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
18’6"
6’7"
26’4"
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
|
