EFTA00621054Set 9
2013-04-2327p9,984w
UNIT
(APU) 36-1501G] INSTALLATION,
1000-1535 HAVING ASC470
12.1 #4 1159SB21515-11 DOUBLER
12.1 #5 AMS3374C TYPES 1& 3 SEALANT KIT, 6 OUNCE FIREWALL
12.1 #6 M.S20615.4M5 RIVET ... maintenance performed IAW GIV AMM 49-10-00.
Step: 12.1.3 Completed Removed existing Doubler P/N 1159SB2I416-75 from APU upper enclosure between BL
1.84 and BL 10.97. Located, fitted ... match drilled and installed new Doubler P/N
1159SB21515-11, and new Doubler P/N 11595B21515.I3. All maintenance performed
IAW Gulfstream Doubler Installation , APU Enclosure Rework Drawing No.
I I59SB21515. Removed existing
https://www.justice.gov/epstein/files/DataSet%209/EFTA00621054.pdf
EFTA00796113Set 9
2018-03-0117p8,620w
Removal of all production and outfitting installed antennas, penetrations of fuselage skin, external skin doublers
(except as noted below) to perform the inspection as well as any required follow ... presented for approval if additional access is deemed to be required.
• External skin doublers, adapter or contour plates that are riveted on the aircraft skin (or other means of permanent
https://www.justice.gov/epstein/files/DataSet%209/EFTA00796113.pdf
EFTA01326217Set 10
2019-06-03607p140,720w
Approvals:
Iridium Antenna Instalati08
FM 8110.3 • CI 490-490 indium Antenna Doubler Design B Inslalabon, Identification No. N120JE-052310-1-ECNOI. Revision N/C. dated
May 23.2019 and Damage Tolerance Analysis ... Gulfstream Cy-IV CI 490-490 Iridium Antenna Doubler Insulation, Repot
No. N120JE-052319-OT01, Revision N/C. dated May 23. 2019. Approved by FM Structures DERT-605818.NAL Trevor J.
Sarong. Instructions
https://www.justice.gov/epstein/files/DataSet%2010/EFTA01326217.pdf
EFTA00011669Set 8
2018-11-30442p72,450w
additional fuselage modification inspections.
2.3 Inspection Method
Inspect fuselage skin in the modification area, doubler fastener holes area, using high frequency eddy current
inspection techniques, according to the intervals outlined ... holes, the inspector should look for cracks on the surface of the
skin and doubler around the fastener holes.
REPORT No. 584-00-0047, Rev: BHE & Associates, Ltd. Page
https://www.justice.gov/epstein/files/DataSet%208/EFTA00011669.pdf
EFTA01326943Set 10
2018-11-30444p80,759w
additional fuselage modification inspections.
2.3 Inspection Method
Inspect fuselage skin in the modification area, doubler fastener holes area, using high frequency eddy current
inspection techniques, according to the intervals outlined ... holes, the inspector should look for cracks on the surface of the
skin and doubler around the fastener holes.
REPORT No. 584-00-0047, Rev: D BHE & Associates, Ltd. Page
https://www.justice.gov/epstein/files/DataSet%2010/EFTA01326943.pdf