| GENERAL |
GENERAL | ENGINES | INSTRUMENTS | TECHNICAL SPECIFICATIONS | PERFORMANCE |
| Seating |
Two side by side bucket seats, adjustable in length, equipped with a 4-point safety harness |
| Cockpit |
Open sided cockpit module with Lexan windscreen fitted to roof panel |
| Undercarriage |
The suspension system is manufactured from 4130 Chrome Moly steel tubing. 13" pneumatic tyres are fitted to the main undercarriage. The T600T has a solid 5" tailwheel and the main wheels are equipped with cable-operated drum brakes or optional disc brakes. The T600N has a nosewheel controlled via push rods connected to the rudder pedals.
|
| Wing |
Monoplane with double surface high wing. Aerodynamic airfoil struts support each wing and are braced by jury struts. |
| Controls |
Full 3-axis operated by conventional centre mounted joystick and dual rudder pedals. |
| Fuel Tank |
50 litre aluminium tank. |
| Materials |
Fittings are manufactured from 316 stainless steel. All other steel parts are manufactured from 4130 chrome Moly steel and powder coated in satin black. All aluminium tubing is clear anodised.
A.N. aircraft grade bolts and hardware are used thorughout the airframe. Wing and control surface skins are made from UV treated Dacron or Ultralam available in several colours. |
| ENGINES |
GENERAL | ENGINES | INSTRUMENTS | TECHNICAL SPECIFICATIONS | PERFORMANCE |
| Type |
Rotax 582 water cooled 2-stroke.
Jabiru 2200A 80HP 4-stroke.
All tractor configuration. |
| Gearbox |
'E' type. Electric start on the 582. (Direct drive on the Jabiru). |
| Propellors |
Brolga 3-blade composite 68" diameter ground adjustable or Warpdrive composite 68" 2-Blade fitted to Jabiru. |
Additional
Features |
Rectifier regulator. Remote choke valves. Electric fuel pump. Lord engine mounts for effective vibration damping. |
| INSTRUMENTS |
GENERAL | ENGINES | INSTRUMENTS | TECHNICAL SPECIFICATIONS | PERFORMANCE |
| Standard: |
0-120 knots ASI. 0-20,000ft altimeter. Slip indicator. 0-8000rpm tachometer. (0-4000 rpm on Jabiru)
Dual EGT gauge with probes. |
| TECHNICAL SPECIFICATIONS | GENERAL | ENGINES | INSTRUMENTS | TECHNICAL SPECIFICATIONS | PERFORMANCE |
| Dimensions |
| Length |
 |
5.8m |
| Wing Span |
|
9.6m |
| Wing Area |
|
15.692m2 |
| Wing Loading (MTOW) |
|
[450 kg] 28.67Kg/m2 |
| Total Fin Height |
|
2.4m (T600N) 1.66m (T600T) |
|
| Max. Weight |
| Dry Empty Weight |
|
(T600T) 187kg |
| Max Take Off Weight |
|
450Kg |
|
| Fuel Capacity |
50L on both the T600N and T600T |
| Performance |
|
| Engine |
Rotax 582 'E' Gearbox |
Jabiru 2200A |
|
3-blade Brolga propellor |
Direct Drive with G.T. Propellor |
| VNE |
80kts 92 mph |
102kts 117mph |
| Max Level |
76kts 86 mph |
90kts 103mph |
| Stall at MTOW |
34kts 39 mph |
35kts 40 mph |
| Cruise at 5200 rpm |
60kts 68 mph |
65kts 75 mph |
| Roll Rate |
1.5 secs 45deg - 45 deg |
1.5 secs 45deg - 45 deg |
| Rate of Climb at MTOW |
(2 occupants) 800 ft/min
(pilot only) 1200 ft/min |
(2 occupants) 800 ft/min
(pilot only) 1200 ft/min |
| Sink at MTOW |
(2 occupants) 650 ft/min
(pilot only) 425 ft/min |
(2 occupants) 650 ft/min
(pilot only) 425 ft/min |
Thruster T600N 582 Sprint Specifications (New August 2003)
|
- Fully enclosed 2-seat cockpit and fuselage
- High wing, three axis, nosewheel aircraft
- Maximum take-off weight is 450kg
- Ultralam skins fitted as standard
|
|
- Rotax 582 DCDI, 'E' type gearbox (ratio 3:1), 2-stroke, 65hp
|
|
- Brolga, 3-bladed, 68" Composite, 17 degree pitch blocks
|
|
- ASI, VSI, Altimeter, Compass, Slip Indicator, Dual EGT and Tacho
|
|
- Cruise - 60Kts @ 5000rpm / 70 Kts @ 5600rpm
- VNE - 102 Kts @ 6450rpm
- Climb rate - 750ft/min @ MTOW
- Descent rate - 450ft/min @ MTOW
|
|
- 12 litres/hour @ 5600rpm ~ 70 Kts
- 10 litres/hour @ 5000rpm ~ 70 Kts
|
|
- £22,250 +VAT + Registration + Permit
|
|
- Disc brakes - +£600.0
- Fuel Computer - +£325.00
- Strobes - +£275.00
|
|
