Let L-410 UVP-E (modification of the model from PWDT) Просмотр ZIP-архива
CVA_L410_UVPE/let410uvpe_ref.htm
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<title>BEECH KING AIR 350</title>
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<p><font face="Verdana" size="2"><b>LET L-410 UVP-E<br>
</b>REFERENCE INFORMATION<br>
<br>
For standard procedures, see the Checklists tab.</font></p>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="361" colspan="3" bgcolor="#C0C0C0" valign="middle">
<p align="center"><b><font face="Verdana" size="2">LIMITATION OF OPERATING
SPEED</font></b></td>
</tr>
<tr>
<td width="75">
<p align="center"><b><font face="Verdana" size="2">Speed designation</font></b></td>
<td width="216">
<p align="center"><b><font face="Verdana" size="2">Name of the speed</font></b></td>
<td width="68">
<p align="center"><b><font face="Verdana" size="2">Speed (km/h) IAS</font></b></td>
</tr>
<tr>
<td width="75"><font size="2" face="Verdana">Vmax.max</font></td>
<td width="216"><font size="2" face="Verdana">Design limit speed (calculated)</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">400</font></b></td>
</tr>
<tr>
<td width="75"><font size="2" face="Verdana">Vmax. MO</font></td>
<td width="216"><font size="2" face="Verdana">Maximum operating speed</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">350</font></b></td>
</tr>
<tr>
<td width="75"><font size="2" face="Verdana">Vmax. FE18</font></td>
<td width="216">
<p align="justify"><font size="2" face="Verdana">Max. permissible cruise
speed with wing flaps extended to 18°</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">250</font></b></td>
</tr>
<tr>
<td width="75"><font size="2" face="Verdana">Vmax. FE42</font></td>
<td width="216">
<p align="justify"><font size="2" face="Verdana">Max. permissible cruise
speed with wing flaps extended to 42°</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">220</font></b></td>
</tr>
<tr>
<td width="75"><font size="2" face="Verdana">Vmax. LO</font></td>
<td width="216">
<p align="justify"><font size="2" face="Verdana">Maximum permissible landing
gear operating speed</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">250*</font></b></td>
</tr>
<tr>
<td width="75"><font size="2" face="Verdana">Vmax. Spoil</font></td>
<td width="216">
<p align="justify"><font size="2" face="Verdana">Maximum permissible spoiler
extension speed</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">190</font></b></td>
</tr>
</table>
<p><font size="2" face="Verdana">* At speed v=205 km/h IAS is extension blocked</font></p>
<h3> </h3>
<h3><span style="font-size: x-small; font-family: Verdana">Flight performance</span></h3>
<p><font size="2" face="Verdana">Flight performance are valid under following
conditions:</font></p>
<p><font size="2" face="Verdana">- international standard atmosphere<br>
- maximum take-off weight 6 400 kg<br>
- customer bleed is off</font></p>
<h4><span style="font-size: x-small; font-family: Verdana">Both engines are
operation</span></h4>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="75" rowspan="4">
<p align="center"><b><font face="Verdana" size="2">(1)</font></b></td>
<td width="216" align="justify">
<p align="center"><font size="2" face="Verdana">Real take-off run at speed v<sub>R</sub>
= 150 km/h IAS (161 km/h EAS)</font></td>
<td width="68" align="center">
<p align="center"><b><font face="Verdana" size="2">400 m.</font></b></td>
</tr>
<tr>
<td width="216" align="justify">
<p align="justify"><font size="2" face="Verdana">Maximum take-off engine
rating, propeller speed</font></td>
<td width="68" align="center"><b><font face="Verdana" size="2">2080 RPM</font></b></td>
</tr>
<tr>
<td width="216" align="left"><font size="2" face="Verdana">take-off
configuration flaps</font></td>
<td width="68" align="center"><b><font face="Verdana"><font size="2">18</font><sup><font size="2">°</font></sup></font></b></td>
</tr>
<tr>
<td width="216" align="left">
<p align="justify"><font size="2" face="Verdana">aerodrome altitude ISA, no
wind, concrete runway steep</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">0 m</font></b></td>
</tr>
</table>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="84" rowspan="2">
<p align="center"><b><font face="Verdana" size="2">(2)</font></b></td>
<td width="236" align="left">
<p align="justify"><font size="2" face="Verdana">Real landing run after
landing speed of 140 km/h IAS when using wheel brakes and reverse thrust of
both engines</font></td>
<td width="62" align="center"><b><font size="2" face="Verdana">240 m *</font></b><p>
<b><font size="2" face="Verdana">* Required runway length</font></b></td>
</tr>
<tr>
<td width="236" align="left">
<p align="justify"><font size="2" face="Verdana">Maximum landing weight Is
6200 kg, both engines idle, landing configuration – wing flaps extended to
42<sup>°</sup>, spoilers. extended before touch-down (as per Flight Manual),
airport altitude: 0 m ISA, no wind, concrete runway steep 0, approach speed
v<sub>a</sub>p<sub>r</sub>= 155 km/h IAS (161 km/h EAS)</font></td>
<td width="62" align="center"><b><font size="2" face="Verdana">800 m (100 m
clearway)</font></b></td>
</tr>
</table>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="75" rowspan="4">
<p align="center"><b><font face="Verdana" size="2">(3)</font></b></td>
<td width="216" align="left"><font size="2" face="Verdana">Climb rate</font></td>
<td width="68"> </td>
</tr>
<tr>
<td width="216" align="left">
<p align="justify"><font size="2" face="Verdana">Maximum continuous engine
rating</font></td>
<td width="68" align="center"> </td>
</tr>
<tr>
<td width="216" align="left"><font size="2" face="Verdana">Propeller speed</font></td>
<td width="68" align="center"><b><font size="2" face="Verdana">1900 RPM</font></b></td>
</tr>
<tr>
<td width="216" align="left">
<p align="justify"><font size="2" face="Verdana">cruise configuration (wing
flaps and landing gear retracted)</font></td>
<td width="68" align="center"> </td>
</tr>
</table>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="74" bgcolor="#C0C0C0">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2"><b>Flight
altitude</b></font></td>
<td width="165" bgcolor="#C0C0C0">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2"><b>Climb time
from 400 m <br>
circuit in minutes</b></font></td>
<td width="120" bgcolor="#C0C0C0">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2"><b>Torque</b></font></td>
</tr>
<tr>
<td width="74" align="center"><font face="Verdana" size="2">500</font></td>
<td width="165" align="center"><font face="Verdana" size="2">0,3</font></td>
<td width="120" align="center">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2">< 100</font></td>
</tr>
<tr>
<td width="74" align="center"><font face="Verdana" size="2">1000</font></td>
<td width="165" align="center"><font face="Verdana" size="2">1,6</font></td>
<td width="120" align="center">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2">< 100</font></td>
</tr>
<tr>
<td width="74" align="center"><font face="Verdana" size="2">2000</font></td>
<td width="165" align="center"><font face="Verdana" size="2">4,4</font></td>
<td width="120" align="center">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2">< 100</font></td>
</tr>
<tr>
<td width="74" align="center"><font face="Verdana" size="2">3000</font></td>
<td width="165" align="center"><font face="Verdana" size="2">7,7</font></td>
<td width="120" align="center">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2">< 100</font></td>
</tr>
<tr>
<td width="74" align="center"><font face="Verdana" size="2">4000</font></td>
<td width="165" align="center"><font face="Verdana" size="2">12,5</font></td>
<td width="120" align="center">
<p style="TEXT-ALIGN: center"><font face="Verdana" size="2">< 100</font></td>
</tr>
</table>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363" height="234">
<tr>
<td width="9%" height="221" rowspan="14"><b><font size="2" face="Verdana">
(5)</font></b></td>
<td width="150%" height="19"><font size="2" face="Verdana">Range</font></td>
</tr>
<tr>
<td width="150%" height="16" valign="top"><font size="2" face="Verdana">
Range value is valid under following conditions:</font></td>
</tr>
<tr>
<td width="150%" height="10"><font size="2" face="Verdana">- 8 main fuel
tanks In the wing</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- max. take-off
weight 6400 kg</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- ISA atmospheric
conditions, no wind</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- two engines
operative</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- leveled flight
block altitude 4200 m</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- cruise speed
365 km/h IAS</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- climb rate at
climbing from 400 m to 4200 m: 3 m/s</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- rate at descent
from 4200 m to 400 m: 3 m/s</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">propeller speed
1900 RPM</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">descent at engine
rating<br>
cruise speed 310 km/h, <br>
propeller speed n<sub>prop</sub> = 1700 RPM</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- range tolerance:
3%</font></td>
</tr>
<tr>
<td width="150%" height="16"><font size="2" face="Verdana">- cruise
configuration (wing flaps retracted)</font></td>
</tr>
</table>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="31" rowspan="3">
<p align="center"><b><font face="Verdana" size="2">(a)</font></b></td>
<td width="329" colspan="2"><font face="Verdana" size="2">Range with maximum
payload 1615 kg and 625 kg of fuel (without wing tip tanks)</font></td>
</tr>
<tr>
<td width="262">
<p align="justify"><font face="Verdana" size="2">- with fuel reserve for 30
minutes at speed 287 km/h IAS at altitude of 2100 m</font></td>
<td width="66" align="center"><b><font face="Verdana" size="2">546 km</font></b></td>
</tr>
<tr>
<td width="262">
<p align="justify"><font face="Verdana" size="2">- with fuel reserve for 45
minutes at speed 287 km/h IAS at altitude of 2100 m</font></td>
<td width="66" align="center"><b><font face="Verdana" size="2">466 km</font></b></td>
</tr>
</table>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="31" rowspan="3">
<p align="center"><b><font face="Verdana" size="2">(b)</font></b></td>
</tr>
<tr>
<td width="328" colspan="2">
<p align="justify"><font face="Verdana" size="2">Maximum range without wing
tip tanks and payload of 1330 kg and 910 kg of fuel</font></td>
</tr>
<tr>
<td width="262">
<p align="justify"><font face="Verdana" size="2">- with fuel reserve for 30
minutes at speed of 287 km/h IAS at altitude 2 100 m</font></td>
<td width="66" align="center"><b><font face="Verdana" size="2">298 km</font></b></td>
</tr>
</table>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="31" rowspan="3">
<p align="center"><b><font face="Verdana" size="2">(c)</font></b></td>
</tr>
<tr>
<td width="328" colspan="2">
<p align="justify"><font size="2" face="Verdana">Maximum range with wing tip
tanks with payload of 885 kg and 1300 kg of fuel</font></td>
</tr>
<tr>
<td width="262">
<p align="justify"><font size="2" face="Verdana">- with fuel reserve for 30
minutes at speed 287 km/h IAS at altitude 2100 m</font></td>
<td width="66" align="center"><b><font face="Verdana" size="2">1380 km</font></b></td>
</tr>
</table>
<h3><span style="font-size: x-small; font-family: Verdana">Flight with one
engine in operative </span></h3>
<h3><span style="font-size: x-small; font-family: Verdana">(1) Climb speed</span></h3>
<p><font size="2" face="Verdana">Intermediate Contingency Power Setting
Propeller speed: 2080 RPM</font></p>
<p><font size="2" face="Verdana">Left engine stopped - feathered propeller,
flight speed = 200 km/h IAS (210 km/h EAS), cruise configuration (wing flaps
and landing gear retracted)</font></p>
<table border="1" cellpadding="0" cellspacing="0" style="border-collapse: collapse" bordercolor="#111111" id="AutoNumber1" width="363">
<tr>
<td width="9%" bgcolor="#C0C0C0">
<p style="TEXT-ALIGN: center"><b><font size="2" face="Verdana">Flight
altitude [m]</font></b></td>
<td width="58%" bgcolor="#C0C0C0">
<p style="TEXT-ALIGN: center"><b><font size="2" face="Verdana">Climb time
from 400 m circuit in minutes</font></b></td>
<td width="92%" bgcolor="#C0C0C0">
<p style="TEXT-ALIGN: center"><b><font size="2" face="Verdana">Torque</font></b></td>
</tr>
<tr>
<td width="9%" align="center"><font face="Verdana" size="2">500</font></td>
<td width="58%" align="center"><font size="2" face="Verdana">1,0</font></td>
<td width="92%">
<p style="TEXT-ALIGN: center"><font size="2" face="Verdana">< 100</font></td>
</tr>
<tr>
<td width="9%" align="center"><font face="Verdana" size="2">1000</font></td>
<td width="58%" align="center"><font size="2" face="Verdana">6,0</font></td>
<td width="92%">
<p style="TEXT-ALIGN: center"><font size="2" face="Verdana">< 100</font></td>
</tr>
<tr>
<td width="9%" align="center"><font face="Verdana" size="2">2000</font></td>
<td width="58%" align="center"><font size="2" face="Verdana">19,0</font></td>
<td width="92%">
<p style="TEXT-ALIGN: center"><font size="2" face="Verdana">< 100</font></td>
</tr>
<tr>
<td width="9%" align="center"><font face="Verdana" size="2">3000</font></td>
<td width="58%" align="center"><font size="2" face="Verdana">40,3</font></td>
<td width="92%">
<p style="TEXT-ALIGN: center"><font size="2" face="Verdana">< 100</font></td>
</tr>
</table>
<p style="MARGIN-TOP: 0px; MARGIN-BOTTOM: 0px">
</p>
<p style="MARGIN-TOP: 0px; MARGIN-BOTTOM: 0px">
<font face="Verdana" size="2"><b>NOTE:</b> This aircraft's
real-world reference informations have been NOT modified for Flight Simulator.</font></p>
<p style="MARGIN-TOP: 0px; MARGIN-BOTTOM: 0px"> </p>
<p style="MARGIN-TOP: 0px; MARGIN-BOTTOM: 0px">
<font face="Verdana" size="2">FARNAIR Hungary Ltd.</font></p>
</body>
</html>
25708-CVA-L410-UVPE.zip
| Имя файла | Дата | Размер |
|---|---|---|
| CVA_L410_UVPE/410cas.jpg | 13.05.2005 21:58 | 68 KB |
| CVA_L410_UVPE/410dhl.jpg | 13.05.2005 21:56 | 67 KB |
| CVA_L410_UVPE/410olimex.jpg | 13.05.2005 21:57 | 61 KB |
| CVA_L410_UVPE/410olimex04.jpg | 13.05.2005 21:57 | 63 KB |
| CVA_L410_UVPE/Aircraft.cfg | 29.06.2005 20:36 | 13 KB |
| CVA_L410_UVPE/docs/ | 28.06.2005 00:08 | |
| CVA_L410_UVPE/docs/back.jpg | 12.04.2004 04:48 | 16 KB |
| CVA_L410_UVPE/docs/fs_01.jpg | 02.08.2004 06:25 | 22 KB |
| CVA_L410_UVPE/docs/fs_02.jpg | 02.08.2004 06:25 | 21 KB |
| CVA_L410_UVPE/docs/fs_03.jpg | 02.08.2004 06:25 | 22 KB |
| CVA_L410_UVPE/docs/fs_04.jpg | 05.08.2004 15:20 | 27 KB |
| CVA_L410_UVPE/docs/fs_05.jpg | 05.08.2004 15:21 | 18 KB |
| CVA_L410_UVPE/docs/l410.gif | 15.03.2004 20:40 | 2 KB |
| CVA_L410_UVPE/docs/L410_readme.html | 23.08.2004 03:30 | 22 KB |
| CVA_L410_UVPE/docs/logo.gif | 13.04.2004 02:42 | 10 KB |
| CVA_L410_UVPE/docs/Normal_checklist1.pdf | 24.07.2004 14:53 | 326 KB |
| CVA_L410_UVPE/docs/Normal_checklist2.pdf | 24.07.2004 14:55 | 243 KB |
| CVA_L410_UVPE/docs/real_01.jpg | 02.08.2004 06:22 | 18 KB |
| CVA_L410_UVPE/docs/real_02.jpg | 02.08.2004 06:23 | 19 KB |
| CVA_L410_UVPE/docs/real_03.JPG | 02.08.2004 06:22 | 18 KB |
| CVA_L410_UVPE/L-410 UVP-E.air | 21.06.2005 17:09 | 15 KB |
| CVA_L410_UVPE/let410uvpe_check.htm | 26.08.2004 03:48 | 32 KB |
| CVA_L410_UVPE/let410uvpe_ref.htm | 26.08.2004 03:49 | 16 KB |
| CVA_L410_UVPE/model.uvp-e_d/ | 27.06.2005 23:54 | |
| CVA_L410_UVPE/model.uvp-e_d/l-410 uvp-e dvc.mdl | 21.06.2005 17:36 | 2 MB |
| CVA_L410_UVPE/model.uvp-e_d/Model.cfg | 26.03.2005 22:10 | 34 B |
| CVA_L410_UVPE/model.uvp-e_s/ | 27.06.2005 23:54 | |
| CVA_L410_UVPE/model.uvp-e_s/l-410 uvp-e svc.mdl | 21.06.2005 17:34 | 2 MB |
| CVA_L410_UVPE/model.uvp-e_s/Model.cfg | 26.03.2005 22:10 | 34 B |
| CVA_L410_UVPE/panel/ | 28.06.2005 00:08 | |
| CVA_L410_UVPE/panel/cpt.toggles.737.CAB | 07.11.2002 07:55 | 30 KB |
| CVA_L410_UVPE/panel/cpt.toggles.light.green.CAB | 07.11.2002 07:57 | 52 KB |
| CVA_L410_UVPE/panel/cva_l410_v1_1.gau | 04.10.2004 01:29 | 5 MB |
| CVA_L410_UVPE/panel/cva_l410_xml_v1_0.cab | 19.04.2005 01:11 | 5 KB |
| CVA_L410_UVPE/panel/l410_ident.cab | 30.10.2003 06:19 | 780 B |
| CVA_L410_UVPE/panel/l410_main.bmp | 26.02.2005 15:34 | 769 KB |
| CVA_L410_UVPE/panel/l410_radio.bmp | 26.06.2004 16:22 | 164 KB |
| CVA_L410_UVPE/panel/l410_switches.bmp | 10.03.2005 21:58 | 317 KB |
| CVA_L410_UVPE/panel/panel.cfg | 28.06.2005 00:01 | 9 KB |
| CVA_L410_UVPE/README_cz.txt | 29.06.2005 20:27 | 2 KB |
| CVA_L410_UVPE/rmd_l410.xml | 29.06.2005 01:56 | 1 KB |
| CVA_L410_UVPE/sound/ | 27.06.2005 23:54 | |
| CVA_L410_UVPE/sound/Sound.cfg | 03.10.2003 03:34 | 42 B |
| CVA_L410_UVPE/texture/ | 29.06.2005 02:14 | |
| CVA_L410_UVPE/texture/l410_fuse.bmp | 28.06.2005 00:18 | 683 KB |
| CVA_L410_UVPE/texture/l410_glass.bmp | 30.08.2003 03:13 | 5 KB |
| CVA_L410_UVPE/texture/l410_panel.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture/l410_panel_b.bmp | 19.04.2005 00:44 | 683 KB |
| CVA_L410_UVPE/texture/l410_panel_c.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture/l410_panel_c_L.bmp | 26.03.2005 19:39 | 512 KB |
| CVA_L410_UVPE/texture/l410_parts.bmp | 28.06.2005 00:20 | 683 KB |
| CVA_L410_UVPE/texture/l410_parts_b.bmp | 28.06.2005 00:26 | 683 KB |
| CVA_L410_UVPE/texture/l410_parts_c.bmp | 12.10.2003 04:11 | 341 KB |
| CVA_L410_UVPE/texture/l410_parts_d.bmp | 26.03.2005 19:45 | 128 KB |
| CVA_L410_UVPE/texture/l410_parts_e.bmp | 28.06.2005 00:28 | 683 KB |
| CVA_L410_UVPE/texture/l410_props.bmp | 30.10.2003 02:57 | 1 MB |
| CVA_L410_UVPE/texture/l410_wing.bmp | 28.06.2005 00:29 | 683 KB |
| CVA_L410_UVPE/texture/rm_thumb.jpg | 29.06.2005 02:14 | 23 KB |
| CVA_L410_UVPE/texture.rda2/ | 29.06.2005 02:17 | |
| CVA_L410_UVPE/texture.rda2/l410_fuse.bmp | 28.06.2005 00:30 | 683 KB |
| CVA_L410_UVPE/texture.rda2/l410_glass.bmp | 30.08.2003 03:13 | 5 KB |
| CVA_L410_UVPE/texture.rda2/l410_panel.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture.rda2/l410_panel_b.bmp | 19.04.2005 00:44 | 683 KB |
| CVA_L410_UVPE/texture.rda2/l410_panel_c.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture.rda2/l410_panel_c_L.bmp | 26.03.2005 19:39 | 512 KB |
| CVA_L410_UVPE/texture.rda2/l410_parts.bmp | 28.06.2005 00:30 | 683 KB |
| CVA_L410_UVPE/texture.rda2/l410_parts_b.bmp | 28.06.2005 00:31 | 683 KB |
| CVA_L410_UVPE/texture.rda2/l410_parts_c.bmp | 12.10.2003 04:11 | 341 KB |
| CVA_L410_UVPE/texture.rda2/l410_parts_d.bmp | 26.03.2005 19:45 | 128 KB |
| CVA_L410_UVPE/texture.rda2/l410_parts_e.bmp | 28.06.2005 00:28 | 683 KB |
| CVA_L410_UVPE/texture.rda2/l410_props.bmp | 30.10.2003 02:57 | 1 MB |
| CVA_L410_UVPE/texture.rda2/l410_wing.bmp | 28.06.2005 00:32 | 683 KB |
| CVA_L410_UVPE/texture.rda2/rm_thumb.jpg | 29.06.2005 02:17 | 22 KB |
| CVA_L410_UVPE/texture.rda3/ | 29.06.2005 02:15 | |
| CVA_L410_UVPE/texture.rda3/l410_fuse.bmp | 28.06.2005 00:32 | 683 KB |
| CVA_L410_UVPE/texture.rda3/l410_glass.bmp | 30.08.2003 03:13 | 5 KB |
| CVA_L410_UVPE/texture.rda3/l410_panel.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture.rda3/l410_panel_b.bmp | 19.04.2005 00:44 | 683 KB |
| CVA_L410_UVPE/texture.rda3/l410_panel_c.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture.rda3/l410_panel_c_L.bmp | 26.03.2005 19:39 | 512 KB |
| CVA_L410_UVPE/texture.rda3/l410_parts.bmp | 28.06.2005 00:37 | 683 KB |
| CVA_L410_UVPE/texture.rda3/l410_parts_b.bmp | 28.06.2005 00:38 | 683 KB |
| CVA_L410_UVPE/texture.rda3/l410_parts_c.bmp | 12.10.2003 04:11 | 341 KB |
| CVA_L410_UVPE/texture.rda3/l410_parts_d.bmp | 26.03.2005 19:45 | 128 KB |
| CVA_L410_UVPE/texture.rda3/l410_parts_e.bmp | 28.06.2005 00:28 | 683 KB |
| CVA_L410_UVPE/texture.rda3/l410_props.bmp | 30.10.2003 02:57 | 1 MB |
| CVA_L410_UVPE/texture.rda3/l410_wing.bmp | 28.06.2005 00:38 | 683 KB |
| CVA_L410_UVPE/texture.rda3/rm_thumb.jpg | 29.06.2005 02:15 | 22 KB |
| CVA_L410_UVPE/texture.rda4/ | 29.06.2005 02:16 | |
| CVA_L410_UVPE/texture.rda4/l410_fuse.bmp | 28.06.2005 00:39 | 683 KB |
| CVA_L410_UVPE/texture.rda4/l410_glass.bmp | 30.08.2003 03:13 | 5 KB |
| CVA_L410_UVPE/texture.rda4/l410_panel.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture.rda4/l410_panel_b.bmp | 19.04.2005 00:44 | 683 KB |
| CVA_L410_UVPE/texture.rda4/l410_panel_c.bmp | 26.03.2005 19:45 | 512 KB |
| CVA_L410_UVPE/texture.rda4/l410_panel_c_L.bmp | 26.03.2005 19:39 | 512 KB |
| CVA_L410_UVPE/texture.rda4/l410_parts.bmp | 28.06.2005 00:40 | 683 KB |
| CVA_L410_UVPE/texture.rda4/l410_parts_b.bmp | 28.06.2005 00:40 | 683 KB |
| CVA_L410_UVPE/texture.rda4/l410_parts_c.bmp | 12.10.2003 04:11 | 341 KB |
| CVA_L410_UVPE/texture.rda4/l410_parts_d.bmp | 26.03.2005 19:45 | 128 KB |
| CVA_L410_UVPE/texture.rda4/l410_parts_e.bmp | 28.06.2005 00:28 | 683 KB |
| CVA_L410_UVPE/texture.rda4/l410_props.bmp | 30.10.2003 02:57 | 1 MB |
| CVA_L410_UVPE/texture.rda4/l410_wing.bmp | 28.06.2005 00:41 | 683 KB |
| CVA_L410_UVPE/texture.rda4/rm_thumb.jpg | 29.06.2005 02:16 | 22 KB |
| CVA_L410_UVPE/ | 29.06.2005 02:51 | |
| avsim_su.diz | 11.12.2009 01:31 | 406 B |
| Итого: | 40 MB | |
Modified by Czech authors model from PWDT (http://www.avsim.su/f/fs2004-originalnie-samoleti-40/pwdt-let-l-410-uvp-3120.html) Changed the 2D panel (for the better) refined dynamics. If you'd like to tie the panel and the dynamics of the original model.
→ Size:
10 MB
→ Date:
16 years ago (10.12.2009 22:49)
→ Approved by moderator:
Aleks_Balagur
→ License:
Freeware - Free version, Do Not Redistribute
→ Downloaded:
5204 time(s)