X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 16 Oct 2005 20:25:08 -0400 Message-ID: X-Original-Return-Path: <5zq@cox.net> Received: from eastrmmtao03.cox.net ([68.230.240.36] verified) by logan.com (CommuniGate Pro SMTP 5.0c4) with ESMTP id 766288 for lml@lancaironline.net; Sun, 16 Oct 2005 09:44:19 -0400 Received-SPF: none receiver=logan.com; client-ip=68.230.240.36; envelope-from=5zq@cox.net Received: from OFFICE ([68.110.249.147]) by eastrmmtao03.cox.net (InterMail vM.6.01.05.02 201-2131-123-102-20050715) with SMTP id <20051016134307.RXAL2767.eastrmmtao03.cox.net@OFFICE> for ; Sun, 16 Oct 2005 09:43:07 -0400 X-Original-Message-ID: <001101c5d257$98ec2e10$6401a8c0@OFFICE> From: "Bill&Sue" <5zq@cox.net> X-Original-To: "Lancair Mailing List" References: Subject: Re: [LML] FliteStar Model X-Original-Date: Sun, 16 Oct 2005 09:43:31 -0400 MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="----=_NextPart_000_000D_01C5D236.118716E0" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.2180 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 This is a multi-part message in MIME format. ------=_NextPart_000_000D_01C5D236.118716E0 Content-Type: multipart/alternative; boundary="----=_NextPart_001_000E_01C5D236.118716E0" ------=_NextPart_001_000E_01C5D236.118716E0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Naf, this file might be required also. Bill Does anyone have a FliteStar Aircraft Data file for the LNC2? Mine is = corrupted and I'm too lazy to start over. Naf Paul Nafziger LNC2 N7PN ------=_NextPart_001_000E_01C5D236.118716E0 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Naf, this file might be required = also.
 
Bill
 
 
 
 
 
 
Does = anyone have a=20 FliteStar Aircraft Data file for the LNC2?  Mine is corrupted and = I'm too=20 lazy to start over.
 
Naf
 
Paul Nafziger
LNC2 N7PN
 
------=_NextPart_001_000E_01C5D236.118716E0-- ------=_NextPart_000_000D_01C5D236.118716E0 Content-Type: text/plain; name="N5ZQ.txt" Content-Transfer-Encoding: quoted-printable Content-Disposition: attachment; filename="N5ZQ.txt" [Aircraft Setup Information] Aircraft Type=3DPiston variable pitch Speed Units=3DKnots Fuel Units=3DGallons Weight Units=3DPounds CG Units=3DInches [Basic Aircraft Data] Make=3DLANCAIR 320 Model=3DLNC2 Registration=3DN5ZQ Color=3DW EquipmentFAA=3D/G EquipmentICAO=3DSG/C Home Base=3DVA42 Fuel capacity=3D52 Taxi fuel=3D0.50 Takeoff fuel=3D1.00 Service ceiling=3D18000 Service ceiling ROC=3D200 Sea level ROC=3D500 Indicated climb speed=3D140 Indicated descent speed=3D170 Descent rate=3D500 Sea level climb fuel rate=3D11.00 Service ceiling climb fuel rate=3D7.00 Primary fuel burn=3D0.00 Secondary Fuel burn=3D0.00 Use Fuel On Board=3DFALSE Data version=3D4 [Operating Costs] TBO hours=3D2000 Annual hours=3D250 [Operating Cost Items] # Type, Description, Cost Annual, "Annual inspection", 1000.00 Hourly, "Maintenance reserve", 3.00 Annual, "Avionics reserve", 300.00 Annual, "Hangar/tiedown", 0.00 Fuel, "Fuel", 2.30 Hourly, "Oil", 1.00 Annual, "Oxygen refill", 30.00 Annual, "Insurance", 500.00 Annual, "Depreciation", 0.00 [ICAO Flight Plan Info] Wake Turbulance Category=3DLight Radio=3D2 Survival=3D2 Jackets=3D22 Dinghies=3DTRUE Dinghies Number=3D1 Dinghies Capacity=3D2 Dinghies Cover=3DFALSE Dinghies Colour=3DYELLOW Additional Other Information=3D [Weight & Balance Data] Envelope Weight Low=3D1100 Envelope Weight High=3D2000 Envelope CG Low=3D20.00 Envelope CG High=3D32.00 Max Gross Weight=3D1900 Fuel Density=3D6.00 Min CG Pos=3D22.80 Max CG Pos=3D30.30 [Weight & Balance Main Envelope Points] # Weight, Arm 1184, 22.80 1184, 30.30 1900, 30.30 1900, 22.80 1184, 22.80 [Weight & Balance Moment Items] # Type, Description, DefaultWeight, MinWeight, MaxWeight, = FuelBurnOrder, Arm # or, for variable arm items:=20 # Type, Description, DefaultWeight, MinWeight, MaxWeight, = FuelBurnOrder # Weight, Arm Fixed, "Empty weight", 1184, -1, 1184, 1, 21.9 Passenger, "Passenger", 0, -1, 240, 1, 43.0 Baggage, "Baggage 1 ", 10, 0, 100, 1, 63.0 Baggage, "Baggage 2", 0, 0, 50, 1, 82.0 Baggage, "Aft Shelf", 0, 0, 10, 1, 100.0 Fuel, "Fuel Header Tank", 60, 30, 60, 2, 7.1 Fuel, "Fuel Wing Tanks ", 120, 0, 252, 1, 37.8 Crew, "Pilot - Bill", 180, 0, 180, 1, 43.0 Crew, "Pilot - Sue", 140, 0, 140, 1, 43.0 [Performance Info] Performance Model=3DQuick Default values=3DVALID Default Climb Power=3D65 Default Climb MP=3D0.00 Default Cruise Altitude=3D8000 Default Cruise Power=3D75 Default Cruise MP=3D0.00 Default Descent Power=3D60 Default Descent MP=3D0.00 Default Holding Power=3D45 Default Holding MP=3D0.00 Minimum RPM=3D1200 Maximum RPM=3D0 Minimum MP=3D14.00 Maximum MP=3D0.00 Maximum TAS=3D180 Maximum Fuel Flow=3D9.20 [Quick Model] Label1=3D45, "" Label2=3D60, "" Label3=3D75, "" DisplayPercent=3DTRUE [Quick Model Data] # Weight, Altitude, Fuel, TAS, Fuel, TAS, Fuel, TAS Maximum, 1000, 6.5, 130, 7.5, 155, 9.2, 180 Maximum, 4000, 5.8, 130, 7.0, 153, 8.7, 180 Maximum, 8000, 5.4, 133, 6.8, 150, 8.5, 180 Maximum, 12000, 5.0, 135, 6.3, 148, 7.6, 170 Maximum, 16000, 4.5, 138, 6.0, 145, 6.8, 162 [Quick Model Data - Temperature Effect] # Weight, FuelChange ISA -20, FuelChange ISA +20, SpeedChange ISA -20, = SpeedChange ISA +20 Maximum, 0.0, 0.0, 0.0, 0.0 ------=_NextPart_000_000D_01C5D236.118716E0--