Просмотр ZIP-архива - Nardi FN-333

Nardi FN-333 Просмотр ZIP-архива

FN-333/FN-333/FN333_check.htm

<body bgcolor="#3399FF" background="docs_files/docbkg.jpg" text="#FF6600" link="#FFFF00" vlink="#FFFF00" alink="#FFFF00">
<p><strong><font color="#FF6600" size="5" face="Verdana, Arial, Helvetica, sans-serif">Nardi 
  FN-333 Riviera Checklist:</font></strong></p>
<p><font color="#FF6600"><img src="Docs_files/FN333_checklist.jpg" width="200" height="142"></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">PRE 
  FLIGHT CONTROL CHECK<br>
  Before flight verify you have full control authority. Perform while sitting 
  on the ground with the engine off.<br>
  Elevator Up 25.0<br>
  Elevator Down 20.0<br>
  Aileron Up 25.0<br>
  Aileron Down 18.0<br>
  Rudder 25.0</font></strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>______________________________________________________<br>
  STARTUP<br>
  Mixture : 100%<br>
  Fuel Pump: ON<br>
  Fuel Valve: OPEN<br>
  Fuel Selector: BOTH<br>
  Magnetos: START<br>
  Throttle: 0%</strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>______________________________________________________<br>
  TAKEOFF<br>
  Elevator Trim Set to 0.0 deg<br>
  Flaps AS NEEDED (0.0 or 10.0 deg)<br>
  Throttle 100% (or derated if possible)<br>
  Brakes RELEASE<br>
  V1 50 KIAS<br>
  V2 60 KIAS - ROTATE <br>
  _______________________________________________________<br>
  NORMAL CLIMB<br>
  Throttle 70%<br>
  Airspeed 110 KIAS</strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>_______________________________________________________<br>
  CRUISE (FAST)<br>
  Throttle 90%<br>
  Airspeed 140 KIAS</strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>CRUISE 
  (BEST RANGE)<br>
  Throttle 70%<br>
  Airspeed 130 KIAS</strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>_______________________________________________________<br>
  LANDING<br>
  Airspeed - Pattern 70 KIAS<br>
  Flaps DOWN<br>
  Gear DOWN<br>
  Floats UP<br></strong></font><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>Water 
  Rudder UP<br>
  Airspeed - Over the Fence 60 KIAS</strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>_______________________________________________________<br>
  WATER LANDING<br>
  Airspeed - Pattern 70 KIAS<br>
  Flaps DOWN<br>
  Gear UP<br>
  Floats DOWN</strong></font><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong><br>Water 
  Rudder AS DESIRED<br>
  Airspeed - Over the Fence 60 KIAS</strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>_______________________________________________________</strong></font></p>
<p align="center"><strong><font size="+1">FEDERAL AVIATION AGENCY</font></strong></p>
<div align="right"> 
  <table width="100" height="1" cellpadding="0" cellspacing="0">
    <tr bgcolor="#FF6600"> 
      <td height="1" width="1"></td>
      <td></td>
      <td width="1"></td>
    </tr>
    <tr> 
      <td bgcolor="#FF6600"></td>
      <td>7A5<br>
        Revision 2<br>
        NARDI<br>
        FN-333<br>
        April 18, 1963</td>
      <td bgcolor="#FF6600"></td>
    </tr>
    <tr bgcolor="#FF6600"> 
      <td height="1" width="1"></td>
      <td></td>
      <td height="1" width"1"></td>
    </tr>
  </table>
  <br>
</div>
<p align="center"><strong><u><br>
  TYPE CERTIFICATE DATA SHEET NO. 7A5</u></strong></p>
<p align="justify"><br>
  This data sheet which is a part of type certificate No. 7A5 prescribes conditions 
  and limitations under which the product for which the type certificate was issued 
  meets the airworthiness requirements of the Civil Air Regulations.</p>
<table width="100%" border="0" cellspacing="0" cellpadding="0">
  <tr>
    <td width="25%">Type Certificate Holder</td>
    <td width="25%">NARDI S. A.</td>
  </tr>
  <tr>
    <td> </td>
    <td>Milan, Italy</td>
  </tr>
</table>
<p align="left"><br>
  <u><strong>I - Model FN-333, 4 PCAmM (Normal Category), approved December 15, 
  1958</strong></u><br>
</p>
<table width="100%" border="0" cellpadding="0" cellspacing="0">
  <tr> 
    <td>Engine </td>
    <td width="5%"> </td>
    <td colspan="2">Continental IO-470-P</td>
  </tr>
  <tr> 
    <td>Fuel * </td>
    <td> </td>
    <td colspan="2">91/96 Minimum grade aviation gasoline</td>
  </tr>
  <tr> 
    <td>Engine limits *</td>
    <td> </td>
    <td colspan="2"> For all operations, 2600 r.p.m. (250 hp.)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td colspan="2"> </td>
  </tr>
  <tr> 
    <td>Propeller and</td>
    <td> </td>
    <td colspan="2">1. Hartzell HC82X20-5L/L8433-H</td>
  </tr>
  <tr> 
    <td>  propeller limits</td>
    <td> </td>
    <td>   </td>
    <td> 2 blades, metal, constant speed with reversible pitch</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">Maximum diameter 84 in.</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">Maximum diameter 81 in. (No further reduction permitted)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">Pitch settings at 30 in. sta.:</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">   Low 13°, high 27°30', reversed -14°</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td colspan="2"> </td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td colspan="2">2. Hartzell HCA3X20-5L/L8433-6B</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">3 blades, metal, constant speed with reversible pitch</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">Maximum diameter 78 in.</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">Maximum diameter 76 in. (No further reduction permitted)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">Pitch settings at 30 in. sta.:</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>   </td>
    <td colspan="2">   Low 12°30", high 28°30', reversed 
      -14°30'</td>
  </tr>
</table>
<br>
<table width="100%" border="0" cellpadding="0" cellspacing="0">
  <tr> 
    <td width="20%">Airspeed limits</td>
    <td width="5%"> </td>
    <td width= "40%">*Vne (never exceed)</td>
    <td width="55%"> 206 m.p.h. (178 knots)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>*Vno (max. structural cruising) </td>
    <td>162 m.p.h. (140 knots)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>#Vp (maneuvering speed)</td>
    <td> 146.5 m.p.h. (127 knots)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>*Vfe (flaps extended in all positions) </td>
    <td>125 m.p.h. (109 knots)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>*Vle (landing gear extended) </td>
    <td>125 m.p.h. (109 knots)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>*Vfle (wing floats extended) </td>
    <td>125 m.p.h. (109 knots)</td>
  </tr>
  <tr> 
    <td> </td>
    <td> </td>
    <td>*Vwre (water rudder extended) </td>
    <td>206 m.p.h. (178 knots)</td>
  </tr>
</table>
<br>
<table width="100%" border="0" cellpadding="0" cellspacing="0">
  <tr> 
    <td width="30%">C.G. range </td>
    <td width="5%"> </td>
    <td width="75%">*(+110) to (+117)</td>
  </tr>
  <tr> 
    <td>(landing gear extended)</td>
    <td> </td>
    <td> </td>
  </tr>
  <tr> 
    <td>Empty weight C.G. range</td>
    <td> </td>
    <td> None</td>
  </tr>
  <tr> 
    <td>Datum</td>
    <td> </td>
    <td> Nose of aircraft</td>
  </tr>
  <tr> 
    <td>Leveling means </td>
    <td> </td>
    <td>Datum pads on left door frame</td>
  </tr>
  <tr> 
    <td>Maximum weight </td>
    <td> </td>
    <td>*3270 lb.</td>
  </tr>
  <tr> 
    <td>No. seats</td>
    <td> </td>
    <td> 4 (2 at +52.1, 2 at +95.3)</td>
  </tr>
  <tr> 
    <td>Maximum baggage </td>
    <td> </td>
    <td>*300 lb. (+95.3)</td>
  </tr>
  <tr> 
    <td>Fuel capacity</td>
    <td> </td>
    <td> 65.8 U.S. gal. (two wing tanks, 32.9 U.S. gal. ea.) (+107.5)</td>
  </tr>
  <tr> 
    <td>Oil capacity</td>
    <td> </td>
    <td> 3.5 U.S. gal. (+141.6). See NOTE 1 for data on system oil.</td>
  </tr>
</table>
<br>
<table width="100%" border="0" cellspacing="0" cellpadding="0">
  <tr> 
    <td width="30%">Control surface movements</td>
    <td width="3%"> </td>
    <td width="15%">Wing flaps </td>
    <td width="3%"> </td>
    <td width="12%"> </td>
    <td width="3%"> </td>
    <td width="15%"> Down 45°</td>
  </tr>
  <tr>
    <td> </td>
    <td> </td>
    <td>Aileron</td>
    <td> </td>
    <td>Up 25°</td>
    <td> </td>
    <td>Down 18°</td>
  </tr>
  <tr>
    <td> </td>
    <td> </td>
    <td>Elevator Tab</td>
    <td> </td>
    <td>Up 23°</td>
    <td> </td>
    <td>Down 23°</td>
  </tr>
  <tr>
    <td> </td>
    <td> </td>
    <td>Elevator</td>
    <td> </td>
    <td>Up 25°</td>
    <td> </td>
    <td>Down 20°</td>
  </tr>
  <tr>
    <td> </td>
    <td> </td>
    <td>Rudder</td>
    <td> </td>
    <td>Right 25°</td>
    <td> </td>
    <td>Left 25°</td>
  </tr>
  <tr>
    <td> </td>
    <td> </td>
    <td>Stabilizer</td>
    <td> </td>
    <td>Fixed</td>
    <td> </td>
    <td> </td>
  </tr>
</table>
<br>
<table width="100%" border="0" cellspacing="0" cellpadding="0">
  <tr> 
    <td width="20%" height="58" valign="top">Serial Nos. eligible</td>
    <td width="5%"> </td>
    <td width="70%"><p>The Registro Aeronautico Italiano (RAI) Certificate of 
        Airworthiness endorsed as noted below under "Certification basis" 
        must be submitted for each individual aircraft for which application for 
        certification is made.<br> </p>
      </td>
  </tr>
  <tr>
    <td valign="top">Certification basis</td>
    <td> </td>
    <td>CAR 10. Type Certificate No. 7A5 issued December 25, 1958.<br>
      Date of Application for Type Certificate December 3, 1957.<br>
      Each aircraft and any replacement parts manufactured in Italy must be clearly 
      identified as imported.<br> </td>
  </tr>
  <tr>
    <td> </td>
    <td> </td>
    <td>A U.S. airworthiness certificate may be issued on the basis of a Certificate 
      of Airworthiness for Export signed by a representative of the Registro Aeronautico 
      Italiano (RAI) containing the following statement: "The airplane covered 
      by this certificate has been examined and found to comply with U.S. Civil 
      Air Regulations Part 3, dated May 15, 1956, including Amendments 3-1, 3-2, 
      3-3, 3-4 and 3-5, and conforms to TC 7A5."<br> </td>
  </tr>
  <tr>
    <td valign="top">Equipment</td>
    <td> </td>
    <td>The basic required equipment as prescribed in the applicable airworthiness 
      regulations (see Certification Basis) must be installed in the aircraft 
      for certification. In addition, the following item of equipment is required:<br> </td>
  </tr>
  <tr>
    <td> </td>
    <td> </td>
    <td>(a) Pre-stall warning indicator, Safe Flight Instrument Corp. 164.S</td>
  </tr>
</table>
<br>
<table width="100%" border="0" cellspacing="0" cellpadding="0">
  <tr>
    <td valign="top" width="20%">NOTE 1. </td>
    <td width="80%">Current weight and balance report including list of equipment in certificated 
      empty weight, and loading instructions, must be provided for each aircraft 
      at the time of original certification. The certificated empty weight and 
      corresponding center of gravity locations must include system oil of 1 lb. 
      at (+141.6).<br> </td>
  </tr>
  <tr>
    <td valign="top">NOTE 2.</td>
    <td>The following placards must be displayed on the instrument panel in full 
      view of the pilot:
      <table width="100%" border="0" cellspacing="0" cellpadding="0">
        <tr>
          <td width="5%" valign="top">(a)</td>
          <td width="5%"> </td>
          <td width="90%">"THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY 
            AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE 
            FORM OF PLACARDS, MARKINGS. NO ACROBATIC MANEUVERS, INCLUDING SPINS, 
            ARE APPROVED."<br> </td>
        </tr>
        <tr>
          <td valign="top">(b)</td>
          <td> </td>
          <td>"WARNING: REVERSING PROPELLER IN FLIGHT PROHIBITED. OPERATE 
            REVERSE LEVER IN LOW PITCH ONLY. MAXIMUM 2400 RPM IN REVERSE PITCH."<br> </td>
        </tr>
        <tr>
          <td valign="top">(c)</td>
          <td> </td>
          <td> In addition to the above placards, the prescribed operating limitations 
            indicated by "*" under Section I above, must be displayed 
            by permanent markings.<br> </td>
        </tr>
      </table></td>
  </tr>
</table>
<p><br>
  NOTE 3. This aircraft is approved for night flying when the prescribed equipment 
  is installed.</p>
<p align="center"><br>
  .....END.....</p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>_______________________________________________________</strong></font></p>
<p><font color="#FF6600"><strong><font color="#FFFF00" face="Verdana, Arial, Helvetica, sans-serif"><a href="panel_FN333.htm">View 
  Panel Instructions </a></font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif"><a href="FN333_REF.htm">View 
  Reference </a></font></strong></font></p>
<p><strong><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/riviera_sticker.gif" width="266" height="76"></font></strong> 
</p>
<p><strong><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><a href="http://www.mariopilot.6x.to"><img src="Docs_files/signature_forum.gif" width="316" height="40" border="0"></a></font></strong> 
</p>

55674-FN-333.zip

Имя файла	Дата	Размер
FN-333/effects/	07.10.2007 13:59
FN-333/effects/fx_FN333_beacon.fx	29.09.2007 18:49	3 KB
FN-333/effects/FX_FN333_ll.fx	30.09.2007 15:41	2 KB
FN-333/effects/fx_FN333_navgre.fx	29.09.2007 18:49	5 KB
FN-333/effects/fx_FN333_navred.fx	29.09.2007 18:49	5 KB
FN-333/effects/fx_FN333_navwhi.fx	30.09.2007 15:20	5 KB
FN-333/effects/fx_FN333_StartUp.fx	29.09.2007 18:51	2 KB
FN-333/effects/fx_FN333_vclight.fx	28.09.2007 22:23	1 KB
FN-333/effects/texture/	07.10.2007 14:00
FN-333/effects/texture/Beacon.bmp	01.04.2006 20:21	65 KB
FN-333/effects/texture/NAV_Green.bmp	16.03.2006 22:08	65 KB
FN-333/effects/texture/NAV_Red.bmp	16.03.2006 22:08	65 KB
FN-333/effects/texture/NAV_White.bmp	18.03.2006 00:41	65 KB
FN-333/FN-333/	07.10.2007 14:00
FN-333/FN-333/Aircraft.cfg	06.10.2007 18:22	11 KB
FN-333/FN-333/Docs_files/	07.10.2007 14:01
FN-333/FN-333/Docs_files/ADF_help.jpg	06.10.2007 15:57	48 KB
FN-333/FN-333/Docs_files/docbkg.jpg	30.09.2007 20:15	35 KB
FN-333/FN-333/Docs_files/FN333_checklist.jpg	30.09.2007 18:53	24 KB
FN-333/FN-333/Docs_files/FN333_climb.jpg	30.09.2007 18:55	25 KB
FN-333/FN-333/Docs_files/FN333_cruise.jpg	30.09.2007 18:56	27 KB
FN-333/FN-333/Docs_files/FN333_dvc.jpg	06.10.2007 15:38	183 KB
FN-333/FN-333/Docs_files/FN333_floating.jpg	30.09.2007 19:01	29 KB
FN-333/FN-333/Docs_files/FN333_landing.jpg	30.09.2007 18:59	31 KB
FN-333/FN-333/Docs_files/FN333_panel.jpg	06.10.2007 15:14	333 KB
FN-333/FN-333/Docs_files/FN333_splas_off.jpg	30.09.2007 19:00	28 KB
FN-333/FN-333/Docs_files/FN333_splash.jpg	30.09.2007 19:01	22 KB
FN-333/FN-333/Docs_files/FN333_startup.jpg	30.09.2007 18:59	24 KB
FN-333/FN-333/Docs_files/FN333_takeoff.jpg	30.09.2007 18:58	24 KB
FN-333/FN-333/Docs_files/FN333_taxi.jpg	30.09.2007 18:58	27 KB
FN-333/FN-333/Docs_files/FN333_turn.jpg	30.09.2007 18:57	28 KB
FN-333/FN-333/Docs_files/Fuel_Digi_Bkg.gif	06.10.2007 15:41	20 KB
FN-333/FN-333/Docs_files/gearfloat_status.gif	06.10.2007 15:33	12 KB
FN-333/FN-333/Docs_files/GEARFLOATWR_back.gif	06.10.2007 16:30	16 KB
FN-333/FN-333/Docs_files/Oil_Digi_Bkg.gif	06.10.2007 15:46	22 KB
FN-333/FN-333/Docs_files/riviera_sticker.gif	06.10.2007 16:40	7 KB
FN-333/FN-333/Docs_files/signature_forum.gif	06.10.2007 16:43	11 KB
FN-333/FN-333/FN-333.air	29.09.2007 16:50	11 KB
FN-333/FN-333/FN333_check.htm	07.10.2007 15:14	15 KB
FN-333/FN-333/FN333_ref.htm	07.10.2007 15:13	22 KB
FN-333/FN-333/model/	07.10.2007 14:03
FN-333/FN-333/model/FN-333.mdl	29.09.2007 19:59	3 MB
FN-333/FN-333/model/model.cfg	16.09.2006 19:05	25 B
FN-333/FN-333/panel/	07.10.2007 14:17
FN-333/FN-333/panel/compass.bmp	07.08.2007 16:05	24 KB
FN-333/FN-333/panel/DVCL.bmp	01.09.2007 14:40	1 MB
FN-333/FN-333/panel/DVCR.bmp	29.09.2007 16:01	1 MB
FN-333/FN-333/panel/ENGINE_GAUGES_PANEL.bmp	29.09.2007 16:08	60 KB
FN-333/FN-333/panel/MN_FN333.cab	30.09.2007 18:19	2 MB
FN-333/FN-333/panel/panel.cfg	28.09.2007 22:10	8 KB
FN-333/FN-333/panel/panel_2D.bmp	27.07.2007 17:32	1 MB
FN-333/FN-333/panel/SWITCHES_PANEL.bmp	29.09.2007 16:09	91 KB
FN-333/FN-333/panel/throttle_panel.bmp	05.08.2007 18:10	165 KB
FN-333/FN-333/panel/throttle_panel_VC.bmp	31.08.2007 17:52	165 KB
FN-333/FN-333/panel/WARNINGS_PANEL.bmp	30.07.2007 17:25	78 KB
FN-333/FN-333/panel_FN333.htm	06.10.2007 16:45	12 KB
FN-333/FN-333/README.txt	07.10.2007 14:22	5 KB
FN-333/FN-333/sound/	07.10.2007 14:04
FN-333/FN-333/sound/c172_gyro.wav	15.08.2001 03:06	4 MB
FN-333/FN-333/sound/c172_noncombustion1.wav	28.08.2001 08:14	279 KB
FN-333/FN-333/sound/c172_noncombustion2.wav	28.08.2001 08:14	292 KB
FN-333/FN-333/sound/c172_prop1a.wav	30.06.2001 04:08	59 KB
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FN-333/FN-333/sound/c172_prop2b.wav	30.06.2001 04:08	87 KB
FN-333/FN-333/sound/door_small_close.wav	10.04.2003 02:06	56 KB
FN-333/FN-333/sound/door_small_open.wav	10.04.2003 02:06	60 KB
FN-333/FN-333/sound/ext_1500.wav	06.06.2006 13:59	108 KB
FN-333/FN-333/sound/ext_2400.wav	05.06.2006 18:11	127 KB
FN-333/FN-333/sound/ext_3400.wav	06.08.2006 18:26	24 KB
FN-333/FN-333/sound/EXT_idle.wav	06.08.2006 17:46	68 KB
FN-333/FN-333/sound/ext_shutdown.wav	06.08.2006 18:56	51 KB
FN-333/FN-333/sound/ext_startup.wav	06.08.2006 18:48	33 KB
FN-333/FN-333/sound/FN-333_FLAPS.wav	16.09.2007 18:41	319 KB
FN-333/FN-333/sound/FN-333_GEAR-DOWN.wav	16.09.2007 18:40	912 KB
FN-333/FN-333/sound/FN-333_GEAR-UP.wav	16.09.2007 18:40	970 KB
FN-333/FN-333/sound/FN-333_STALL.wav	15.11.2003 15:56	104 KB
FN-333/FN-333/sound/in_1500.wav	06.06.2006 13:57	93 KB
FN-333/FN-333/sound/in_2400.wav	05.02.2006 14:15	127 KB
FN-333/FN-333/sound/in_3400.wav	06.06.2006 13:46	70 KB
FN-333/FN-333/sound/in_idle.wav	06.08.2006 17:48	82 KB
FN-333/FN-333/sound/in_shutdown.wav	06.08.2006 19:04	55 KB
FN-333/FN-333/sound/in_startup.wav	06.08.2006 18:39	43 KB
FN-333/FN-333/sound/sound.cfg	26.09.2007 20:28	9 KB
FN-333/FN-333/sound/starter_EXT.wav	06.06.2006 13:02	111 KB
FN-333/FN-333/sound/starter_IN.wav	06.06.2006 13:00	105 KB
FN-333/FN-333/sound/waterloop.wav	01.03.2002 04:26	704 KB
FN-333/FN-333/sound/xc172_noncombustion1.wav	30.06.2001 04:08	132 KB
FN-333/FN-333/sound/xc172_noncombustion2.wav	30.06.2001 04:08	159 KB
FN-333/FN-333/sound/xc172_prop1a.wav	30.06.2001 04:08	78 KB
FN-333/FN-333/sound/xc172_prop1b.wav	30.06.2001 04:08	67 KB
FN-333/FN-333/sound/xc172_prop2a.wav	30.06.2001 04:08	70 KB
FN-333/FN-333/sound/xc172_prop2b.wav	30.06.2001 04:08	87 KB
FN-333/FN-333/Texture/	07.10.2007 14:17
FN-333/FN-333/Texture/compass_L.bmp	28.09.2007 22:16	16 KB
FN-333/FN-333/Texture/DVCL_L.bmp	28.09.2007 22:17	256 KB
FN-333/FN-333/Texture/DVCR_L.bmp	29.09.2007 19:09	256 KB
FN-333/FN-333/Texture/FN333_C1.bmp	28.09.2007 18:42	1 MB
FN-333/FN-333/Texture/FN333_C2.bmp	28.09.2007 23:24	1 MB
FN-333/FN-333/Texture/FN333_Lfuselage.bmp	27.09.2007 17:33	1 MB
FN-333/FN-333/Texture/FN333_Lwing.bmp	27.09.2007 18:20	1 MB
FN-333/FN-333/Texture/FN333_rfins.bmp	28.09.2007 14:57	1 MB
FN-333/FN-333/Texture/FN333_Rfuselage.bmp	27.09.2007 17:31	1 MB
FN-333/FN-333/Texture/FN333_rwing.bmp	27.09.2007 18:21	1 MB
FN-333/FN-333/Texture/FN333_T1.bmp	28.09.2007 15:56	1 MB
FN-333/FN-333/Texture/prop_FN333.bmp	03.08.2006 14:02	64 KB
FN-333/FN-333/Texture/throttle_panel_L.bmp	28.09.2007 22:31	64 KB
avsim_su.diz	06.01.2015 18:30	406 B
Итого:		28 MB

Nardi FN-333 | Rating: 5!

FS2004 Aircrafts

- Screenshot 2

- Screenshot 3

Итальянская амфибия выпущенная в ограниченном количестве в 60 годах. Хорошая динамика, оригинально сделан выпуск и уборка шасси. Приборная панель фотореалистичная, я не стал ее менять потому что там есть кнопка водяного руля. На воде при помощи этого руля он рулит очень шустро.

→ Size: 15 MB

→ Date: 11 years ago (06.01.2015 15:36)

→ Author: Неизвестен

→ Uploaded by: fuligan (uploaded 15 files )

→ Approved by moderator: 3255936bb9516e6ffaf7cf5cdb0070fd

→ License: Freeware - Free version, Unlimited Distribution

→ Downloaded: 519 time(s)

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