Case File
efta-02498063DOJ Data Set 11OtherEFTA02498063
Date
Unknown
Source
DOJ Data Set 11
Reference
efta-02498063
Pages
3
Persons
0
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Extracted Text (OCR)
Text extracted via OCR from the original document. May contain errors from the scanning process.
From:
Larry Visoski
Sent:
Saturday, June 20, 2015 2:19 PM
To:
Je vacation
Subject:
Fwd: Flight Test Recommendations from Dallas Airmotive - Ref G-4 SN 1085
Below is Mike Clune's report from Dall=s AirMotive,.
I will ask Gulfstream regarding your question=about Engine rigging, stall and speed
Thx
Larry
Sent from my iPhone
Begin forwarded=message:
From: "Clune, M=ke"
Date: June 20, 2015 at 8:33:29 AM EDT
To: L=rry Visoski
<=>Cc: "Sasser, Randy" «mailto
>, "Dw er, Everett RRNA
= "Cameron, Alex (RRNA)" «mailto
Subject: Flight Test Reco=mendations from Dallas Airmotive - Ref G-4 SN 1085
Larry,
Thank you for giving me the opportunity to fly with y=u yesterday. The flight gave me a good insight on
the issue tha= you have been dealing with.
During our flight debrief yesterday afternoon, Cherie= Roberts provided some very good
recommendations (see below) from a Gulfstr=am standpoint;
1.
&=bsp; Perform a primary flight control rigging check.&=bsp; This was per the recommendations of
the Gulfstream Flight Test Pilot, R=n Newton.
2.
&=bsp; Open the engine cowlings and check for the positron of the engine thrust strut to insure
they are centered and not touching t=e side of the mounting structure.
EFTA_R1_01623294
EFTA02498063
Gulfstream-Brusinwick should be able to accomplish th=se inspection prior to your trip to Paris. During
the flight to=Paris your principal should be able to detect if there is
A change in the vibration/buffet that he feels. =lf the vibration /buffet is diminished to a satisfactory
condition an= much more important, your principal is happy —we're done.<=:p>
Hover if the vibration /buffet is still there the nex= step is engine related. Per Charles Robert's
recommendation trese actions can be accomplished in your hangar at West Palm Beach;
1.
Remove the fan blades on the left engine a=d re-position the fan blades by 90% to the fan hub.
Since Charles was=seeing a 2'd order low frequency vibration on his test equipment,
this is the norm=l solution for this type of problem.
2.
Once the fan blades have been re-positioned, per=orm a fan balance on both engines to get the
fan / N1 vibration levels to t=e lowest possible condition.
As we discussed t=is will take a fan balance specialist that knows all the tricks. We h=ve field service
personnel there in Florida that has this experience.<=o:p>
Also since the e=gines are on Corporate Care, Rolls-Royce has specialists that can perform t=is function
as well.
3.
During the fan balance process on both eng=nes, we recommend that you do an inlet guide vane
schedule check on both en=ines. This will insure the LP and HP
rotating speeds a=e matched between engines.
Just as a reminder, if we go forward and comply=with the engine recommendations, you will need Rolls-
Royce Corporate Care a=proval.. Please contact your local Rolls-Royce Regional Corporate
Care Manager for assistance.
Larry, have a great flight to Paris and if you need a=ything from Dallas Airmotive, please contact either
Randy Sasser or m=self at anytime.
2
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EFTA02498064
Michael Clune
Director, Technical Services
Office:
Cell: &nbs=;
Fax =nbsp;
900 Nolen Drive= Suite 100 • Grapevine, TX 76051
This e=ail transmission, and any documents, files or previous email messages attac=ed to it may contain
confidential information. If the reader of this messag= is not the intended recipient or the employee or agent
responsible for delivering the message to the intende= recipient, you are hereby notified that any dissemination,
distribution or=copying of this communication is strictly prohibited. If you are not, or be=ieve you may not be, the
intended recipient, please advise the sender immediately by return email or by calli=g +1 214.956.3001. Immediately
take all steps necessary to permanently dele=e the email and all attachments from your computer system.
&nb=p;
&=bsp;
&nb=p;
&=bsp;
&nb=p;
3
EFTA_R1_01623296
EFTA02498065
Technical Artifacts (4)
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Phone
+1 214.956.3001Phone
2498063Phone
2498064Phone
2498065Related Documents (6)
DOJ Data Set 10CorrespondenceUnknown
EFTA Document EFTA02078835
0p
DOJ Data Set 10CorrespondenceUnknown
EFTA Document EFTA02097596
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DOJ Data Set 11OtherUnknown
EFTA02225369
1p
DOJ Data Set 10CorrespondenceUnknown
EFTA Document EFTA01731630
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DOJ Data Set 11OtherUnknown
EFTA02327165
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DOJ Data Set 9OtherUnknown
From: Larry Visoski
1p
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