X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 01 May 2011 13:00:23 -0400 Message-ID: X-Original-Return-Path: Received: from mta31.charter.net ([216.33.127.82] verified) by logan.com (CommuniGate Pro SMTP 5.4c3j) with ESMTP id 4963289 for lml@lancaironline.net; Sun, 01 May 2011 08:30:08 -0400 Received-SPF: pass receiver=logan.com; client-ip=216.33.127.82; envelope-from=lhenney@charter.net Received: from imp09 ([10.20.200.9]) by mta31.charter.net (InterMail vM.7.09.02.04 201-2219-117-106-20090629) with ESMTP id <20110501122931.UCDY7341.mta31.charter.net@imp09> for ; Sun, 1 May 2011 08:29:31 -0400 Received: from OfficeGateway ([97.93.194.249]) by imp09 with smtp.charter.net id eCVX1g00K5PKNQZ05CVX8x; Sun, 01 May 2011 08:29:31 -0400 X-Authority-Analysis: v=1.1 cv=zUqQ2eogioz8lh+3uqjRe4Y1MWSUJU+U3b3PFzAwX18= c=1 sm=1 a=yUnIBFQkZM0A:10 a=4m9KTjnTdOqbBMZ6vWl+tA==:17 a=e4cuZbTcFlNlq5yxDRUA:9 a=CjuIK1q_8ugA:10 a=yMhMjlubAAAA:8 a=SSmOFEACAAAA:8 a=YmyAbr2f1nZD5lkKF_4A:9 a=4m9KTjnTdOqbBMZ6vWl+tA==:117 From: "L Henney" X-Original-To: Subject: Legacy Engine Out info. X-Original-Date: Sun, 1 May 2011 07:29:17 -0500 X-Original-Message-ID: <002701cc07fb$63a9a630$2afcf290$@charter.net> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0028_01CC07D1.7AD48890" X-Mailer: Microsoft Outlook 14.0 Thread-Index: AcwH+0QbhBO6KqxhQ0u7nhEaqwRSUw== Content-Language: en-us This is a multipart message in MIME format. ------=_NextPart_000_0028_01CC07D1.7AD48890 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit Hi Gents, I am working on a Legacy transition syllabus for a friend. We are looking for engine out data to help with the simulations for training. Specifically I would appreciate Rate of Descent data for the following situations. 1) Engine out prop feathered (prop pulled with oil remaining) Rate of Descent at 135 kts. 2) Engine out Prop not feathered (loss of all oil) Rate of Descent at 135 kts 3) Simulation of #1 above? Idle engine partial flaps speedbrakes out, etc? What do you use? 4) Simulation of #2 above ? And for what it's worth, I use 800 and 1500 fpm on the 360 at 100 kts for items 1 and 2. Engine idle requiring 10 and 20 flaps respectively. Finally, Does a Emergency Landing Pattern of 3000 Ft agl work well at 135 kts. Ie. High Key 3K, Low Key 1500 AGL? We would greatly appreciate the inputs of those Legacy experts who have gone before us in this area. Thanks, Larry Henney ------=_NextPart_000_0028_01CC07D1.7AD48890 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Hi = Gents,

 

I am working on a Legacy transition syllabus for a = friend.  We are looking for engine out data to help with the = simulations for training.  Specifically I would appreciate Rate of = Descent data for the following situations.

 

1)      =  Engine out prop feathered (prop pulled = with oil remaining)  Rate of Descent at 135 kts.

2)      = Engine out Prop not feathered (loss of all = oil)  Rate of Descent at 135 kts

3)      = Simulation of #1 above?  Idle engine = partial flaps speedbrakes out, etc?  What do you = use?

4)      = Simulation of #2 above ?

 

And for what = it’s worth, I use 800 and 1500 fpm on the 360 at 100 kts for items = 1 and 2.  Engine idle requiring 10 and 20 flaps = respectively.

 

Finally, Does a  Emergency Landing Pattern of = 3000 Ft agl work well at 135 kts.  Ie. High Key 3K, Low Key 1500 = AGL? 

 

We would greatly appreciate the inputs of those Legacy = experts who have gone before us in this area.

 

Thanks,

 

Larry = Henney

 

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