X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 21 Oct 2012 09:56:38 -0400 Message-ID: X-Original-Return-Path: Received: from nm27-vm4.bullet.mail.ne1.yahoo.com ([98.138.91.187] verified) by logan.com (CommuniGate Pro SMTP 6.0c2) with ESMTPS id 5834732 for lml@lancaironline.net; Sat, 20 Oct 2012 14:21:23 -0400 Received-SPF: none receiver=logan.com; client-ip=98.138.91.187; envelope-from=cwfmd@yahoo.com Received: from [98.138.90.52] by nm27.bullet.mail.ne1.yahoo.com with NNFMP; 20 Oct 2012 18:20:46 -0000 Received: from [98.138.89.194] by tm5.bullet.mail.ne1.yahoo.com with NNFMP; 20 Oct 2012 18:20:46 -0000 Received: from [127.0.0.1] by omp1052.mail.ne1.yahoo.com with NNFMP; 20 Oct 2012 18:20:46 -0000 X-Yahoo-Newman-Property: ymail-3 X-Yahoo-Newman-Id: 424450.72381.bm@omp1052.mail.ne1.yahoo.com Received: (qmail 81723 invoked by uid 60001); 20 Oct 2012 18:20:46 -0000 DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; h=X-YMail-OSG:Received:X-Rocket-MIMEInfo:X-Mailer:Message-ID:Date:From:Subject:To:MIME-Version:Content-Type; b=usPJ7kVbgh8+FtLA5Mn4Kox4HpkJCP5jJ6NFco6UGE5LVyGIkab5SrMQOvZu3JlAjhr94YJPULCbgW2zhf0uGlexCvb6gQ5EYZdWhrGSTLIlvVhc8TF1dscgARPClCrdWgLl01Ow5W2tbr2Fx2hRSXiMxrogTdIkDfSyCfvwWto=; X-YMail-OSG: _HeGrGYVM1nZ3gZ.DB0mylSjXihUoIKYfv8gnskfbgdf0.N D7_MlVt.5_Fz2OOLygtrnGmaVYrhAfGUth3yuAiAZ08_F.8MvT5S.NbRMKtu myA2lfyqltSR77JbEZHZs_I9IrDMjVNYrWQoW2_wb9PZ15rZ85uoe7Jzpswl cd7FyJy14AtVV.3OnV_iu0QsC1BBD045LmeKUVjGTHALxG9cKpN6biBvOmIF 0FFOVT6W3epKx1V7ui15CKFNDYvazyeQwvRnbgs4OGAZQShBMR4TusZejpph j2DxS1Z27WDc7dETTbExlgMmX_plV7j9kWVlCf.2IBKEaM4EFzJECvahD25_ 3xARbv03VBB_wZF2EmxaA0ys6S7NwhqqI61gOJVLG1irtmRd1Cc5Nw2wMTUs ccjFV.gJA435WZKCS_q7OHwZSHh62KV7_CzH86XNxSWbCaonDfqpv2xETnh3 RkwUPjmo04Fba24JrY2seukTY28wPV5tV0onp6aIFo8YA Received: from [98.196.182.216] by web181705.mail.ne1.yahoo.com via HTTP; Sat, 20 Oct 2012 11:20:46 PDT X-Rocket-MIMEInfo: 001.001,DQoNCg0KDQoNCldSVCB0dXJib2NoYXJnZWQgdGFrZW9mZnMgKG5vdCBub3JtYWxseSBhc3BpcmF0ZWQgYXMgZGlzY3Vzc2VkIGluIHRoaXMgdGhyZWFkKQ0KwqANClBsZWFzZSBiZSBjYXV0aW91cyBhYm91dCBjaGFuZ2luZyBmcm9tIG1hbmZhY3R1cmVyJ3MgcmVjb21tZW5kYXRpb25zLCBlc3BlY2lhbGx5IHVuZGVyIGhpZ2ggcG93ZXIsIFR1cmJvQ2hhcmdlZCzCoFRBS0VPRkYsIGV4dHJlbWUgY29uZGl0aW9ucyAoaGlnaCB0ZW1wL2Rlc25zaXR5IGFsdGl0dWRlLSBpZiB1IGhlYXIgdGhhdCBvbiBBU09TLXQBMAEBAQE- X-Mailer: YahooMailClassic/15.0.8 YahooMailWebService/0.8.123.450 X-Original-Message-ID: <1350757246.79135.YahooMailClassic@web181705.mail.ne1.yahoo.com> X-Original-Date: Sat, 20 Oct 2012 11:20:46 -0700 (PDT) From: cwfmd@yahoo.com Subject: Leaning for High Density Altitude takeoff and any climb X-Original-To: Lancair Mailing MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="-237291172-677911632-1350757246=:79135" ---237291172-677911632-1350757246=:79135 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable WRT turbocharged takeoffs (not normally aspirated as discussed in this thre= ad) =A0 Please be cautious about changing from manfacturer's recommendations, espec= ially under high power, TurboCharged,=A0TAKEOFF, extreme conditions (high t= emp/desnsity altitude- if u hear that on ASOS-think! ). I am pretty sure we= lost a friend in 1993, who used to set up his multi-engine Duke for =A0tak= eoff below the recommended specs to "save wear on the engines" and "save ga= s". =A0 =A0It is often the case that our limited gauges, enhanced as they are, may = not tell us about hot spots or short term thermodynamic issues. We might be= amazed at how much faster an undectected condition can cook engine parts, = well below the speed, temporal, or spatial resolution and=A0coverage of you= r best sensors. =A0 Full Rich for takeoff is usually for cooling=A0rather than=A0for power cons= iderations. Takeoff is one of the highest heat stress conditions: Less cool= ing air from zero to=A0Vr and in climb and I suspect. the highest temperatu= re change of the flight- it's still "warming up". =A0 It's good to know as much as we can through these kinds of discussions, but= without hard evidence and lengthy experience, our safety record indicates = we should be very very careful about takeoff ops including:=20 -draining the sumps, -=A0thorough preflight,=20 -careful runup checks,=20 -try both tanks during taxi,, -low threshold of decision to return to the ramp for a spark plug check,=20 -brief your aborted takeoff procedure on runway,=20 =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 landing straig= ht ahead?=A0=A0 (1.5 x takeoff distance is a good rule of thumb for V1) =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0off road ops or=A0through the fence? =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0 =A0or on the highway? It's never perfect but these can always be reviewed and greatly reduce the = bad odds. =A0 Try playing a game: how close did you hit the predicted takeoff distance? =A0=A0=A0=A0 . =A0=A0=A0=A0 a. My estimte gets a little closer each time=A0with practice.= =A0 Here's my data:) =A0=A0=A0=A0 b. I did not notice or record where we lifted off =A0=A0=A0=A0 c. I did not have time to do that calculation.=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0 see =A091.103(b) =A0=A0=A0=A0 d. How do you do that calculation?=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0=A0= =A0=A0=A0=A0=A0=A0=A0=A0=A0=A0 =A0see =A091.13 =A0 Y'all be careful out there! Bill ---237291172-677911632-1350757246=:79135 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
WRT turbocharged takeoffs (not normally aspirated as discussed in this= thread)
 
Please be cautious about changing from manfacturer's recommendations, = especially under high power, TurboCharged, TAKEOFF, extreme conditions= (high temp/desnsity altitude- if u hear that on ASOS-think! ). I am pretty= sure we lost a friend in 1993, who used to set up his multi-engine Duke fo= r  takeoff below the recommended specs to "save wear on the engines" a= nd "save gas".
 
 It is often the case that our limited gauges, enhanced as they a= re, may not tell us about hot spots or short term thermodynamic issues. We = might be amazed at how much faster an undectected condition can cook engine= parts, well below the speed, temporal, or spatial resolution and cove= rage of your best sensors.
 
Full Rich for takeoff is usually for cooling rather than for= power considerations. Takeoff is one of the highest heat stress conditions= : Less cooling air from zero to Vr and in climb and I suspect. the hig= hest temperature change of the flight- it's still "warming up".
 
It's good to know as much as we can through these kinds of discussions= , but without hard evidence and lengthy experience, our safety record indic= ates we should be very very careful about takeoff ops including:
-draining the sumps,
- thorough preflight,
-careful runup checks,
-try both tanks during taxi,,
-low threshold of decision to return to the ramp for a spark plug chec= k,
-brief your aborted takeoff procedure on runway,
           &nbs= p;         landing straight ahead?&= nbsp;  (1.5 x takeoff distance is a good rule of thumb for V1)
           &nbs= p;            &= nbsp;           off = road ops or through the fence?
           &nbs= p;            &= nbsp;           &nbs= p;            &= nbsp;   or on the highway?
It's never perfect but these can always be reviewed and greatly reduce= the bad odds.
 
Try playing a game: how close did you hit the predicted takeoff distan= ce?
     .
     a. My estimte gets a little closer each time&= nbsp;with practice.  Here's my data:)
     b. I did not notice or record where we lifted= off
     c. I did not have time to do that calculation= .            &n= bsp;            = ;       see  91.103(b)
     d. How do you do that calculation?  = ;            &n= bsp;            = ;            &n= bsp;      see  91.13
 
Y'all be careful out there!
Bill
---237291172-677911632-1350757246=:79135--