plan to certify in the Swiss Ecolight
Class - Please ask if you have a specific demand |
| 8 |
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For reference only, on most aspects the CH 601 XL
exceeds these aircraft |
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Specification Overview
| (c) 2003, Sport Aviation |
Category |
MTOM
[lbs / kg] |
Design Payload10
[lbs / kg] |
Design Load at MTOM |
Cruise Speed (75 %)
[mph / km/h] |
max. Speed (Vne)
[mph / km/h] |
Engine
[PS] |
Fuel
[US Gal/kg] |
Range12,14
[sm / km] |
Endurance12,14
[h] |
ZODIAC XL
CH 601 |
Ecolight LTF-UL11 |
1040 / 472.5 |
252 / 115 |
+6.4, -6.4
ultimate |
134 / 216 |
180 / 290 |
Rotax 912ULS
100 |
24 / 65 |
650 / 1040 |
4.9 |
| Ecolight LSA12 |
1232 / 560 |
444 / 202.5
(912ULS) |
132 / 21417 |
Rotax 912ULS
100, or
Jabiru 3300
110, or
Lycoming O-235
125 |
ZODIAC XL
CH 601 XL (Kit) |
Experimental (Kit) |
1300 / 590 |
496 / 225
(912ULS) |
+6.0, -6.0
ultimate |
134 / 216 |
180 / 290 |
Rotax 912ULS
100 |
24 / 65 |
656 / 1056 |
4.9 |
| 138 / 222 |
Jabiru 3300
110 |
662 / 1065 |
4.8 |
| 138 / 222 |
Lycoming O-235
125 |
575 / 925 |
4.2 |
| STOL CH 701 SP |
Ecolight LTF-UL11 |
1040 / 472.5 |
291 / 133 |
+6.0, -3.0
ultimate |
80 / 129 |
110 / 177 |
Rotax 912
80, or
Rotax 582
65 |
20 / 54 |
400 / 640 |
4.0 |
| Ecolight LSA12 |
1232 / 560 |
483 / 220.5 |
| STOL CH 701 SP (Kit) |
Experimental (Kit) |
1232 / 560 |
533 / 241.5 |
+6.0, -3.0
ultimate |
80 / 129 |
110 / 177 |
Rotax 912
80, or
Rotax 912ULS
100 |
20 / 54 |
400 / 640 |
4.0 |
| STOL CH 801 |
Experimental (Kit) |
2200 / 100016 |
800 / 360 |
+5.7, -2.8
ultimate |
120 / 193 |
150 / 240 |
150..240
(e.g. O-360-A, Walter-LOM M332B, M337A, M337B, PZL-Franklin
6A-350-C1R) |
30 / 80 |
315 / 50715
(630 / 1015 ext. range option)15 |
3.015
(6.0 ext. range option)15 |
| Zodiac CH 640 (Kit) |
Experimental (Kit) |
2200 / 100016 |
823 / 360
(4 x 205 / 4 x 90) |
+5.7, - 2.9
ultimate |
160 / 256
(O-360) |
175 / 280 |
150..240
(max. 200 kg) |
38 / 104 (std.)
46 / 125 (ext.) |
dependant on engine |
dependant on engine |
| AMD Alarus CH 2000 |
JAR-23 |
1692 / 769 |
667 / 307 |
+4.4, -2.2 (Utility at 1616 lbs -
sustained)
+3.8, -1.9 (normal at MTOM - sustained) |
99 kts / 184 |
143 kts / 265 |
116 |
28 / |
486 / 778 |
4.0 |
| 10 |
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Pilot, Passenger(s), Baggage/Cargo - a typical
aircraft with full standard fuel |
| 11 |
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Standard ISA atmosphere, sea level, no reserve |
| 12 |
LTF-UL |
Lufttüchtigkeitsanforderungen
für aerodynamisch gesteuerte Ultraleichtflugzeuge 30. Jan. 2003 |
| 13 |
LSA |
Light Sport Airplane - Sport Pilot (USA) |
| 13 |
EASA-UL |
EASA Advanced NPA - European Sport/Recreational
Aviation Standard Proposal |
| 14 |
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with MTOM at 75% |
| 15 |
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Lycoming O-360-A, Sensenich 76-EM8-0-54 fixed
pitch prop |
| 16 |
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We recommend a "limitation" to 999 kg due to
typical European airport tax regulations |
| 17 |
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speed limited by propeller selection to meet LSA
specs |
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ZODIAC CH 601 XL
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