3XTrim에서 생산하며 3X55 모델

<P><SPAN id=writeContents style="FONT-SIZE: 12px"> </P> <DIV>폴란드의 3XTrim에서 생산하며, 미국에는 3X55라는 모델로 판매되는 스포츠플레인이라고 합니다.</DIV> <DIV> </DIV> <P><EMBED src=http://www.youtube.com/v/Jt66ltKK5ss&hl=ko&fs=1 width=425 height=344 type=application/x-shockwave-flash allowfullscreen="true" allowScriptAccess='sameDomain'></EMBED> </P> <DIV> </DIV> <P id=f_line><FONT face=Arial size=3><STRONG>The 3X55</STRONG></FONT> <DIV></DIV> <DIV><FONT face=Arial></FONT> </DIV> <DIV><FONT face=Arial>The 3X55 has been designed and manufactured in </FONT><A href="http://www.3xtrim.pl/" target=_blank><FONT face=Arial color=#0000ff><U>"3Xtrim" Aircraft Factory</U></FONT></A><FONT face=Arial> in Bielsko-Biala (southern Poland). It continues the 55-year tradition and experience of the world class SZD-PZL-Bielsko Glider Factory. The 3Xtrim Airplane Factory was established by Adam Kurbiel, a designer of modern gliders at the SZD-PZL.</FONT></DIV> <DIV><FONT face=Arial></FONT> </DIV> <DIV><FONT face=Arial>3X55 is built to meet the requirements of AULA (Advance Ultra-Light Airplane) and LSA (Light Sport Airplane). Exceptional flying characteristics low maintenance and operational costs, make this aircraft a perfect choice for training and pleasure flying. The very quiet cockpit can be equipped with latest, state of the art “Glass” instruments, radio, transponder and GPS. The 3X55 is also available with glider tow hook, amphibious floats, skis and dedicated trailer. A large-capacity fuel tank can be installed for long cross-country flights.</FONT></DIV> <DIV><FONT face=Arial></FONT> </DIV> <DIV><FONT face=Arial>3X55 has succeded in navigation sport events such as 16th World Precision Flying Champioships in Herning, Denmark, August 2004. The pilot was unbeaten Christopher Wieczorek, who won the Championships and claimed the title of World Champion.</FONT></DIV> <DIV><BR> </DIV> <DIV><A href="http://www.rainbowsportaviation.com/picv.php?path=images/photo_0_b.jpg" target=_blank> <IMG style="CURSOR: pointer" [안내]태그제한으로등록되지않습니다-xxonclick=image_window(this) src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.rainbowsportaviation.com%2Fimages%2Fphoto_0.jpg" name=target_resize_image[] tmp_height="80" tmp_width="163"></A> <A href="http://www.rainbowsportaviation.com/picv.php?path=images/photo_1_b.jpg&fot=Mogens Juhl" target=_blank> <IMG style="CURSOR: pointer" [안내]태그제한으로등록되지않습니다-xxonclick=image_window(this) src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.rainbowsportaviation.com%2Fimages%2Fphoto_1.jpg" name=target_resize_image[] tmp_height="80" tmp_width="120"></A><A href="http://www.rainbowsportaviation.com/picv_n.php?path=images/photo_2_b.jpg" target=_blank> <IMG style="CURSOR: pointer" [안내]태그제한으로등록되지않습니다-xxonclick=image_window(this) src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.rainbowsportaviation.com%2Fimages%2Fphoto_2.jpg" name=target_resize_image[] tmp_height="80" tmp_width="120"></A><A href="http://www.rainbowsportaviation.com/picv.php?path=images/photo_3_b.jpg" target=_blank> <IMG style="CURSOR: pointer" [안내]태그제한으로등록되지않습니다-xxonclick=image_window(this) src="https://img1.daumcdn.net/relay/cafe/original/?fname=http%3A%2F%2Fwww.rainbowsportaviation.com%2Fimages%2Fphoto_3.jpg" name=target_resize_image[] tmp_height="80" tmp_width="120"></A> </DIV> <DIV> </DIV> <DIV> </DIV> <P id=f_line>3X55's main features <DIV></DIV> <UL> <LI> <DIV>Two-seat, high-wing aircraft with fixed tricycle landing gear.</DIV> <LI> <DIV>Very low operational costs, easy and simple maintenance.</DIV> <LI> <DIV>Sandwich structure wings with one spar, ailerons and slotted flaps.</DIV> <LI> <DIV>Comfortable (47.2in width), very quiet, heated and ventilated cockpit accommodates 2 persons up to 2 m in height.</DIV> <LI> <DIV>Spacious baggage compartment behind the pilot seat.</DIV> <LI> <DIV>Composite door frames supported by gas springs with emergency release for quick egress.</DIV> <LI> <DIV>Steerable nose wheel with shock absorbing rubber donuts.</DIV> <LI> <DIV>Fuselage, rudder and horizontal stabilizer made entirely from composites.</DIV> <LI> <DIV>Electric trim with an electronic position indicator.</DIV> <LI> <DIV>One piece, composite main spring landing gear with hydraulic, toe operated disc brakes, ensures safe take-off and landings on all types of airport surfaces.</DIV> <LI> <DIV>Elevator, ailerons and flaps controlled by aluminium push-pull rods, rudder by cables.</DIV> <LI> <DIV>Electrical system has a service-free 12 V, 18 Ah battery, position lights, strobe light on fuselage and landing light on engine cowling.</DIV> <LI> <DIV>On request, 3X55 Trainer may be equipped with a fifth-generation Galaxy Rescue System (GRS), offering safety for the crew and aircraft at speeds up to 127 kts.</DIV></LI></UL> <P id=f_line><FONT size=3><STRONG>Basic Technical Specification</STRONG></FONT> <DIV></DIV> <DIV> <TABLE style="BORDER-TOP-WIDTH: 0px; BORDER-LEFT-WIDTH: 0px; BORDER-BOTTOM-WIDTH: 0px; BORDER-RIGHT-WIDTH: 0px" width=590> <TBODY> <TR> <TD class=marg width=30></TD> <TD width=300 height=20> <DIV><FONT size=2>Wing span</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>9.60 m / 31.5 ft</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Length/height</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>6.87 m / 22.5 ft / 2.4 m / 7.9 ft</FONT></DIV></TD> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Cabin width</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>1.2m / 47.2 in</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Wing area</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>11.84 m<SUP>2</SUP> / 127.4 ft <SUP>2</SUP></FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Wing load</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>46.5 kg/m<SUP>2</SUP> / 9.52 lbs/ft<SUP>2</SUP></FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Manoeuvre load index</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>+3.8 / -1.5 / flaps 2.0</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Max. Take-off weight</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>600 kg / 1322 lbs</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Empty weight</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>325 kg / 716 lbs</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Useful load</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>275 kg / 606 lbs</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Fuel tank capacity std/large</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>18.2 US gal / 22.8 US gal</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Overhaul life</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>as required</FONT></DIV></TD></TR></TBODY></TABLE></DIV> <P id=f_line><FONT size=2></FONT>  <DIV></DIV> <DIV><FONT size=2><STRONG>Performance</STRONG></FONT></DIV> <DIV><FONT size=2>at Rotax 912 ULS engine and fixed pitch propeller - Woodcomp SR200</FONT></DIV> <DIV><BR> <TABLE style="BORDER-TOP-WIDTH: 0px; BORDER-LEFT-WIDTH: 0px; BORDER-BOTTOM-WIDTH: 0px; BORDER-RIGHT-WIDTH: 0px" width=590> <TBODY> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Never Exceed Speed V<SUB>NE</SUB></FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>109 kts</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Cruise speed at MCP</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>100 kts</FONT></DIV></TD> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Cruise speed 75% MCP</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>90 kts</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Stall speed V<SUB>so</SUB></FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>39 kts</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Manoeuvering Speed V<SUB>A</SUB></FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>75 kts</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Maximum Flap Extended Speed V<SUB>FE</SUB>full flaps / take-off flaps</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>62 kts / 74 kts</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Maximum climb rate</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>1000 ft/min / 62 kts</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Take-off distance 50 ft obstacle</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>918 ft / 280 m</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=300 height=20> <DIV><FONT size=2>Range at velocity 90 kts (std/large fuel tank)</FONT></DIV></TD> <TD width=290 height=20> <DIV><FONT size=2>350 NM/650 km / 450 NM/830 km</FONT></DIV></TD></TR></TBODY></TABLE></DIV> <P id=f_line><FONT size=2></FONT>  <DIV></DIV> <DIV><FONT size=2><STRONG>Powerplant</STRONG></FONT></DIV> <DIV> <TABLE style="BORDER-TOP-WIDTH: 0px; BORDER-LEFT-WIDTH: 0px; BORDER-BOTTOM-WIDTH: 0px; BORDER-RIGHT-WIDTH: 0px" width=590> <TBODY> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Engine type</FONT></DIV></TD> <TD width=200 height=20> <DIV><A href="http://www.rotax.com/" target=blank><FONT color=#0000ff size=2><U>Bombardier-Rotax 912 ULS</U></FONT></A></DIV></TD> <TD width=200 height=20> <DIV><A href="http://www.rotax.com/" target=blank><FONT color=#0000ff size=2><U>Bombardier-Rotax 912 UL</U></FONT></A></DIV></TD></TR> <TR> <TD class=marg width=30><FONT color=#0000ff size=2><U></U></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Number cylinders / strokes</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>4/4</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>4/4</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Stroke volume</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>1352 cm<SUP>3</SUP></FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>1211 cm<SUP>3</SUP></FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Peak power MP (5 min.)</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>100 HP / 73.6 kW at 5800 rpm</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>80 HP / 59.6 kW at 5800 rpm</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Max. continuous power MPC</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>95 HP / 69.6 kW at 5500 rpm</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>79 HP / 58.0 kW at 5500 rpm</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Head / cylinder cooling</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>fluid / air</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>fluid / air</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Carburettors</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>2 constant depression</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>2 constant depression</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Electronic ignition</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>dual breakerless capacitor discharge</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>dual breakerless capacitor discharge</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Alternator</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>250 W (option)</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>250 W (option)</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Internal gear ratio</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>1 : 2.43</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>1 : 2.27</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Fuel</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>Euro-Super 95 DIN 51607 or Avgas 100LL</FONT></DIV></TD> <TD width=200 height=20> <DIV><FONT size=2>Euro-Super 95 DIN 51607 or Avgas 100LL</FONT></DIV></TD></TR> <TR> <TD class=marg width=30><FONT size=2></FONT></TD> <TD width=190 height=20> <DIV><FONT size=2>Propeller</FONT></DIV></TD> <TD width=200 colSpan=2 height=20> <DIV><A href="http://www.woodcomp.cz/" target=blank><FONT color=#0000ff size=2><U>Woodcomp SR200</U></FONT></A><FONT size=2>, fixed, dia. 1.7 m / 66.9 in</FONT></DIV> <DIV><A href="http://www.woodcomp.cz/" target=blank><FONT color=#0000ff size=2><U>Woodcomp SR2000</U></FONT></A><FONT size=2>, adjustable in flight (electric), dia. 1.7 m / 66.9in</FONT></DIV></TD></TR></TBODY></TABLE><BR></DIV> <DIV>Technical specifications are subject to change without notice.</DIV> <DIV> </DIV> <DIV> </DIV> <DIV>출처:파일럿</DIV></SPAN>