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Date: Sun, 3 Jan 2010 08:48:22 -0500
Message-ID: <1ab24f411001030548m4a515f79o29274c826d4b5332@mail.gmail.com>
Subject: Now Lycoming (again)
From: Lynn Hanover <lehanover@gmail.com>
To: flyrotary@lancaironline.net
Content-Type: multipart/alternative; boundary=00032555accac8526d047c42db79

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The FAA is superseding an existing airworthiness directive (AD) for Lycoming
Engines (formerly Textron Lycoming) models 320, 360, and 540 series,
"Parallel Valve" reciprocating engines, with certain Engine Components, Inc.
(ECi) cylinder assemblies, part number (P/N) AEL65102 series "Titan,"
installed. That AD currently requires initial and repetitive visual
inspections and compression tests to detect cracks at the head-to-barrel
interface, replacement of cylinder assemblies found cracked, and replacement
of certain cylinder assemblies at new, reduced times-in-service. This AD
requires the same actions, but for an expanded population of cylinder
assemblies. This AD results from reports of 10 additional cylinder head
separations since issuing AD 2008-19-05, on cylinder serial numbers not
listed in that AD. We are issuing this AD to prevent loss of engine power
due to cracks at the head-to-barrel interface and possible engine failure
caused by separation of a cylinder head, which could result in loss of
control of the aircraft.

From ANN

You hang in there sunshine, I think yours will make 2000 hours.

Or, Flyrotary...................no cylinder head...........


Lynn E. Hanover

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<div>The FAA is superseding an existing airworthiness directive (AD) for Ly=
coming Engines (formerly Textron Lycoming) models 320, 360, and 540 series,=
 &quot;Parallel Valve&quot; reciprocating engines, with certain Engine Comp=
onents, Inc. (ECi) cylinder assemblies, part number (P/N) AEL65102 series &=
quot;Titan,&quot; installed. That AD currently requires initial and repetit=
ive visual inspections and compression tests to detect cracks at the head-t=
o-barrel interface, replacement of cylinder assemblies found cracked, and r=
eplacement of certain cylinder assemblies at new, reduced times-in-service.=
 This AD requires the same actions, but for an expanded population of cylin=
der assemblies. This AD results from reports of 10 additional cylinder head=
 separations since issuing AD 2008-19-05, on cylinder serial numbers not li=
sted in that AD. We are issuing this AD to prevent loss of engine power due=
 to cracks at the head-to-barrel interface and possible engine failure caus=
ed by separation of a cylinder head, which could result in loss of control =
of the aircraft.</div>

<div>=A0</div>
<div>From ANN</div>
<div>=A0</div>
<div>You hang in there sunshine, I think yours will make 2000 hours.</div>
<div>=A0</div>
<div>Or, Flyrotary...................no cylinder head...........</div>
<div>=A0</div>
<div>=A0</div>
<div>Lynn E. Hanover</div>

--00032555accac8526d047c42db79--