| SPECIFICATIONS | ||
| LENGTH | 19 FEET | 5800 MM |
| HEIGHT | 5 FEET 10 IN. | 1800 MM |
| WINGSPAN | 27 FEET 3 IN. | 8300 MM |
| WING AREA | 123 SQ.FT. | 11.5 M.SQ. |
| WING LOADING | 11.8 LB/SQ.FT | 57.4 KG/M.SQ. |
| POWER LOADING | 9.0 LBS/HP | 4.1 KG/HP |
| SEATS | 2 SIDE-BY-SIDE | |
| CABIN WIDTH | 44 INCHES | 1110 MM |
| EMPTY WEIGHT | 800 LBS | 360 KG |
| MAX GROSS WEIGHT | 1450 LBS | 660 KG |
| USEFUL LOAD | 650 LBS | 300 KG |
| FUEL (STD) | 34 US GAL (205 LBS) | 130 l (93 KG) |
| ENGINE | JABIRU 2200, 4-CYL., 4-CYCLE, AIR COOLED, DIRECT DRIVE | |
| POWER | 80 HP (60 kW) @ 3300 RPM | |
| DISPLACEMENT | 2210 cc | |
| IGNITION | DUAL IGNITION, BREAKERLESS TRANSISTORIZED | |
| STARTER | ELECTRIC, 12 V | |
| FUEL CONSUMPTION | 3.75 GAL/HR | 14 l/HR |
| PROPELLERS | FIXED PITCH, 55-IN DIAM., GROUND ADJUSTABLE | |
| PERFORMANCE | ||
| TAKEOFF, GROUND ROLL | 450 FT | 137 M |
| TAKEOFF, OVER 50 FT | 850 FT | 260 M |
| RATE OF CLIMB, SL | 1280 FPM | 6.5 M/S |
| S.E. RATE OF CLIMB, SL | 300 FPM | 1.5 M/S |
| TOP SPEED | 155+ MPH | 250+ KM/H |
| CRUISE SPEED, 75% | 145 MPH | 233 KM/H |
| RANGE (NO RESERVE) | 650 MILES | 1045 KM |
| STALL SPEED (Vso) | 55 MPH | 88 KM/H |
| LANDING, GROUND ROLL | 450 FT | 137 M |
| LANDING, OVER 50 FT. | 800 FT | 244 M |
| CEILING | 12,000+ FT | 3,660+ M |
Source: Zenair Ltd. All figures are based on factory prototype flight test results, subject to change and revision.
The Gemini CH 620 project
is still under development and kits are not available. |
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© Zenith Aircraft Company: 2004-07-14
GEMINI
Your Personal
Twin-Engine
Kit Aircraft
