'Short span; short fuselage' version: span 8.03 m (26 ft 4 in), length 5.03 m (16 ft 6 in), wing area 7.90 m2 (85.0 sq ft). 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. Valid XHTML and CSS. The longer fuselage and the standard SK wing. Endurance: 4.5 hr.
Jabiru Performance Measurements & Specifictions Performance Measurements Jabiru 230‐D Jabiru J170 Maximum Speed 130 knots 115 knots Cruise Speed Vh 120 knots 100 knots Vne 138 knots 132 knots Stall (Full Flap) 39 knots 38 knots Stall Clean 45 knots … On the 3300 theres plenty of ground adjustable 2 and 3 blade working well. Speed max: 138 mph. Wing section NASA 4412; drooped wingtips; dihedral 1° 15'; incidence 2° 30'; no twist. 150 plus sold by end 2001. LANDING GEAR : Non-retractable tricycle type, with 15° steerable nosewheel coupled to rudder. Jabiru SK.
Unswept wing (braced) and tailplane, swept fin; dorsal and ventral fins; all flying surfaces square-tipped; wings detachable for storage and transportation. Jabiru SK: Quick-build kit version of ST (components are manufactured alongside production aircraft); first was 66th production Jabiru; quoted home-build time is 600 hours. Jabiru SP480: Proposed version of SP for JAR-VLA certification, with maximum take-off weight of 480 kg (1,058 lb); under development in late 1999.
Ultralight or certified aircraft, suitable for factory or amateur assembly. 54 0 obj
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J_�H��J������2��eT��8
Ui��J�Cc= Fuel capacity 70 litres (18.5 US gallons; 15.4 Imp gallons). Landing gear: nose wheel.SK60 Engine: Jabiru 1.6lt, 60 hp.
Data below refer to Jabiru Calypso with Jabiru 2200 engine. Donc, pour répondre à la question de Kawa, ce que j'ai modifié de mon Jabiru 2200, dans le but d'agir sur la fiabilité, (l'avenir nous dira ds quel sens !) 0
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HP range: 60-80. Specs, range, speed, operating weights and performance for the Jabiru J170 here We use cookies to help you get the best experience when using our website. Cruise: 90-95 kts @ 14 lt/hr. In-flight adjustable pitch trim; wide-span slotted flaps.
Range: 600 sm. CUSTOMERS : Production of complete and kit aircraft totalled some 535 by December 2002. Enlarged rudder; mainwheel legs moved forward; steerable tailwheel and differential braking. Stall: 46 mph.
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Jabiru SP4: Kit, combining longer fuselage of UL 450 with Jabiru 2200 engine and short-span wings of SK; originally designated SP. Jabiru's version is fibreglass not Carbon so more flex and damping. Nosewheel 2.60-4, 4.00-4 or 5.00-6; tailwheel 250x50. //-->. STRUCTURE : All-GFRP except metal wing struts, nosewheel assembly and engine mount.
MTOW 500kg (1,102 lb). Also known as Jabiru SP3300. c```���01G��830�2�3�(��!��@!��J�a�yl�l� ���X2m�}?�`p�;`jx�f$����m`�C�!|F� =$
Total of 54 built with 1600 engine between April 1993 and March 1996. �UV��,+���HY�Er�G�2k��K/���'J�5 H\a��F8�D�1��L�7p2����ST��i��A��z+�֞�Z;~. Thanks for contributing, sharing and contacting us. Since I could not find any positive long term reports, I posted in the Jabiru forum if anybody ever made to to TBO without significant repairs other than the scheduled maintenance, … Instrumentation: Basic VFR; vacuum instruments optional. ���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 +�/�/!S���o1�C��A�i��� _���� Engine: Jabiru 2200. We have composite spinners available for these propellers in 8″, 9″, 9.5″ 10″ 11″ and 12″ diameters. �m�^�f���� !=jn
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. CURRENT VERSIONS : Jabiru LSA: Light Sport Aircraft; factory-built; registered under AUF (Australian Ultralight Federation) rules (Pt 101.55). endstream
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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. Stall speed 39 kts.SP taildragger Wing: UL. Flyaway Calypso 2200 US$59,995 (April 2002). Not many prop options for 2200, none other than Jabiru's is approved and they are pinned to a set pitch . Jabiru SP6: Company designation of SP4 kit with 89.5 kW (120 hp) Jabiru 3300 engine. Prototype built by Peter Kayne of Narrogin, Western Australia. bfRegisterSummarize("ff_elem13", "", "", "not available", false) Cruise: 75 % 90 kt. Original short rudder supplanted by full-height rudder (also available as retrofit) on all versions. Engine: Jabiru 2200.
PROGRAMME : Design of original Jabiru LSA, started 1987; prototype (first of two, VH-JCX and VH-JQX) made first flight August 1989; first customer delivery April 1991; factory-built version certified to CAO 101 Pt 55 on 1 October 1991; 20 built with KFM engine before change to 44.7 kW (60 hp) Jabiru 1600 flat-four, many of these subsequently re-engined; kitplane construction certification achieved in Australia, New Zealand, South Korea, UK and USA by early 1997; marketed in US as amateur-built kit, achieving FAR Pt 21.191 (g) certification on 8 February 1996 (as well as Australian CAO 19 equivalent); marketing office opened at Aiken, South Carolina, in anticipation of substantial US sales of at least 100 per year but later closed in favour of network of dealerships. From 2002, enlarged fin version (3/4 height rudder) adopted, entire vertical tail being moved further forward. Jabiru Engine: Jabiru, 80 hp.
Seats: 2SK80 Engine: Jabiru 2.2lt, 80 hp. Lots of unhappy stories of non wooden props on 4 cyl Jabiru.
By continuing to use this website, you are agreeing to our Cookie Policy. endstream
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Fuel capacity 65 litres (17.2 US gallons; 14.3 Imp gallons). Cantilever selfsprung GFRP mainwheel legs; rubber block nosewheel shock-absorption; wheel fairings standard over 4.00-6 or 5.00-6 tyres; Bigfoot 6.00-6 tyres optional. Jabiru SP-T: Tailwheel version of SP. h�bbd```b``� "�@$�f�Z����50yL��`RL~�\-`sBA��0[D:$�M���`��@�Ѿ!n�
���Me`�m&X�������� � f
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. Cruising speed 117 kt (217 km/h; 135 mph).
Gross: 1060 lbs. Joint venture announced in 1998 with CDE Aviation Company of Sri Lanka, subsidiary of Lionair, to establish Jabiru Asia for manufacture of Jabiru ST3 for Asian markets, especially India. h�b``g`` Launched in UK in 2000 and meeting 35 kt (65 km/h; 41 mph) stalling speed requirement. It has currently not been vibration analyzed for use on any other direct drive engine. Cruise: 129 mph. Cruise: 75% 105 kt. FLYING CONTROLS : Conventional and manual. Endurance: 4 hr. POWER PLANT : One 59.7 kW (80 hp) Jabiru 2200A/J flat-four engine, driving a two-blade, fixed-pitch, wood/composites propeller.
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. SP 470 Engine: 2.2 Jabiru.
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All Rights Reserved. Landing dist: 300 ft. Service ceiling: 15,000 ft. Seats: 2. Length: 16.5 ft. Wing span: 26.25 ft. Wing area: 85 sq.ft. By 1998 sales were underway in the UK and worldwide 130 ezamples were flying. Our 2 Blade Jabiru 2200 propeller is suitable for use on the Jabiru J2200 engine.
: changé l'arbre à cames et les poussoirs pour ceux montés sur les derniers moteurs. %%EOF
Height: 6.58 ft.
DESIGN FEATURES : Designed to Australian AUFPt 101.55 and British BCAR Section S. with reference to FAR Pt 21 and JAR-VLA. COSTS: Calypso- US$20,900: SP US$19,900 (2003) both minus engine. ^ JR���������V��(�c�=�Ǐg�!�HK����7�Șa�bDو(N����F�) gB��F�a� )Cx$%� �����ьk$ќׂHfђH������Y^$�t��4h#ߚM�幺N��넣�a��/*�8� }�hchJ4+4Z��M���RwE>N\5�w�.��j�li�ݾJK7�͠���yG����A�p��ֿ�-a������m-��2�7�0�U�ݢ"V3��u@��v��q����2F;.6Hvg�$�o��*64�IC2p�� Ŗ��`7�g��E;�eEv���D(�;����~�տ����l\峉L��U�G�ϋy:�]��,V�*��ә#�&������,�]d�*/�? Unless you have a 19 reg you cant fit or adjust them without Jabiru approval. ST3 UL Stall: 35 kt / 40 mph / 65 kmh Cruise: 85 kt / 98 mph / 157 kmh VNE: 116 kt / 133 mph / 215 kmh Empty Weight: 253 kg / 558 lbs MTOW Weight: 450 kg / 992 lbs Climb Ratio: 1000 ft/min / 5 m/s Glide Ratio: 1:14 Take-off distance (50ft obstacle): 1180 ft / 360 m Landing distance (50ft obstacle): 1180 ft / 360 m . 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. Seats: 2. Jabiru Calypso: Initially factory-built; now available only as kit; previously known as UL 450 ; SLA (Small Light Aeroplane to UK's now-replaced BCAR Section S), first aircraft was built in Ireland in 1998. Fuel cap: 17 USG.
'Short span; short fuselage' version: span 8.03 m (26 ft 4 in), length 5.03 m (16 ft 6 in), wing area 7.90 m2 (85.0 sq ft). 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. Valid XHTML and CSS. The longer fuselage and the standard SK wing. Endurance: 4.5 hr.
Jabiru Performance Measurements & Specifictions Performance Measurements Jabiru 230‐D Jabiru J170 Maximum Speed 130 knots 115 knots Cruise Speed Vh 120 knots 100 knots Vne 138 knots 132 knots Stall (Full Flap) 39 knots 38 knots Stall Clean 45 knots … On the 3300 theres plenty of ground adjustable 2 and 3 blade working well. Speed max: 138 mph. Wing section NASA 4412; drooped wingtips; dihedral 1° 15'; incidence 2° 30'; no twist. 150 plus sold by end 2001. LANDING GEAR : Non-retractable tricycle type, with 15° steerable nosewheel coupled to rudder. Jabiru SK.
Unswept wing (braced) and tailplane, swept fin; dorsal and ventral fins; all flying surfaces square-tipped; wings detachable for storage and transportation. Jabiru SK: Quick-build kit version of ST (components are manufactured alongside production aircraft); first was 66th production Jabiru; quoted home-build time is 600 hours. Jabiru SP480: Proposed version of SP for JAR-VLA certification, with maximum take-off weight of 480 kg (1,058 lb); under development in late 1999.
Ultralight or certified aircraft, suitable for factory or amateur assembly. 54 0 obj
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J_�H��J������2��eT��8
Ui��J�Cc= Fuel capacity 70 litres (18.5 US gallons; 15.4 Imp gallons). Landing gear: nose wheel.SK60 Engine: Jabiru 1.6lt, 60 hp.
Data below refer to Jabiru Calypso with Jabiru 2200 engine. Donc, pour répondre à la question de Kawa, ce que j'ai modifié de mon Jabiru 2200, dans le but d'agir sur la fiabilité, (l'avenir nous dira ds quel sens !) 0
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HP range: 60-80. Specs, range, speed, operating weights and performance for the Jabiru J170 here We use cookies to help you get the best experience when using our website. Cruise: 90-95 kts @ 14 lt/hr. In-flight adjustable pitch trim; wide-span slotted flaps.
Range: 600 sm. CUSTOMERS : Production of complete and kit aircraft totalled some 535 by December 2002. Enlarged rudder; mainwheel legs moved forward; steerable tailwheel and differential braking. Stall: 46 mph.
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Jabiru SP4: Kit, combining longer fuselage of UL 450 with Jabiru 2200 engine and short-span wings of SK; originally designated SP. Jabiru's version is fibreglass not Carbon so more flex and damping. Nosewheel 2.60-4, 4.00-4 or 5.00-6; tailwheel 250x50. //-->. STRUCTURE : All-GFRP except metal wing struts, nosewheel assembly and engine mount.
MTOW 500kg (1,102 lb). Also known as Jabiru SP3300. c```���01G��830�2�3�(��!��@!��J�a�yl�l� ���X2m�}?�`p�;`jx�f$����m`�C�!|F� =$
Total of 54 built with 1600 engine between April 1993 and March 1996. �UV��,+���HY�Er�G�2k��K/���'J�5 H\a��F8�D�1��L�7p2����ST��i��A��z+�֞�Z;~. Thanks for contributing, sharing and contacting us. Since I could not find any positive long term reports, I posted in the Jabiru forum if anybody ever made to to TBO without significant repairs other than the scheduled maintenance, … Instrumentation: Basic VFR; vacuum instruments optional. ���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 +�/�/!S���o1�C��A�i��� _���� Engine: Jabiru 2200. We have composite spinners available for these propellers in 8″, 9″, 9.5″ 10″ 11″ and 12″ diameters. �m�^�f���� !=jn
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. CURRENT VERSIONS : Jabiru LSA: Light Sport Aircraft; factory-built; registered under AUF (Australian Ultralight Federation) rules (Pt 101.55). endstream
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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. Stall speed 39 kts.SP taildragger Wing: UL. Flyaway Calypso 2200 US$59,995 (April 2002). Not many prop options for 2200, none other than Jabiru's is approved and they are pinned to a set pitch . Jabiru SP6: Company designation of SP4 kit with 89.5 kW (120 hp) Jabiru 3300 engine. Prototype built by Peter Kayne of Narrogin, Western Australia. bfRegisterSummarize("ff_elem13", "", "", "not available", false) Cruise: 75 % 90 kt. Original short rudder supplanted by full-height rudder (also available as retrofit) on all versions. Engine: Jabiru 2200.
PROGRAMME : Design of original Jabiru LSA, started 1987; prototype (first of two, VH-JCX and VH-JQX) made first flight August 1989; first customer delivery April 1991; factory-built version certified to CAO 101 Pt 55 on 1 October 1991; 20 built with KFM engine before change to 44.7 kW (60 hp) Jabiru 1600 flat-four, many of these subsequently re-engined; kitplane construction certification achieved in Australia, New Zealand, South Korea, UK and USA by early 1997; marketed in US as amateur-built kit, achieving FAR Pt 21.191 (g) certification on 8 February 1996 (as well as Australian CAO 19 equivalent); marketing office opened at Aiken, South Carolina, in anticipation of substantial US sales of at least 100 per year but later closed in favour of network of dealerships. From 2002, enlarged fin version (3/4 height rudder) adopted, entire vertical tail being moved further forward. Jabiru Engine: Jabiru, 80 hp.
Seats: 2SK80 Engine: Jabiru 2.2lt, 80 hp. Lots of unhappy stories of non wooden props on 4 cyl Jabiru.
By continuing to use this website, you are agreeing to our Cookie Policy. endstream
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Fuel capacity 65 litres (17.2 US gallons; 14.3 Imp gallons). Cantilever selfsprung GFRP mainwheel legs; rubber block nosewheel shock-absorption; wheel fairings standard over 4.00-6 or 5.00-6 tyres; Bigfoot 6.00-6 tyres optional. Jabiru SP-T: Tailwheel version of SP. h�bbd```b``� "�@$�f�Z����50yL��`RL~�\-`sBA��0[D:$�M���`��@�Ѿ!n�
���Me`�m&X�������� � f
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. Cruising speed 117 kt (217 km/h; 135 mph).
Gross: 1060 lbs. Joint venture announced in 1998 with CDE Aviation Company of Sri Lanka, subsidiary of Lionair, to establish Jabiru Asia for manufacture of Jabiru ST3 for Asian markets, especially India. h�b``g`` Launched in UK in 2000 and meeting 35 kt (65 km/h; 41 mph) stalling speed requirement. It has currently not been vibration analyzed for use on any other direct drive engine. Cruise: 129 mph. Cruise: 75% 105 kt. FLYING CONTROLS : Conventional and manual. Endurance: 4 hr. POWER PLANT : One 59.7 kW (80 hp) Jabiru 2200A/J flat-four engine, driving a two-blade, fixed-pitch, wood/composites propeller.
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. SP 470 Engine: 2.2 Jabiru.
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All Rights Reserved. Landing dist: 300 ft. Service ceiling: 15,000 ft. Seats: 2. Length: 16.5 ft. Wing span: 26.25 ft. Wing area: 85 sq.ft. By 1998 sales were underway in the UK and worldwide 130 ezamples were flying. Our 2 Blade Jabiru 2200 propeller is suitable for use on the Jabiru J2200 engine.
: changé l'arbre à cames et les poussoirs pour ceux montés sur les derniers moteurs. %%EOF
Height: 6.58 ft.
DESIGN FEATURES : Designed to Australian AUFPt 101.55 and British BCAR Section S. with reference to FAR Pt 21 and JAR-VLA. COSTS: Calypso- US$20,900: SP US$19,900 (2003) both minus engine. ^ JR���������V��(�c�=�Ǐg�!�HK����7�Șa�bDو(N����F�) gB��F�a� )Cx$%� �����ьk$ќׂHfђH������Y^$�t��4h#ߚM�幺N��넣�a��/*�8� }�hchJ4+4Z��M���RwE>N\5�w�.��j�li�ݾJK7�͠���yG����A�p��ֿ�-a������m-��2�7�0�U�ݢ"V3��u@��v��q����2F;.6Hvg�$�o��*64�IC2p�� Ŗ��`7�g��E;�eEv���D(�;����~�տ����l\峉L��U�G�ϋy:�]��,V�*��ә#�&������,�]d�*/�? Unless you have a 19 reg you cant fit or adjust them without Jabiru approval. ST3 UL Stall: 35 kt / 40 mph / 65 kmh Cruise: 85 kt / 98 mph / 157 kmh VNE: 116 kt / 133 mph / 215 kmh Empty Weight: 253 kg / 558 lbs MTOW Weight: 450 kg / 992 lbs Climb Ratio: 1000 ft/min / 5 m/s Glide Ratio: 1:14 Take-off distance (50ft obstacle): 1180 ft / 360 m Landing distance (50ft obstacle): 1180 ft / 360 m . Jabiru ST : Certified version; in factory production from mid-1994; first was 50th production Jabiru in mid-1998, the 17th production ST was registered VH-JRU to Jabiru Aircraft as the first ST3 short span and fuselage. Seats: 2. Jabiru Calypso: Initially factory-built; now available only as kit; previously known as UL 450 ; SLA (Small Light Aeroplane to UK's now-replaced BCAR Section S), first aircraft was built in Ireland in 1998. Fuel cap: 17 USG.
. STRUCTURE : All-GFRP except metal wing struts, nosewheel assembly and engine mount.
MTOW 500kg (1,102 lb). Also known as Jabiru SP3300. c```���01G��830�2�3�(��!��@!��J�a�yl�l� ���X2m�}?�`p�;`jx�f$����m`�C�!|F� =$
Total of 54 built with 1600 engine between April 1993 and March 1996. �UV��,+���HY�Er�G�2k��K/���'J�5 H\a��F8�D�1��L�7p2����ST��i��A��z+�֞�Z;~. Thanks for contributing, sharing and contacting us. Since I could not find any positive long term reports, I posted in the Jabiru forum if anybody ever made to to TBO without significant repairs other than the scheduled maintenance, … Instrumentation: Basic VFR; vacuum instruments optional. ���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 +�/�/!S���o1�C��A�i��� _���� Engine: Jabiru 2200. We have composite spinners available for these propellers in 8″, 9″, 9.5″ 10″ 11″ and 12″ diameters. �m�^�f���� !=jn
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. CURRENT VERSIONS : Jabiru LSA: Light Sport Aircraft; factory-built; registered under AUF (Australian Ultralight Federation) rules (Pt 101.55). endstream
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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. Stall speed 39 kts.SP taildragger Wing: UL. Flyaway Calypso 2200 US$59,995 (April 2002). Not many prop options for 2200, none other than Jabiru's is approved and they are pinned to a set pitch . Jabiru SP6: Company designation of SP4 kit with 89.5 kW (120 hp) Jabiru 3300 engine. Prototype built by Peter Kayne of Narrogin, Western Australia. bfRegisterSummarize("ff_elem13", "", "", "not available", false) Cruise: 75 % 90 kt. Original short rudder supplanted by full-height rudder (also available as retrofit) on all versions. Engine: Jabiru 2200.
PROGRAMME : Design of original Jabiru LSA, started 1987; prototype (first of two, VH-JCX and VH-JQX) made first flight August 1989; first customer delivery April 1991; factory-built version certified to CAO 101 Pt 55 on 1 October 1991; 20 built with KFM engine before change to 44.7 kW (60 hp) Jabiru 1600 flat-four, many of these subsequently re-engined; kitplane construction certification achieved in Australia, New Zealand, South Korea, UK and USA by early 1997; marketed in US as amateur-built kit, achieving FAR Pt 21.191 (g) certification on 8 February 1996 (as well as Australian CAO 19 equivalent); marketing office opened at Aiken, South Carolina, in anticipation of substantial US sales of at least 100 per year but later closed in favour of network of dealerships. From 2002, enlarged fin version (3/4 height rudder) adopted, entire vertical tail being moved further forward. Jabiru Engine: Jabiru, 80 hp.
Seats: 2SK80 Engine: Jabiru 2.2lt, 80 hp. Lots of unhappy stories of non wooden props on 4 cyl Jabiru.
By continuing to use this website, you are agreeing to our Cookie Policy. endstream
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Fuel capacity 65 litres (17.2 US gallons; 14.3 Imp gallons). Cantilever selfsprung GFRP mainwheel legs; rubber block nosewheel shock-absorption; wheel fairings standard over 4.00-6 or 5.00-6 tyres; Bigfoot 6.00-6 tyres optional. Jabiru SP-T: Tailwheel version of SP. h�bbd```b``� "�@$�f�Z����50yL��`RL~�\-`sBA��0[D:$�M���`��@�Ѿ!n�
���Me`�m&X�������� � f
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. Cruising speed 117 kt (217 km/h; 135 mph).
Gross: 1060 lbs. Joint venture announced in 1998 with CDE Aviation Company of Sri Lanka, subsidiary of Lionair, to establish Jabiru Asia for manufacture of Jabiru ST3 for Asian markets, especially India. h�b``g`` Launched in UK in 2000 and meeting 35 kt (65 km/h; 41 mph) stalling speed requirement. It has currently not been vibration analyzed for use on any other direct drive engine. Cruise: 129 mph. Cruise: 75% 105 kt. FLYING CONTROLS : Conventional and manual. Endurance: 4 hr. POWER PLANT : One 59.7 kW (80 hp) Jabiru 2200A/J flat-four engine, driving a two-blade, fixed-pitch, wood/composites propeller.
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. SP 470 Engine: 2.2 Jabiru.
Powered by Joomla!.
All Rights Reserved. Landing dist: 300 ft. Service ceiling: 15,000 ft. Seats: 2. Length: 16.5 ft. Wing span: 26.25 ft. Wing area: 85 sq.ft. By 1998 sales were underway in the UK and worldwide 130 ezamples were flying. Our 2 Blade Jabiru 2200 propeller is suitable for use on the Jabiru J2200 engine.
: changé l'arbre à cames et les poussoirs pour ceux montés sur les derniers moteurs. %%EOF
Height: 6.58 ft.
DESIGN FEATURES : Designed to Australian AUFPt 101.55 and British BCAR Section S. with reference to FAR Pt 21 and JAR-VLA. COSTS: Calypso- US$20,900: SP US$19,900 (2003) both minus engine. ^ JR���������V��(�c�=�Ǐg�!�HK����7�Șa�bDو(N����F�) gB��F�a� )Cx$%� �����ьk$ќׂHfђH������Y^$�t��4h#ߚM�幺N��넣�a��/*�8� }�hchJ4+4Z��M���RwE>N\5�w�.��j�li�ݾJK7�͠���yG����A�p��ֿ�-a������m-��2�7�0�U�ݢ"V3��u@��v��q����2F;.6Hvg�$�o��*64�IC2p�� Ŗ��`7�g��E;�eEv���D(�;����~�տ����l\峉L��U�G�ϋy:�]��,V�*��ә#�&������,�]d�*/�? Unless you have a 19 reg you cant fit or adjust them without Jabiru approval. ST3 UL Stall: 35 kt / 40 mph / 65 kmh Cruise: 85 kt / 98 mph / 157 kmh VNE: 116 kt / 133 mph / 215 kmh Empty Weight: 253 kg / 558 lbs MTOW Weight: 450 kg / 992 lbs Climb Ratio: 1000 ft/min / 5 m/s Glide Ratio: 1:14 Take-off distance (50ft obstacle): 1180 ft / 360 m Landing distance (50ft obstacle): 1180 ft / 360 m . 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. Seats: 2. Jabiru Calypso: Initially factory-built; now available only as kit; previously known as UL 450 ; SLA (Small Light Aeroplane to UK's now-replaced BCAR Section S), first aircraft was built in Ireland in 1998. Fuel cap: 17 USG.
