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[rebel-builders] ATTENTION Murphy Elite Operators: Inspectio

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Ken

[rebel-builders] ATTENTION Murphy Elite Operators: Inspection Update 1 For

Post by Ken » Sun Feb 19, 2012 6:32 pm

Interesting observation. On engine bolts I've noticed that it is not
difficult to tighten AN bolts and washers enough to permanently deform
the aluminum under the washer. Work hardening the aluminum under the
washer like that could create a crack sensitive area I think. On
critical engine fasteners I go to the trouble of finding hardened
washers to prevent this sort of thing.

Based on history I'd be very surprised if MAM puts out any bulletins on
this unless there are multiple reports of similar problems.

Ken

Alan Hepburn wrote:
It's kind of interesting that the cracks seem to lead to the edge of the
washers, rather than to the bolt holes themselves. I assume the cracks in
the filler and those in the spar are unrelated. The cracks in the filler
were bound to happen sooner or later. In fact, use of filler like this is
not standard practice. Getting back to the spar cracks, you have to wonder
if the elevator hinge was subjected to some unusual downward force at some
point in its career.

Al

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com] On Behalf Of John &
Lee
Sent: Saturday, September 04, 2010 11:24 PM
To: rebel-builders@dcsol.com
Cc: murtech; kits@pattersonaerosales.com
Subject: [rebel-builders] ATTENTION Murphy Elite Operators: Inspection
Update 1 For Cracks Found In Horizontal Stab

Service Difficulty Report:

Date: 21 August 2010
Model: Murphy Elite
Serial #: 549
Built: 2004
TTSN: 273 Hours
Damage History: None, all time on wheels (tail dragger) except last 33 hours
on Murphy 1800 amphibs (installed end of June 2010).

Findings:

Further to my initial report, I have removed the horizontal stabilizer,
elevator and outboard hinges and conducted further inspections with the
assistance of an AME. I have posted new photographs of these inspections at
http://www.dcsol.com/murphy-rebel/ under Files>Elite>301 E-Horizontal
Stab.

The hairline fractures in the horizontal stabilizer rear spar extend almost
the complete width of the right hinge (underneath it), and about 1/3 of the
width of the left hinge. Interior examination (through access panel)
disclosed hairline fractures at the corner of both tip ribs. The parts were
inspected in the as-found condition, and then after cleaning.The hairline
fractures were difficult to detect optically, and a magnifying glass and
flashlight were used to aid the exterior and interior inspections.

Murphy Aircraft Mfg Ltd Technical Support and Patterson Aero Sales were
advised of these new findings on 4 Sept and photographs were sent to them.
I am currently waiting for modification/repair parts and instructions from
Murphy Aircraft Mfg. Ltd.

Take Care

John Garstang

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