Jabiru Aircraft & Engines

The Jabiru UL-D has been designed to meet the UK Microlight Standard of 268kg max empty weight and 450kg gross weight and the 35 knots (65km/hr)

Features include:

Conventional configuration

Designed to JAR –VLA European Airworthiness Standard

High-winged, strut-braced monoplane with wing flaps, mass balanced elevator and in-flight adjustable trim.

Cruise Speed @ 3050 rpm 100 knots

Range (nil reserve) - 460 nautical miles

4 stroke JABIRU 2200 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 with flaps at Gross Weight 35 KIAS

Fully enclosed, ergonomically designed cabin with 2 doors providing ease of entry and low noise levels.

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.

Comfortable seating with easily removed 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 UL-D Specifications

Aircraft Type

Jabiru UL-D

Engine

Jabiru 2200cc

80 hp

4 cylinder, 4 stroke

Propeller

2 Blade Fixed Pitch

Wooden/Composite

60” dia x 42” pitch

Height

2013 mm

Length

5530 mm

Width Tailplane

2350 mm

Cabin Width

Hip

965 mm

Elbow

1040 mm

Shoulder

1067 mm

Wing Span

9398 mm

Wing Chord

990.6mm (39”)

Wing Area

9.35 sq.m (100 sq.ft)

Wing Loading

Gross

12.16 lbs/sq.ft

Aspect Ratio

8.10

Speeds

Vne (never exceed)

120 kts

Va (Max.Manoeuvre)

100 kts

Cruise at 75% power

100 kts

Max. Straight & Level

120 kts

Stall Speeds at Gross Weight

Vs (full flap)

35 kts

Vso(clean)

41 kts

Climb rate (at sea level) Gross

600 ft/min

Service Ceiling

15,000 ft

Structural Loading

Flight Load Factor

+3.8 to -1.9G

Structure Tested

+8.55 to -3.4G

Take Off Distance Groundroll

200 m (650 ft)

Landing Distance Groundroll

168 m (546 ft)

Glide Ratio (engine idle)

12:1

Crosswind Component

14 mph (14 kts)

Fuel System

Fuel Consumption at Cruise

15 lts/hr

Range

460 nm

Endurance (nil reserve)

4.6 hrs

Empty Weight

260 kg (572 lbs)

Useable Load

190 kg (418 lbs)

Gross Weight (MTOW)

450 kg (990 lbs )

Download inclusions and options and order form for the Jabiru UL-D Standard Package (229KB)

Disclaimer

All specifications are quoted for a standard aeroplane with wheel spats and one standard occupant (unless stated).The product specifications and details are generally descriptive of the product shown and were correct at the time of printing. In accordance with our policy of continued product improvement, we reserve the right to vary the specifications and details at any time.

Updated: June 18, 2008