Dynamics An-24RV ver. 5.102 Просмотр ZIP-архива
An-24RV_flight_instructions_EN.htm
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<title>An-24RV version 2</title>
</head>
<body lang=HU link=blue vlink=purple>
<p class=MsoNormal align=center style='text-align:center'><b><span lang=EN-US
style='font-size:12.0pt'>SamDim Design</span></b></p>
<p class=MsoNormal align=center style='text-align:center'><b><span lang=EN-US
style='font-size:14.0pt'>AN-24RV aircraft</span></b></p>
<p class=MsoNormal align=center style='text-align:center'><b><span lang=EN-US> </span></b></p>
<h1><span lang=EN-US>Flight Instructions</span></h1>
<p class=MsoNormal><span lang=EN-US>Attention: metric system. 100 kts = 185
km/h. 1000 ft = 328 m. 10 miles = 18.5 km</span></p>
<p class=MsoNormal><span lang=EN-US>Regimes for engine AI-24:</span></p>
<table class=MsoNormalTable border=0 cellspacing=0 cellpadding=0
style='margin-left:95.65pt;border-collapse:collapse'>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><b><span lang=EN-US>Regime (mode)</span></b></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><b><span lang=EN-US>UPRT %</span></b></p>
</td>
</tr>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>Take off</span></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>87-100</span></p>
</td>
</tr>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>Nominal</span></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>65</span></p>
</td>
</tr>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>0.85 nom.</span></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>52</span></p>
</td>
</tr>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>0.7 nom.</span></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>41</span></p>
</td>
</tr>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>0.6 nom.</span></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>34</span></p>
</td>
</tr>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>0.4 nom.</span></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>22</span></p>
</td>
</tr>
<tr>
<td width=165 valign=top style='width:124.0pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>0.2 nom.</span></p>
</td>
<td width=104 valign=top style='width:77.95pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>12</span></p>
</td>
</tr>
</table>
<p class=MsoNormal><span lang=EN-US> </span></p>
<h2><span lang=EN-US>Taxiing</span></h2>
<p class=MsoNormal><span lang=EN-US>Disengage the parking brake, the slowly
advance the power levers until UPRT is around 30%. Once the plane starts moving
cut back the power to around UPRT 20-25% for a taxi speed 30</span> <span
lang=EN-US>km/h (16 kts).</span></p>
<h2><span lang=EN-US>Take-off and climbing</span></h2>
<p class=MsoNormal><span lang=EN-US>Flaps to 15° (third position).</span></p>
<p class=MsoNormal><span lang=EN-US>Arm the brakes, turn propeller lock ON and
raise the throttle briefly to 40%. Then raise to 100% and release the brakes
(press "."). Start to raise the plane at ~200 km/h, take off should
be at ~220-250 km/h (depending on the weight). Keep the pitch approximately
8-9°. (max 10 deg.). After take off retract the gear. Above 250 km/h and
minimum 120m above ground altitude (AGL) raise the flaps. After raising the
flaps, use trimm and throttle to keep the climbing rate constant and the speed
at 300 km/h (162 kts). At about 400m AGL reduce UPRT 65% (nominal), and set
pitch for a stable 300 km/h climbing. Climb rate will be as follows:</span></p>
<table class=MsoNormalTable border=0 cellspacing=0 cellpadding=0
style='margin-left:127.6pt;border-collapse:collapse'>
<tr>
<td width=109 valign=top style='width:81.45pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><b><span lang=EN-US>altitude (m)</span></b></p>
</td>
<td width=123 valign=top style='width:92.15pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal align=center style='margin-top:3.0pt;margin-right:0cm;
margin-bottom:3.0pt;margin-left:0cm;text-align:center'><b><span lang=EN-US>climb
rate (m/s)</span></b></p>
</td>
</tr>
<tr>
<td width=109 valign=top style='width:81.45pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>0-2000</span></p>
</td>
<td width=123 valign=top style='width:92.15pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal align=center style='margin-top:3.0pt;margin-right:0cm;
margin-bottom:3.0pt;margin-left:0cm;text-align:center'><span lang=EN-US>7.0</span></p>
</td>
</tr>
<tr>
<td width=109 valign=top style='width:81.45pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>2000-3000</span></p>
</td>
<td width=123 valign=top style='width:92.15pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal align=center style='margin-top:3.0pt;margin-right:0cm;
margin-bottom:3.0pt;margin-left:0cm;text-align:center'><span lang=EN-US>6.0</span></p>
</td>
</tr>
<tr>
<td width=109 valign=top style='width:81.45pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>3000-4000</span></p>
</td>
<td width=123 valign=top style='width:92.15pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal align=center style='margin-top:3.0pt;margin-right:0cm;
margin-bottom:3.0pt;margin-left:0cm;text-align:center'><span lang=EN-US>5.0</span></p>
</td>
</tr>
<tr>
<td width=109 valign=top style='width:81.45pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>4000-5000</span></p>
</td>
<td width=123 valign=top style='width:92.15pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal align=center style='margin-top:3.0pt;margin-right:0cm;
margin-bottom:3.0pt;margin-left:0cm;text-align:center'><span lang=EN-US>4.0</span></p>
</td>
</tr>
<tr>
<td width=109 valign=top style='width:81.45pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm'><span lang=EN-US>5000-6000</span></p>
</td>
<td width=123 valign=top style='width:92.15pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal align=center style='margin-top:3.0pt;margin-right:0cm;
margin-bottom:3.0pt;margin-left:0cm;text-align:center'><span lang=EN-US>3.0</span></p>
</td>
</tr>
</table>
<h2><span lang=EN-US>Cruising</span></h2>
<p class=MsoNormal><span lang=EN-US>Economic cruising mode is UPRT 52% (0.85
nominal). The best economical flight altitude is about 5000 m (16400 ft).</span></p>
<table class=MsoNormalTable border=0 cellspacing=0 cellpadding=0
style='margin-left:38.95pt;border-collapse:collapse'>
<tr>
<td width=78 valign=top style='width:58.6pt;border:none;border-bottom:solid windowtext 1.0pt;
padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><b><span lang=EN-US>Altitude <br>
(m)</span></b></p>
</td>
<td width=82 valign=top style='width:61.85pt;border:none;border-bottom:solid windowtext 1.0pt;
padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><b><span lang=EN-US>Altitude
(feet)</span></b></p>
</td>
<td width=85 valign=top style='width:63.8pt;border:none;border-bottom:solid windowtext 1.0pt;
padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><b><span lang=EN-US>UPRT</span></b></p>
</td>
<td width=85 valign=top style='width:63.8pt;border:none;border-bottom:solid windowtext 1.0pt;
padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><b><span lang=EN-US>IAS <br>
(km/h)</span></b></p>
</td>
<td width=94 valign=top style='width:70.85pt;border:none;border-bottom:solid windowtext 1.0pt;
padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><b><span lang=EN-US>IAS<br>
(knt)</span></b></p>
</td>
<td width=85 valign=top style='width:63.8pt;border:none;border-bottom:solid windowtext 1.0pt;
padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><b><span lang=EN-US>TAS <br>
(km/h)</span></b></p>
</td>
</tr>
<tr>
<td width=78 valign=top style='width:58.6pt;border:none;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>5 000</span></p>
</td>
<td width=82 valign=top style='width:61.85pt;border:none;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>16 400</span></p>
</td>
<td width=85 valign=top style='width:63.8pt;border:none;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>52%</span></p>
</td>
<td width=85 valign=top style='width:63.8pt;border:none;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>330-340</span></p>
</td>
<td width=94 valign=top style='width:70.85pt;border:none;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>172-178</span></p>
</td>
<td width=85 valign=top style='width:63.8pt;border:none;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>440</span></p>
</td>
</tr>
<tr>
<td width=78 valign=top style='width:58.6pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>6 000</span></p>
</td>
<td width=82 valign=top style='width:61.85pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>19 700</span></p>
</td>
<td width=85 valign=top style='width:63.8pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>52%</span></p>
</td>
<td width=85 valign=top style='width:63.8pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>320-330</span></p>
</td>
<td width=94 valign=top style='width:70.85pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>172-178</span></p>
</td>
<td width=85 valign=top style='width:63.8pt;padding:0cm 3.5pt 0cm 3.5pt'>
<p class=MsoNormal style='margin-top:3.0pt;margin-right:0cm;margin-bottom:
3.0pt;margin-left:0cm;page-break-after:avoid'><span lang=EN-US>460</span></p>
</td>
</tr>
</table>
<p class=MsoNormal><span lang=EN-US> </span></p>
<h2><span lang=EN-US>Descending</span></h2>
<p class=MsoNormal><span lang=EN-US>Descending mode is UPRT 20-30%. The alarm
horn will be on below 38%. If bothers (I guess yes), turn ЗВУК
- sound alarms switch OFF on the Engineer's panel. No speed brakes, so pay
attention of speed.</span></p>
<p class=MsoNormal><span lang=EN-US>Descend by approximately 350-360 km/h
(180-185 kts) IAS and 5 to 10 m/s (900 to 1800 ft/min) of descend rate. Keep
300 km/h (162 kts) on downwind and base legs. </span></p>
<p class=MsoNormal><span lang=EN-US>The critical speed for descending is 540
km/h (290 kts) to avoid structure deformation.</span></p>
<h2><span lang=EN-US>Landing</span></h2>
<p class=MsoNormal><span lang=EN-US>Keep speed 300 km/h (162 kts) on pattern.
On the downwind leg, extend the gear. On the base leg deploy the flaps to 15°
and reduce speed to 250 km/h (130 kts). Before the final approach deploy the
landing lights and the flaps to 38°. Keep speed approximately 200-210 km/h
(108-110 kts) on the final approach. Before the touchdown reduce UPRT around 12-15%,
and after touchdown UPRT 0%. Disengage (turn off) "propeller lock".
Propeller blade angle will drop and that will create a rather strong back
thrust (and noise). The brakes can be used below speed 150 km/h (81 kts)
only. </span></p>
<h2><span lang=EN-US>Critical parameters</span></h2>
<p class=MsoNormal><span lang=EN-US>Maximal speed on descend: 540 km/h (290 kts)</span></p>
<p class=MsoNormal><span lang=EN-US>Maximal speed to deploy the gear: 300 km/h
(162 kts)</span></p>
<p class=MsoNormal><span lang=EN-US>Maximal speed to deploy the flaps to 15°:
300 km/h (162 kts)</span></p>
<p class=MsoNormal><span lang=EN-US>Maximal speed to deploy the flaps to 38°:
250 km/h (135 kts)</span></p>
<p class=MsoNormal><span lang=EN-US>Maximal flight altitude: 8 400 m (26 800
ft)</span></p>
<p class=MsoNormal><span lang=EN-US>Maximal side-speed of wind: 12 m/c (22 kts)</span></p>
<p class=MsoNormal><span lang=EN-US>Take off distance: about 900 m (2950 ft)</span></p>
<p class=MsoNormal><span lang=EN-US>Landing distance: about 600 m (2000 ft)</span></p>
<h2><span lang=EN-US>Fuel calculation</span></h2>
<p class=MsoNormal><span lang=EN-US>(unit: 1 lbs = 0.4536 kg)</span></p>
<p class=MsoNormal><span lang=EN-US>Fuel consumption during cruising at
altitude 6000 m (FL197): 705 kg/h (1550 lbs/h)</span></p>
<p class=MsoNormal><span lang=EN-US>Fuel for taxi to line up and climbing to
FL197 and descending from FL197, approach and taxi to full stop: 600 kg (1323
lbs) </span></p>
<p class=MsoNormal><span lang=EN-US>Note that climb to FL197 and descend from
FL197 takes approximately 200 km.</span></p>
<p class=MsoNormal><i><span lang=EN-US>Example: calculate necessary fuel for
distance 750 km at altitude 6000 m and cruising speed 460 km/h GS.</span></i></p>
<ol style='margin-top:0cm' start=1 type=1>
<li class=MsoNormal><span lang=EN-US>Estimate distance for cruising flight:
750 km - 200 km = 550 km </span></li>
<li class=MsoNormal><span lang=EN-US>Estimate duration of cruising at final
flight level: 550/460 = 1.2 h</span></li>
<li class=MsoNormal><span lang=EN-US>Fuel needed for cruising flight: 705 kg/h
* 1.2 h = 846 kg</span></li>
<li class=MsoNormal><span lang=EN-US>Total fuel needed for flight: 600 kg +
846 kg = 1446 kg</span></li>
<li class=MsoNormal><span lang=EN-US>Take 500 kg of reserve fuel (depends on
alternate airport distance)</span></li>
</ol>
<p class=MsoNormal><span lang=EN-US>Grand total: 1446 kg + 500 kg = <b>1946 kg</b></span></p>
</body>
</html>
26308-Dynamics-An24RV-v.5.102.zip
| Имя файла | Дата | Размер |
|---|---|---|
| Loader_Manager_An24/ | 05.01.2010 06:58 | |
| Loader_Manager_An24/CFG/ | 05.01.2010 06:58 | |
| Loader_Manager_An24/CFG/AN24A.CFG | 25.06.2007 19:07 | 2 KB |
| Loader_Manager_An24/CONFIG.CFG | 05.01.2010 07:45 | 167 B |
| Loader_Manager_An24/IMG/ | 05.01.2010 06:58 | |
| Loader_Manager_An24/IMG/AN24A.bmp | 21.06.2007 17:51 | 236 KB |
| Loader_Manager_An24/IMG/BusSeatEmpty.bmp | 05.06.2007 01:57 | 2 KB |
| Loader_Manager_An24/IMG/BusSeatLoad.bmp | 05.06.2007 01:58 | 2 KB |
| Loader_Manager_An24/IMG/EcoSeatEmpty.bmp | 05.06.2007 01:57 | 2 KB |
| Loader_Manager_An24/IMG/EcoSeatLoad.bmp | 05.06.2007 01:58 | 2 KB |
| Loader_Manager_An24/IMG/img001.bmp | 27.06.2007 04:44 | 2 KB |
| Loader_Manager_An24/IMG/img001_B.bmp | 27.06.2007 04:43 | 2 KB |
| Loader_Manager_An24/IMG/img002.bmp | 27.06.2007 04:44 | 450 B |
| Loader_Manager_An24/IMG/img002_B.bmp | 27.06.2007 04:43 | 450 B |
| Loader_Manager_An24/IMG/img003.bmp | 27.06.2007 04:44 | 486 B |
| Loader_Manager_An24/IMG/img003_B.bmp | 27.06.2007 04:43 | 486 B |
| Loader_Manager_An24/IMG/img004.bmp | 27.06.2007 04:44 | 582 B |
| Loader_Manager_An24/IMG/img004_B.bmp | 27.06.2007 04:43 | 582 B |
| Loader_Manager_An24/LMAn24.exe | 04.07.2007 03:06 | 896 KB |
| Loader_Manager_An24/LNG/ | 05.01.2010 06:58 | |
| Loader_Manager_An24/LNG/ENGLISH.LNG | 04.07.2007 02:56 | 806 B |
| Loader_Manager_An24/LNG/RUSSIAN.LNG | 04.07.2007 02:56 | 909 B |
| Loader_Manager_An24/load.ini | 20.10.2009 02:13 | 1 KB |
| Aircraft.cfg | 05.01.2010 07:39 | 13 KB |
| An-24RV_flight_instructions_EN.htm | 31.05.2005 01:18 | 21 KB |
| An-24RV_flight_instructions_RU.htm | 05.01.2010 07:20 | 23 KB |
| Antonov An-24RV.air | 05.01.2010 06:55 | 14 KB |
| Readme.txt | 05.01.2010 08:11 | 1 KB |
| avsim_su.diz | 05.01.2010 12:15 | 406 B |
| Итого: | 1 MB | |
The next version of dynamics (5.102) for the aircraft Samdim An-24RV. The main changes are conserned to the the control on bank and pitch and ground effect.
→ Size:
412 KB
→ Date:
16 years ago (05.01.2010 10:03)
→ Author:
Александр Терентьев АКА Aless
→ Approved by moderator:
Arhangel
→ License:
Freeware - Free version, Unlimited Distribution
→ Downloaded:
3962 time(s)