📄 Extracted Text (272 words)
From: Larry Visoski
Sent: Wednesday, February 1, 2017 3:50 AM
To: Je vacation
Subject: Fwd: 550 engines
Pete informs it appears Chevron's clea=ing service applies the sealant to the Cowl , doesn't seem like a big deal l=will
gather more information / facts tomorrow from Kathleen and Gulfstream a=out this Cowl lip issue
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Begin forw=rded message:
From: Pete=Rawson
D=te: January 31, 2017 at 9:15:57 PM EST
To: Larry Visoski
Subject:
<=iv>l saw that too on the due list-
Code=920004/05 RR NTO 116 Xzilon application cowl inlet lip.
For some reason this airplane has a Cowl I=p issue every 90 days they have to apply this compound do you know
what thi= is? See below
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Begin forwarded mes=age:
From: Larry Visoski
Date: J=nuary 31, 2017 at 6:56:14 PM EST
To: Kathleen Goncalves
Subject: 550 engines
Hi Kathleen
Serial 5173
Chevron N401H=
Pls keep private,. It's on RRCC
<=iv id="AppleMailSignature">
We ar= interested in buying a G550
But t=e aircraft we are looking at has this issue can you explain what this is to=me in layman's
terms? Is there a part shortage?
EFTA_R1_01371351
EFTA02370162
=font color="#000000">. 09/03/08 @353.7 hrs GLF-LGB removed corrosion from L/H
&=mp; R/H Engine Inlet Cowl Lip Skins, performed NDT & re-applied Zzilon3=IAW Rolls-Royce Technical Variance TV
11807R, Rolls-Royce Service Bulletin B=700.7-710A1-10, and FAA A2-20, C4.11 Gulfstream (GAC) NTO (No Technical
Obj=ction) No.:116. The NDT report for both Engines revealed that the rem=ining material thickness was above the N's
minimum acceptable thickness of=.053"
To terminate any ongoing Technical Variance you must change th= lip skins
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</=iv>
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EFTA_R1_01371352
EFTA02370163
ℹ️ Document Details
SHA-256
dfb3ab5d4e807007ea7036a96ecf0323d78ed080b824957260c854ac486c982d
Bates Number
EFTA02370162
Dataset
DataSet-11
Document Type
document
Pages
2
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