Wing section NASA 4412; drooped wingtips; dihedral 1° 15'; incidence 2° 30'; no twist. DESIGN FEATURES : Designed to Australian AUFPt 101.55 and British BCAR Section S. with reference to FAR Pt 21 and JAR-VLA. 10 0 obj <> endobj Jabiru SP4: Kit, combining longer fuselage of UL 450 with Jabiru 2200 engine and short-span wings of SK; originally designated SP. In-flight adjustable pitch trim; wide-span slotted flaps. We have composite spinners available for these propellers in 8″, 9″, 9.5″ 10″ 11″ and 12″ diameters. H��TKk�@��W�؇�gfwgw!�Ц�Bt9��\�S����w�j���T������hV�k1Em���l@�R�V�l�����:B4-��(NA ̶͡��Β��~���{���n�1u�%��Ձ;E}�v� x�~E��PF��G�~��Ԥ�= -H���jܛ��������$����jhռ�V}�I�P. +�/�/!S���o1�C��A�i��� _���� Stall: 46 mph. CUSTOMERS : Production of complete and kit aircraft totalled some 535 by December 2002. Speed max: 138 mph. AVIONICS : Comms: VHF antenna (inside fin) and intercom standard. endstream endobj 14 0 obj <>stream

LANDING GEAR : Non-retractable tricycle type, with 15° steerable nosewheel coupled to rudder. ROC: 1200 fpm. Gross: 1060 lbs. Also available with tailwheel as Calypso T. Meets FAA LSA. J_�H��J������2��eT��8 Ui��J�Cc= Fuel cap: 17 USG. The 2200 in my J160 has just had to be written off due to a sequence of failures which appear to relate to an accident prior to me taking ownership.

Jabiru SP-T: Tailwheel version of SP. Fuel capacity 70 litres (18.5 US gallons; 15.4 Imp gallons). h��Wmo�8�+������N����n�U�z�C By 1998 sales were underway in the UK and worldwide 130 ezamples were flying. Copyright © 2020 all-aero. ���cd3��h8�����e��u�X˿�@���� z��>3�(zD z�n�v2ꕫ,b�`e��'sL�A���}b�g�:R~l��fh�dý�_���S��a���~w(�9�&��Z@A�9�>����U`���4����C�9��}�#��P1FP%�x Landing dist: 300 ft. Service ceiling: 15,000 ft. Seats: 2. Unless you have a 19 reg you cant fit or adjust them without Jabiru approval. Fuel capacity 65 litres (17.2 US gallons; 14.3 Imp gallons).
Jabiru SK. On the 3300 theres plenty of ground adjustable 2 and 3 blade working well. Jabiru factory at Koggala, in southern Sri Lanka; intended to have production capacity for 40 aircraft per year, using engines and avionics imported from Australia, and airframes manufactured locally. Differences from SK include wing span increased by 1.37 m (4 ft 6 in); fuselage by 0.61 m (2 ft 0 in); flaps by total of 1.83 m (6 ft 0 in); and reduced ventral fin.

We really wanted a used Kitfox that already had a Jabiru 2200 installed. Total of 54 built with 1600 engine between April 1993 and March 1996. MTOW 470 kg (1,036 lb); stalling speed 39 kt (73 km/h; 45 mph); optimised for Canadian, Chilean and South African markets, among others. PROGRAMME : Design of original Jabiru LSA, started 1987; prototype (first of two, VH-JCX and VH-JQX) made first flight August 1989; first customer delivery April 1991; factory-built version certified to CAO 101 Pt 55 on 1 October 1991; 20 built with KFM engine before change to 44.7 kW (60 hp) Jabiru 1600 flat-four, many of these subsequently re-engined; kitplane construction certification achieved in Australia, New Zealand, South Korea, UK and USA by early 1997; marketed in US as amateur-built kit, achieving FAR Pt 21.191 (g) certification on 8 February 1996 (as well as Australian CAO 19 equivalent); marketing office opened at Aiken, South Carolina, in anticipation of substantial US sales of at least 100 per year but later closed in favour of network of dealerships. )��"1��qQ�fI��H�{)6d������P�'p�:�({Giȭv�� Data below refer to Jabiru Calypso with Jabiru 2200 engine. 54 0 obj <>stream SYSTEMS : 12 V DC electrical system with 100 W capacity 20 Ah battery. Jabiru SP4: Kit, combining longer fuselage of UL 450 with Jabiru 2200 engine and short-span wings of SK; originally designated SP. Cruising speed 117 kt (217 km/h; 135 mph). %PDF-1.5 %���� Thanks for contributing, sharing and contacting us. 150 plus sold by end 2001. STRUCTURE : All-GFRP except metal wing struts, nosewheel assembly and engine mount. Flyaway Calypso 2200 US$59,995 (April 2002). endstream endobj startxref h�b``g`` MTOW 500kg (1,102 lb). From 2002, enlarged fin version (3/4 height rudder) adopted, entire vertical tail being moved further forward. CURRENT VERSIONS : Jabiru LSA: Light Sport Aircraft; factory-built; registered under AUF (Australian Ultralight Federation) rules (Pt 101.55). Unswept wing (braced) and tailplane, swept fin; dorsal and ventral fins; all flying surfaces square-tipped; wings detachable for storage and transportation. More powerful ST version introduced in 1994. Fuel capacity 70 litres (18.5 US gallons; 15.4 Imp gallons).

Cruise: 75 % 90 kt. I have been considering a few engine options, but it looks as though the simplest and most cost effective solution is to go with a replacement Jabiru of the latest specification. Jabiru ST : Certified version; in factory production from mid-1994; first was 50th production Jabiru in mid-1998, the 17th production ST was registered VH-JRU to Jabiru Aircraft as the first ST3 short span and fuselage.


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