""Sponson"" — Epstein Files Search

Search Entities About Settings

/to search

Dataset

Sort

Status

DOJ Status

Date Range

–

Page Count

–

17 results for “"Sponson"”

Keyboard Shortcuts

/

Focus search

Esc

Blur input

O

Open PDF

←→

Paginate

EFTA01734227Set 10

2012-03-1598p30,604w

Step: 8.6.1 Completed Disconnected the 5 hydraulic lines to gain access to the sponson access cover 22-SR-2 all lines are capped and or plugged. RLP Step: 8.6.2 Completed ... Removed access cover 22,SR-2 on outboard side of sponson Step: 8.6.3 Completed Removed all spinning and bad rivnuts on the Rill wing wedge panel ... bare metal, and spot primer as required. IAW. SRM.51.13.20. Discrepancy: 8.14 R/H wing upper sponson plate is corroded. Resolution: Mechanically removed corrosion from edges of the RAJ upper sponson plate

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01734227.pdf

EFTA01080493Set 9

2012-03-1598p30,578w

Step: 8.6.1 Completed Disconnected the 5 hydraulic lines to gain access to the sponson access cover 22-SR-2 all lines are capped and or plugged. RLP Step: 8.6.2 Completed ... Removed access cover 22-SR-2 on outboard side of sponson Step: 8.6.3 Completed Removed all spinning and bad donuts on the RAI wing wedge panel ... bare metal, and spot primer as required. IAN'. SRM.51-13-20. Discrepancy: 8.14 R/H wing upper sponson plate is corroded. Resolution: Mechanically removed corrosion from edges of the R/H upper sponson plate

https://www.justice.gov/epstein/files/DataSet%209/EFTA01080493.pdf

EFTA00603223Set 9

2017-01-1922p6,020w

trim material from "L" clip for seal reatiner installation to maintain clearance with Sponson plate lug. Maintain minimum 2 X dia edge distance on rivets. Condition due to production variation ... Completed REQUEST ENGINEERING REVIEW TRIMMING THE LM 1159W40226-13 "I." CLIP FOR CLEARANCE FROM SPONSON RIB AFT LU(. Step: 8.1.15.1 Completed Engineering Disposition: Acceptable to trim material from "I." clip ... seal reatiner installation to maintain clearance with Sponson plate lug. Maintain minimum 2 X dia edge distance on rivets. Condition due to production variation. Touch up 213. 2012 per GAFI4A

https://www.justice.gov/epstein/files/DataSet%209/EFTA00603223.pdf

EFTA01848536Set 10

2012-03-091p244w

15th for a highly important trip. Our main issue is corrosion on the upper Sponson metal plate that the UH gear structure attach point on upper surface of the wing ... thru the weekend to meet our departure date,.if not repair is need to sponson, Gulfstream THINKS we may make the 15th date,. I don't believe, Boeing is ready

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01848536.pdf

EFTA00931158Set 9

2012-03-091p362w

15th for a highly important trip. Our main issue is corrosion on the upper Sponson metal plate that the UH gear structure attach point on upper surface of the wing ... thru the weekend to meet our departure date,.if not repair is need to sponson, Gulfstream THINKS we may make the 15th date,. I don't believe, Boeing is ready

https://www.justice.gov/epstein/files/DataSet%209/EFTA00931158.pdf

EFTA00796113Set 9

2018-03-0117p8,620w

Attach Fitting - Alternative Inspection 275001 Wing Flap / Stabilizer Control - Operational Test 571033 Rib. Wing Sponson (Lett)- Inspection 571034 Rib, Wing Sponson (Right) - Inspection 572001 Wing Wedge (Left) - Inspection 572002 Wing

https://www.justice.gov/epstein/files/DataSet%209/EFTA00796113.pdf

EFTA00589859Set 9

2016-02-0324p11,458w

Estimate 541019 Pylon Internal (Left) - Inspection 541020 Pylon Internal (Right) - Inspection 571033 Rib. Wing Sponson (Left) - Inspection 571034 Rib, Wing Sponson (Right) - Inspection 576005 Aileron Interior (Left) - Inspection 576006 Aileron

https://www.justice.gov/epstein/files/DataSet%209/EFTA00589859.pdf

EFTA00604340Set 9

2003-08-1431p7,818w

Long 970931 27 OPT CM Beach CA. 2603.2 566 11 Nov 2011 C Sponson Rib - Installation applicable to aircraft Airframe serial numbers 5001- SC10683 5302. Aircraft operators who have previously

https://www.justice.gov/epstein/files/DataSet%209/EFTA00604340.pdf

EFTA01035013Set 9

2019-03-255p743w

shape. It will need to be repowered and all electronics replaced. The hull and sponsons(pontoons) are in extremely bad condition. Everything above the water line the entire boat

https://www.justice.gov/epstein/files/DataSet%209/EFTA01035013.pdf

EFTA01850399Set 10

2012-03-131p276w

completed Friday at 4pm. That is the plan at this time. The Sponson corrosion is ok for return to service per Gulfstream engineering. Boeing crew if we take that airplane

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01850399.pdf

EFTA00930965Set 9

2012-03-131p278w

completed Friday at 4pm. That is the plan at this time. The Sponson corrosion is ok for return to service per Gulfstream engineering. Boeing crew if we take that airplane

https://www.justice.gov/epstein/files/DataSet%209/EFTA00930965.pdf

EFTA01523386Set 10

2009-07-011p382w

2todal :abs detnbuCon a shateholdersernces to JPMagen Fonds. Arresten Century Pence cv lunds esUitAlhed sponsoned *dress! a mfn",e0 by Med pares. end Ne J P Magen Conpesnee rrey

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01523386.pdf

EFTA01775100Set 10

2011-09-126p729w

Glove Box: 40=93 Hydro-Turf. Mats: ✓ Extended Rear Platform: ✓ Automatic Bilge System: ✓ Sponsons: ✓ Warranty - 1 Y=ar Limited Engine Specifications <http://www.yamahawaverunners.com/vxde=uxen> Engine Type: 4-cylinder

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01775100.pdf

EFTA01458255Set 10

always be ignored? The purest form of co-investment is often seen as Fundless sponson; intend to put little or no equity into being practiced by institutional investors such

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01458255.pdf

EFTA01849952Set 10

2012-03-131p173w

completed Friday at 4pm. That is the plan at this time. The Sponson corrosion is ok for return to service per Gulfstream engineering. Boeing crew if we take that airplane

https://www.justice.gov/epstein/files/DataSet%2010/EFTA01849952.pdf

EFTA02363214Set 11

2012-03-131p201w

completed Friday at 4pm. That is the plan at this time. The Sponson corrosion is ok for return to service per Gulfstream engineering. Boeing crew if we take that airplane

https://www.justice.gov/epstein/files/DataSet%2011/EFTA02363214.pdf

EFTA00660220Set 9

2012-03-131p175w

completed Friday at 4pm. That is the plan at this time. The Sponson corrosion is ok for return to service per Gulfstream engineering. Boeing crew if we take that airplane

https://www.justice.gov/epstein/files/DataSet%209/EFTA00660220.pdf

Corpus: 1990-03-17 – 2025-12-01

March 2012

Mo

Tu

We

Th

Fr

Sa

Su

None

Light

Medium

Heavy

Results by Dataset17 total

Set 9

9

Set 10

7

Set 11

1