| SIGMA ELITAR 2009 WWW.SIGMAELITAR.COM
$75,000.00
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| Posted/updated on: 11/4/2009 7:13:50 PM
MST |
| Category: Other Aircraft
Sub-Category: Light Sport Aircraft |
| Location: WINTER HAVEN,FLORIDA |
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| Contact Seller:
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| Description: |
Sigma Elitar is improved modification of Sigma 4 aircraft due to shift from handicraft (single piece) production to factory (series) production.
Due to shift to series production the following changes we made in the process of the aircraft manufacturing:
 - conductor and stack production
- manufactured products are double quality controlled
- all fiberglass parts are thermally processed in electronically controlled heating cabinet
- due to vacuum treatment technology improvement weight of each wing planes was decreased by 12 kg
- landing gear manufacturing technology change allowed to improve take off and landing characteristics, and decrease landing gear leg weight by 2.8 kg, and also absorb landing shock
- all vital components laboratory testing for conformity
- standards table reduction due to technological processes specification from 3800 to 910 items
- parts interchangeability due to conduct and stack production assembling
- connection through bushings with class openings of all wearing surfaces, allowing to increase flight life of the aircraft.
DIMENSIONS
| Wing span |
9.8 m |
32.15 ft |
| Length |
5.96 m |
19.55 ft |
| Height |
2.92 m |
9.58 ft |
PILOTS COCKPIT
| Length |
4.84 m |
15.87 ft |
| Width |
1.22 m |
4 ft |
| Height |
1.25 m |
4.10 ft |
| Number of seats |
2 pers. |
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AIRSPEED
| Maximum permissible operating flight speed |
240 km/h |
149 mph |
| Maximum cruising speed |
210 km/h |
130 mph |
| Maximum maneuvering speed |
170 km/h |
105 mph |
MAXIMUM PERMISSIBLE WIND SPEED
AND WEATHER MINIMUM
| Head wind during takeoff and landing |
10 m/s |
22 mph |
| Tail wind during takeoff and landing |
5 m/s |
11 mph |
| Cross-wind component at right angle to runway |
5 m/s |
11 mph |
| Cloud ceiling, at least |
150 m |
492 ft |
| Horizontal visibility, at least |
3000 m |
9840 ft |
ENGINE, BRIEF DESCRIPTION
| Engine manufacturer |
BOMBARDIER-ROTAX (Austria) |
| Type of engine |
four-stroke, with four opposed cylinders |
| Make of engine |
ROTAX-912ULS |
| Cooling |
composite water-air |
| Engine power, hp (kW): |
| - maximum takeoff |
100 (73, 9) at crankshaft rotation frequency of 5800 rpm |
| - nominal |
93 (69) at CS rotation frequency of 5500 rpm |
| - in cruising mode |
68, 5 (51) at CS rotation frequency of 5000 rpm |
LIMITATIONS
| Maximum takeoff weight: |
600 kg |
1300 lbs |
| Maximum landing weight: |
600 kg |
1300 lbs |
| Maximum payload |
216, 5 kg |
477 lbs |
| Maximum aircraft operational empty weight: |
383, 5 kg |
845 lbs |
| Gas type |
Auto gas, premium |
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| Fuel tank capacity |
65 L |
17.1 Gal |
| Takeoff run |
70 m |
230 ft |
| Flight range |
650 km |
404 mi | | | |
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| PICTURES (click on pictures for a
larger view): |
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