
J230D

The Jabiru J230-D is the latest development of the popular Jabiru J230 factory built Light Sport Aircraft Range
Responding to customer feedback on the J230-C we have improved the J230-D in several key areas:
A thinner centre console makes better use of the interior space
J160-C style control stick is more comfortable and allows instructors a better grip.
Modifications to the instrument panels gives improved knee
room.
Certifying the aircraft to ASTM 2245-06 standards allows for the option of Night-VFR operations – making a J230-D the first factory built Jabiru able to fly at night (when optioned with the Night package & VH registered).
These changes have been made without affecting the J230-C’s traditional strengths of value, reliability, simplicity, speed, comfort and Room. It still has the J230-C’s excellent interior room and a huge baggage compartment – it is the same fuselage as the J430 but the J430’s rear seats are not
fitted. It can be RAA or VH registered.
Features include:
- Conventional configuration
- Designed to ASTM 2245-06 Airworthiness Standard
High-winged, strut-braced monoplane with wing flaps, mass balanced rudder & elevator and in-flight adjustable trim.
- Cruise Speed @ 2870 rpm 120 knots Range (nil reserve) - 800 nautical miles
- 4 stroke JABIRU 3300 cc engine designed specifically for the Jabiru aircraft.
- Gentle and predictable stall characteristics, together with light and responsive controls, make JABIRU a true sport aircraft.
- Stall speed without flaps at Gross Weight 45 KCAS
- Fully enclosed, ergonomically designed cabin with 3 doors providing ease of entry for baggage stowage.
- Excellent visibility
- Side-by side fixed seating with centre controls and panel mounted throttles. Ideal for training or recreation.
- Tricycle undercarriage with steerable nosewheel and hand operated in line hydraulic disc brakes makes ground handling a breeze.
- Excellent cross wind handling performance – 14 knots
- All composite construction removes the corrosion problem.
- Wing and power loadings provide high performance and handling, particularly in turbulence.
- Removable Seat Covers.
- Designed for minimum maintenance. Upper and lower cowls easily removed.
- Auxiliary electronic fuel pump for ease of starting and added security in flight.
- All the engine management features of conventional GA light aircraft: Carburettor Air Heat, Dual Ignition, Pressure Compensating Carburettor – no mixture control !
- Jabiru fixed pitch wooden propeller with composite cover and urethane leading edge
- Avionics include VHF Transceiver, PM501 Intercom and headsets Transponder Altitude Encoder optional
- 4 Options for instrument panels see: Instrument Panels
- Tinted windscreen
- Steerable nose wheel
- Electrically operated flaps
- Cast aluminium 500 x 6 wheels and 6 ply tyres with spats
- Fully upholstered cockpit
- Cabin Heater
- Choice of decals and registration numbers (from the standard range)
- 135 litre fuel tanks (wing tanks & header tanks)
- Optional adjustable foot pedals to cater for pilots who have difficulties reaching the pedals
- Tool Kit
Jabiru J230D Specifications
Aircraft Type |
J230D |
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| Engine |
Jabiru 3300cc |
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120hp |
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6 cylinder, 4 stroke |
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| Propeller |
2 Blade Fixed Pitch |
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Wooden/Composite |
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60”dia x 53” pitch |
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| Height |
2400 mm (94.48”) |
| Length |
6550 mm (257.8”) |
| Width Tailplane |
2660 mm (104.7”) |
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| Cabin Width |
1120 mm (44.09”) |
| Cabin Height |
1090 mm (42.9”) |
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| Wing Span |
9433 mm (30.9’) |
| Wing Area |
9.34 sqm 100.5sq.ft) |
| Wing Loading Gross (600kg) |
13.13lbs/sq.ft |
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| Aspect Ratio |
9.5 |
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| Speeds (KCAS) |
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| Va (Max. Maneuver) |
90 kts (104 mph) |
| Max Cruise |
120 kts (138 mph) |
| Max. Straight & Level |
120 kts (138 mph) |
| Vne (Never Exceed Speed) |
140 kts ( 161 mph) |
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| Stall speeds at 600kg |
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| Vso (full flap) |
40 kts (46 mph) |
| Vs1 (clean) |
45 kts (52 mph) |
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| Climb Rate (at sea level) 600kg |
1200 ft/min |
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| Service Ceiling |
15,000 ft |
| Empty Weight * |
360 kg (792 lbs) |
| Gross Weight |
600 kg (1320 lbs) |
| Useable Load |
240 kg (528 lbs) |
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| Structural Loading Flight |
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| Load Factor |
+ 3.8 – 1.9 G |
Applied Loads 54degC (129.2degF) |
+6.8G -3.4G |
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| Fuel Capacity (Usable) |
135 lts 35.6 (USgal) |
| Range (Nil Reserve) |
800 nm |
| Endurance (Nil Reserve) |
6.7 hrs |
| Fuel Consumption at Cruise |
23-25 lts/hr |
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| Glide Ratio |
12:1 |
| Crosswind Component |
14 kts |
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| Take Off Distance at 600kg (Ground-roll) |
150 m (492 ft) |
| Landing Distance at 600kg (Ground-roll) |
180 m (656 ft) |
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| *varies with options |
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© copyright Jabiru Aircraft Pty. Ltd. 2005
Updated:
July 7, 2008