Jabiru SP

The Jabiru aircraft is powered by a Jabiru 4 cylinder 4 stroke 2200 cc  air cooled engine. This Australian designed engine has been developed specifically for use in the Jabiru aircraft and is fitted with dual electronic ignition. The aircraft can be supplied as a complete kit.

The Australian Regulations were amended in early 1989 to permit this class of aircraft to be certified. Aircraft in this Category are fully Type Certified by the Civil Aviation Safety Authority (CASA), and are fitted with approved engines and Type Certified Propellers. All design and flight testing is supervised and approved by CASA specialists.

The Jabiru is ideally suited to the following roles:

  • Flying Training
  • Business Commuting
  • Rural Property Management
  • Recreational Flying & Aero Club Operations
specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
Jabiru 2200cc 80hp
2 Blade Fixed Pitch 60" dia. x 42" pitch
186"
67"
264"
85 sq.ft
2
517 lbs
517 lbs
1034 lbs
14.3 gals
500nm

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling
650ft
1000 ft/min.
110kts
105kts
546ft
5,000ft

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed
90kts
132kts
40kts
x

All specifications are based on manufacturer's calculations