Jaberu J160

The Jabiru J160 C is a factory built certified aircraft.

The Jabiru J160-C aircraft has been developed as a new trainer aircraft that is bigger all round. It has a wider cockpit higher cabin and more leg room. Jabiru has an Australian Type Certificate in the primary category for the J160 as well as a production certificate.

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) -   1030 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            45 KIAS

Cessna 150 (2 available)

The C150 is the most popular light two seater trainer aircraft in the world! It has nice, light controls inviting a new enthusiasm to proficiency maneuvers. Steep turns can be made without heaving at the controls. You can go right up to 60 degrees and hold altitude and bank angle perfectly with mere flexing of the wrist. Practicing stalls keep you on your toes. None of the docile mushing exhibited by the Pipers - you actually have to use the rudder pedals to keep the wings level, and the nose drops down in quite an exciting fashion! Zoom climbs and gentle pushovers have you soaring like an eagle by just subtle wrist flexes with your left hand and a gentle push of the throttle. All the 60 degree banked turns that have been practiced make demonstrating the 45 degree ones most instructors ask for trivial. The stalls make you razor sharp on stall recognition and recovery, especially on aircraft with a bigger aerodynamic warning of the stall. The 150 really rewards you if you use nice, gentle and smooth control movements.

     

C150 Specifications

Gross Weight...................................................1600 lbs
Top Speed.......................................................122 m.p.h.
Cruise, 75% Power at 7000 ft........................117 m.p.h.

RANGE:
Cruise, 75% power at 7000ft...........................475 mi
22.5 Gallons, No Reserve................................4.1 hr.

RATE OF CLIMB AT SEA LEVEL..................670 fpm
SERVICE CEILING...........................................12,650 ft

TAKE-OFF:
Ground run..........................................................735 ft
Total Distance Over 50-ft Obstacle ................1,385 ft

LANDING:
Landing Roll........................................................445 ft

EMPTY WEIGHT: (APPROX)..........................1,060 lbs
BAGGAGE: .......................................................120 lbs
WING LOADING: LBS/SQ FT .........................10.2
POWER LOADING lbs/HP...............................16.0
FUEL CAPACITY ..............................................26 gal
OIL CAPACITY...................................................6 qt
PROPELLER: Fixed Pitch (Diameter)............69 in
ENGINE: Continental ........................................O-200-A
100 rated HP at 2750 rpm

Cessna 172

Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production. As of 2008, more than 43,000 had been built. Capable of cruise speeds of up to 110 kts, the four seat C172 has a well earned reputation as both an excellent training aircraft and tourer.

       

General Information Engine Type: Piston - normally aspirated Production: 1973 to 1976 Engine Make: Lycoming O-320-E2D Notes: 1976 model is 3 Knots faster Engine Power: 150     Engine TBO: 2000       Speeds KTS Max Cruising Speed: 122 Recommended Cruise: 115 Stall Speed: 44 Fuel Capacity Litres Standard Fuel: 159 Long Range Fuel: 197 Range NM Range at Std. Cruise: 435 Ceilings Feet Service Ceiling: 13100   Weights Pounds Kilograms Maximum Takeoff Weight: 2300 1043 Standard Empty Weight: 1335 606 Maximum Useful Load: 965 438 Maximum Useful Load with Full Fuel: 713 323 Climb Performance Feet per Minute Maximum Rate of Climb at Sea Level: 645 Takeoff & Landing Distance at Sea Level Feet Metres Takeoff Ground Roll, Gross Weight: 865 264 Takeoff over 50' Obstacle, Gross Weight: 1525 465 Landing Ground Roll, Gross Weight: 520 159 Landing over 50' Obstacle, Gross Weight: 1250 381 Aircraft Dimensions Feet Metres Overall Length: 26.92 8.21 Tail Height: 8.83 2.69 Wingspan: 35.83