자비루 UL, SP

<P><img src="https://t1.daumcdn.net/cafefile/pds46/16_cafe_2007_09_28_12_41_46fc77f5394ec" class="tx-daum-image" alt="이미지를 클릭하면 원본을 보실 수 있습니다." border="0" /><BR><BR><img src="https://t1.daumcdn.net/cafefile/pds44/9_cafe_2007_09_28_12_24_46fc73d1bfb3d" class="tx-daum-image" alt="이미지를 클릭하면 원본을 보실 수 있습니다." border="0" /><BR><BR><img src="https://t1.daumcdn.net/cafefile/pds44/9_cafe_2007_09_28_12_24_46fc73d8b7823" class="tx-daum-image" alt="이미지를 클릭하면 원본을 보실 수 있습니다." border="0" /><BR><BR></P> <P>자비루는  UL ,SP, J200 ,J400  등의 라인업을 가지고 있습니다만  실제로 등록 가능한것은 </P> <P> </P> <P>UL 과 SP 입니다..  종종  j200 이나 j400 을  운영하는데 이것들은  등록 불가능한  비행기입니다.</P> <P> </P> <P>등록번호가 동체나 날개에 적혀 있는지 보시면 되겠지요..</P> <P> </P> <P>자비루 회사는  호주 에 있고..  자비루 2200 엔진을 만드는 회사입니다.</P> <P> </P> <P>소재는 복합소재이고  고익기입니다.</P> <P> </P> <P>조종간은  중앙 스틱방식입니다.. 대천에 등록된  자비루 비행기가 있다고 해서  올립니다.</P> <P> </P> <P>이 비행기는  세스나에 가까운 구조입니다..  비행감도 그렇겠지요..</P> <P> </P> <P>J200 J400은  자가용 비행기에 해당한다고 봐야 합니다 공항에  계륙해야 하는...</P> <P> </P> <TABLE cellSpacing=0 cellPadding=0 width=379 border=0> <TBODY> <TR> <TD> <TABLE class=text cellSpacing=0 cellPadding=0 width=379 border=0> <TBODY> <TR> <TD vAlign=top background=images/bgnavleftfeature.gif></TD></TR> <TR> <TD></TD></TR></TBODY></TABLE></TD></TR> <TR> <TD> </TD></TR> <TR> <TD> <TABLE cellSpacing=0 cellPadding=0 width=379 border=0> <TBODY> <TR> <TD width=379 background=images/main_11.jpg> <TABLE cellSpacing=0 cellPadding=0 width=276 border=0> <TBODY> <TR> <TD width=8></TD> <TD class=feature width=256></TD></TR></TBODY></TABLE></TD></TR> <TR> <TD vAlign=top background=images/bgnavleftfeature.gif> <TABLE class=text cellSpacing=3 cellPadding=2 width=377 border=0> <TBODY> <TR> <TD class=specheader vAlign=top width=164 background=images/bggeneric.gif></TD> <TD class=text vAlign=top width=196 background=images/bggeneric.gif></TD></TR> <TR> <TD class=specheader vAlign=top background=images/bggeneric.gif></TD> <TD class=text vAlign=top background=images/bggeneric.gif></TD></TR> <TR> <TD class=specheader vAlign=top background=images/bggeneric.gif></TD> <TD class=text vAlign=top background=images/bggeneric.gif></TD></TR> <TR> <TD class=specheader vAlign=top background=images/bggeneric.gif></TD> <TD class=text vAlign=top background=images/bggeneric.gif></TD></TR> <TR> <TD class=specheader vAlign=top background=images/bggeneric.gif></TD> <TD class=text vAlign=top background=images/bggeneric.gif></TD></TR> <TR> <TD class=specheader vAlign=top background=images/bggeneric.gif></TD> <TD class=text vAlign=top background=images/bggeneric.gif></TD></TR> <TR> <TD class=specheader vAlign=top background=images/bggeneric.gif></TD> <TD class=text vAlign=top background=images/bggeneric.gif></TD></TR> <TR> <TD class=specheader vAlign=top background=images/bggeneric.gif></TD> <TD class=text vAlign=top background=images/bggeneric.gif></TD></TR></TBODY></TABLE></TD></TR></TBODY></TABLE></TD></TR></TBODY></TABLE> <H1 align=center>Jabiru UL-D</H1> <H1 align=center><SPAN class=content> <IMG height=170 hspace=10 src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.jabiru.net.au%2Fimages%2FUL-D-flytop.jpg" width=350 align=right vspace=10></SPAN></H1> <P><SPAN class=content>The Jabiru UL-D has been designed to meet the UK Microlight Standard of 268kg max empty weight and 450kg gross weight and the 35 knots (65km/hr) </SPAN>stall speed. </P> <H2>Features include:</H2> <UL> <LI>Conventional configuration <LI> <DIV align=left>Designed to JAR –VLA European Airworthiness Standard </DIV> <LI> <DIV align=left>High-winged, strut-braced monoplane with wing flaps, mass balanced elevator and in-flight adjustable trim.</DIV> <LI><STRONG>Cruise Speed @ 3050 rpm      100 knots </STRONG> <LI><STRONG>Range   (nil reserve) -   460 nautical miles </STRONG> <LI>4 stroke JABIRU 2200 cc engine designed specifically for the Jabiru aircraft. <LI>Gentle and predictable stall characteristics, together with light and responsive controls, make JABIRU a true sport aircraft. <LI> <IMG height=170 hspace=10 src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.jabiru.net.au%2Fimages%2FUL-D-Loop-Mag-UK-NX2I2146.jpg" width=350 align=right vspace=10>Stall speed with flaps at Gross Weight   35 KIAS <LI>Fully enclosed, ergonomically designed cabin with 2 doors providing ease of entry and low noise levels. <LI>Excellent visibility <LI>Side-by side fixed seating with centre controls and panel mounted throttles. Ideal for training or recreation. <LI>Tricycle undercarriage with steerable nosewheel and hand operated in line hydraulic disc brakes makes ground handling a breeze. <LI>Excellent cross wind handling performance – 14 knots <LI>All composite construction removes the corrosion problem. <LI>Wing and power loadings provide high performance and handling, particularly in turbulence. <LI>Comfortable seating with easily removed covers. <LI>Designed for minimum maintenance. Upper and lower cowls easily removed. <LI>Auxiliary electronic fuel pump for ease of starting and added security in flight. <LI>All the engine management features of conventional GA light aircraft: Carburettor Air Heat, Dual Ignition, Pressure Compensating Carburettor – no mixture control ! <LI>Jabiru fixed pitch wooden propeller with composite cover and urethane leading edge <IMG height=219 hspace=10 src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.jabiru.net.au%2FEngines%2F4%2520cylinder%2F4-cyc-fine-fin-Jabiru-Engin.gif" width=258 align=right vspace=10> <LI>Avionics include VHF Transceiver, PM501 Intercom and headsets Transponder Altitude Encoder optional <LI>4 Options for instrument Panels see:<A href="http://www.jabiru.net.au/instrumentsbodyFrame-1.htm"><U><FONT color=#0000ff> </FONT><SPAN class=style10><FONT color=#ff0000>Instrument Panels</FONT></SPAN></U></A> <LI>Tinted Windscreen <LI>Steerable Nose Wheel <LI>Electrically operated flaps <LI>Cast aluminium 500 x 6 wheels and 6 ply tyres with spats <LI>Fully upholstered cockpit <LI>Cabin Heater <LI>Choice of decals and registration numbers (from the standard range) <LI>135 litre fuel tanks (wing tanks & header tanks) <LI>Optional adjustable foot pedals to cater for pilots who have difficulties reaching the pedals <LI>Tool Kit </LI></UL> <H2>Jabiru UL-D Specifications </H2> <TABLE cellSpacing=0 cellPadding=0 border=1> <TBODY> <TR> <TD vAlign=top width=317> <P><STRONG>Aircraft Type</STRONG></P></TD> <TD vAlign=top width=230> <P><STRONG>Jabiru UL-D</STRONG></P></TD> <TD vAlign=top width=338 rowSpan=59> </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Engine</TD> <TD vAlign=top>Jabiru 2200cc</TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top>80 hp </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top>4 cylinder, 4 stroke </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top height=28>Propeller </TD> <TD vAlign=top>2 Blade Fixed Pitch </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top>Wooden/Composite </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top>60” dia   x   42” pitch </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top> <P align=left>Height </P></TD> <TD vAlign=top> <P align=left>2013 mm </P></TD></TR> <TR> <TD vAlign=top> <P align=left>Length </P></TD> <TD vAlign=top> <P align=left>5530 mm </P></TD></TR> <TR> <TD vAlign=top> <P align=left>Width Tailplane </P></TD> <TD vAlign=top> <P align=left>2350 mm </P></TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Cabin Width</TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Hip </TD> <TD vAlign=top>965 mm </TD></TR> <TR> <TD vAlign=top>Elbow </TD> <TD vAlign=top>1040 mm </TD></TR> <TR> <TD vAlign=top>Shoulder</TD> <TD vAlign=top>1067 mm </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Wing Span </TD> <TD vAlign=top>9398 mm</TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top> <P align=left>Wing Chord </P></TD> <TD vAlign=top> <P align=left>990.6mm (39”)</P></TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top> <P align=left>Wing Area </P></TD> <TD vAlign=top> <P align=left>9.35 sq.m (100 sq.ft) </P></TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Wing Loading </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Gross </TD> <TD vAlign=top>12.16 lbs/sq.ft </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top> <P align=left>Aspect Ratio </P></TD> <TD vAlign=top> <P align=left>8.10</P></TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Speeds</TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Vne (never exceed) </TD> <TD vAlign=top>120 kts    </TD></TR> <TR> <TD vAlign=top>Va (Max.Manoeuvre) </TD> <TD vAlign=top>100 kts</TD></TR> <TR> <TD vAlign=top>Cruise at 75% power </TD> <TD vAlign=top>100 kts </TD></TR> <TR> <TD vAlign=top>Max. Straight & Level </TD> <TD vAlign=top>120 kts    </TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Stall Speeds at Gross Weight </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Vs (full flap) </TD> <TD vAlign=top>35 kts </TD></TR> <TR> <TD vAlign=top>Vso(clean) </TD> <TD vAlign=top>41 kts</TD></TR> <TR> <TD vAlign=top>Climb rate (at sea level) Gross </TD> <TD vAlign=top>600 ft/min</TD></TR> <TR> <TD vAlign=top> <P align=left>Service Ceiling </P></TD> <TD vAlign=top> <P align=left>15,000 ft </P></TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Structural Loading</TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Flight Load Factor</TD> <TD vAlign=top>+3.8   to  -1.9G</TD></TR> <TR> <TD vAlign=top>Structure Tested </TD> <TD vAlign=top>+8.55 to   -3.4G</TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Take Off Distance Groundroll </TD> <TD vAlign=top>200 m       (650 ft) </TD></TR> <TR> <TD vAlign=top> <P align=left>Landing Distance Groundroll </P></TD> <TD vAlign=top> <P align=left>168 m       (546 ft)<STRONG></STRONG></P></TD></TR> <TR> <TD vAlign=top> <P align=left>Glide Ratio (engine idle) </P></TD> <TD vAlign=top> <P align=left>12:1 </P></TD></TR> <TR> <TD vAlign=top> <P align=left>Crosswind Component </P></TD> <TD vAlign=top> <P align=left>14 mph (14 kts) </P></TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top>Fuel System </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top> <P align=left>Fuel Consumption at Cruise </P></TD> <TD vAlign=top> <P align=left>15 lts/hr<STRONG></STRONG></P></TD></TR> <TR> <TD vAlign=top> <P align=left>Range </P></TD> <TD vAlign=top> <P align=left>460 nm   <STRONG></STRONG></P></TD></TR> <TR> <TD vAlign=top> <P align=left>Endurance (nil reserve) </P></TD> <TD vAlign=top> <P align=left>4.6 hrs<STRONG></STRONG></P></TD></TR> <TR> <TD vAlign=top> </TD> <TD vAlign=top> </TD></TR> <TR> <TD vAlign=top> <P align=left>Empty Weight </P></TD> <TD vAlign=top> <P align=left>260 kg (572 lbs)<STRONG></STRONG></P></TD></TR> <TR> <TD vAlign=top> <P align=left>Useable Load </P></TD> <TD vAlign=top> <P align=left>190 kg (418 lbs) </P></TD></TR> <TR> <TD vAlign=top> <P align=left>Gross Weight (MTOW) </P></TD> <TD vAlign=top> <P align=left>450 kg (990 lbs )<STRONG></STRONG></P></TD></TR></TBODY></TABLE> <H3> </H3>