Просмотр ZIP-архива - Nardi FN-333

Nardi FN-333 Просмотр ZIP-архива

FN-333/FN-333/FN333_ref.htm

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<p><strong><font color="#FF6600" size="5" face="Verdana, Arial, Helvetica, sans-serif">Nardi 
  FN-333 Riviera Handbook:</font></strong></p>
<p><font color="#FF6600" size="4" face="Verdana, Arial, Helvetica, sans-serif"><strong><em>Startup 
  Procedure:</em></strong></font></p>
<p><font color="#FF6600"><em><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_startup.jpg" width="200" height="160"></font></strong></em></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>To 
  Startup the engine, first check if:</strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">Mixture 
  : 100%<br>
  Fuel Pump: ON<br>
  Fuel Valve: OPEN<br>
  Fuel Selector: BOTH<br>
  Magnetos: BOTH<br>
  Throttle: 0%</font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">Then 
  turn the starter key and wait for the engine to start. Idling RPM is around 
  1000.</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Taxiing- 
  GROUND:</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_taxi.jpg" width="200" height="160"></font></strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>Taxiing 
  on ground is accomplished by just adding a little of power and steering with 
  Rudder Pedals. You may use reverse thrust to go backwards, but don't let the 
  aircraft gain too much speed while backing up. The riviera can spalsh from the 
  ground to the water if the shore is adequate (on Flight Simulator this can always 
  be done). From groud to water you need to lower your floats before entering 
  water, and it is better to leave water rudder UP during the transition to avoid 
  it hitting the ground. Once you are floating, retract the landing gear (it is 
  prepared for such operation).</strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Taxiing- 
  WATER:</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_floating.jpg" width="200" height="128"></font></strong></font></p>
<p><font color="#FF6600" face="Verdana, Arial, Helvetica, sans-serif"><strong>Taxiing 
  on water requires more power than on ground to start moving. Steering with Rudder 
  Pedals can be done when there's enough speed, otherwise the water rudder should 
  be used. You may use reverse thrust to go backwards, but in water the system 
  needs to be "forced" to run at a higher power or it will not be enough 
  to start moving. To do this, quickly move your throttle to any desired setting 
  between 35% and 70%, quickly cut off to 0% and pull the reverse lever (or press 
  F2). Again don't let the aircraft gain too much speed while backing up. The 
  riviera can get out from the water to the ground if the shore is adequate (on 
  Flight Simulator this can always be done). From water to ground you need to 
  extend your landing gear uderwater (it is prepared for such operation). It is 
  better to set water rudder UP during the transition to avoid it hitting the 
  ground. Once you are on ground, retract the floats.</strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"></font></strong></font></p>
<p> </p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Taking 
  Off - GROUND:</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_takeoff.jpg" width="200" height="160"></font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">To 
  Take off, set elevator trim at 0% or accrdignly on your CG position - aircraft 
  load status. Set one notch of flaps (11°). Make sure that Propeller condition 
  is at full forward. Check that water rudder is retracted and floats are UP. 
  Advance Throttle to 100% (or derated if possible) slowly and rotate when the 
  aircraft reaches 60 KIAS. After the aircraft lifts off, retract your landing 
  gear, and set prop pitch to bleow 2500 RPM (yellow line) to prevent engine from 
  overheating and oil pressure to stay on red line. Maximum power of 250 HP @2600 
  RPM (Full Forward) is available only for short time. <font color="#FF6600"><strong> 
  When enough speed is reached (~96 KIAS) retract flaps.</strong></font></font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Taking 
  Off - WATER:</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_splas_off.jpg" width="200" height="160"></font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">To 
  Take off, set elevator trim at 0% or accrdignly on your CG position - aircraft 
  load status. Set one notch of flaps (11°). Make sure that Propeller condition 
  is at full forward. Set Water Rudder as desired and leave floats DOWN. check 
  landing gear UP. Advance Throttle to 100% (or derated if possible) slowly and 
  rotate when the aircraft reaches 60 KIAS. After the aircraft lifts off, retract 
  the floats. Set prop pitch to bleow 2500 RPM (yellow line) to prevent engine 
  from overheating and oil pressure to stay on red line. Maximum power of 250 
  HP @2600 RPM (Full Forward) is available only for short time. When enough speed 
  is reached (~96 KIAS) retract flaps.</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Manoeuvering- 
  turns :</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_turn.jpg" width="200" height="160"></font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">The 
  Riviera need a little of rudder pressure in the direction of the turn to compensate 
  the little slipping that otherwise occurs. The tighter the turn, the more the 
  rudder required. After a certain bank angle is no longer possible to compensate 
  the slip without losing rapidly altitude.</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Cruise:</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_cruise.jpg" width="200" height="159"></font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">You 
  Can cruise at altitudes Up to 8000 Ft or as high as you can breathe on a non-pressurized 
  aircraft... With a throttle setting at about 75% you should travel at around 
  130 KIAS. Remember to set prop pitch for a maximum RPM of 2500. You can set 
  it at lower values for noise reduction or greater fuel economy at altitude.</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Landing 
  - GROUND:</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_landing.jpg" width="200" height="160"></font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">To 
  land on ground check: Floats and Water rudder UP. To Land You may keep a speed 
  not lower than 41 KIAS that is full flaps stall speed. Lower than 45 the plane 
  approaches stall and becomes unstable. You can anyway try (at your own risk) 
  to land at 40 KIAS for very short-field results. Ideal landing speed over the 
  fence is about 60 KIAS, then you just throttle back to idle and gently pull 
  the nose up. Landing is always done with full flaps. Propeller must be reset 
  to full forward during the short final approach in order for the reverser to 
  work properly. You can either stop the Riviera by braking, engaging prop reverser 
  or simply letting it roll. Applying brakes and reverser will stop the plane 
  very quickly.</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif">Landing 
  - WATER:</font></strong></font></p>
<p><font color="#FF6600"><strong><font size="4" face="Verdana, Arial, Helvetica, sans-serif"><img src="Docs_files/FN333_splash.jpg" width="200" height="107"></font></strong></font></p>
<p><font color="#FF6600"><strong><font face="Verdana, Arial, Helvetica, sans-serif">To 
  land on WATER check: Floats DOWN and Water rudder AS DESIRED, Landing Gear UP. 
  To Land You may keep a speed not lower than 41 KIAS that is full flaps stall 
  speed. Lower than 45 the plane approaches stall and becomes unstable. You can 
  anyway try (at your own risk) to land at 40 KIAS for very short-field results. 
  Ideal landing speed over the fence is about 60 KIAS, then you just throttle 
  back to idle and gently pull the nose up. Landing is always done with full flaps. 
  Propeller must be reset to full forward during the short final approach in order 
  for the reverser to work properly. You can stop the Riviera only by engaging 
  prop reverser (brakes won't be of any use...). </font></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 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_Check.htm">View 
  Checklist </a></font></strong></font></p>
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55674-FN-333.zip

Имя файла	Дата	Размер
FN-333/effects/	07.10.2007 13:59
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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
FN-333/FN-333/sound/c172_prop1b.wav	30.06.2001 04:08	64 KB
FN-333/FN-333/sound/c172_prop2a.wav	30.06.2001 04:08	65 KB
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: 1170ff8ee450e614b4b3735f6e28c1f3

→ License: Freeware - Free version, Unlimited Distribution

→ Downloaded: 519 time(s)

Comments 1 View ZIP-Content Download

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