Epstein Files Search

EFTA00794724Set 9

2018-11-1546p16,210w

Apvd: Discrepancy: WHILE C/W CMP 571005 WING EXTERIOR (LEFT) INSPECTION FOUND WING TO FLAP SEAL BETWEEN INBOARD AND SECOND FLAP TRACK ON WING TRAILING EDGE TO BE TORN Resolution: CLEANED ... AFFECTED AREA OF LEFT WING FLAP SEAL BETWEEN INBOARD AND SECOND FLAP TRACK ON WING TRAILING EDGE. APPLIED SEALANT TO AFFEC TED AREA AND ALLOWED TO CURE. NO FURTHER ACTION ... Discrepancy: WHILE COMPLYING WITH CMP 571005 WING EXTERIOR (LEFT) - INSPECTION FOUND L/H C TRACK FLAP TROUGH ROLLER TO BE CORRODED. Resolution: REMOVED CORRODED ROLLER ASSY BEARING, PIN AND BUSHING

https://www.justice.gov/epstein/files/DataSet%209/EFTA00794724.pdf

EFTA00794770Set 9

2018-10-0140p13,662w

Apvd: Discrepancy: WHILE C/W CMP 571005 WING EXTERIOR (LEFT) INSPECTION FOUND WING TO FLAP SEAL BETWEEN INBOARD AND SECOND FLAP TRACK ON WING TRAILING EDGE TO BE TORN Resolution: CLEANED ... AFFECTED AREA OF LEFT WING FLAP SEAL BETWEEN INBOARD AND SECOND FLAP TRACK ON WING TRAILING EDGE. APPLIED SEALANT TO AFFEC TED AREA AND ALLOWED TO CURE. NO FURTHER ACTION ... Discrepancy: WHILE COMPLYING WITH CMP 571005 WING EXTERIOR (LEFT) - INSPECTION FOUND L/H C TRACK FLAP TROUGH ROLLER TO BE CORRODED. Resolution: REMOVED CORRODED ROLLER ASSY BEARING, PIN AND BUSHING

https://www.justice.gov/epstein/files/DataSet%209/EFTA00794770.pdf

EFTA00798623Set 9

2016-12-12126p40,656w

12/1212016 03/27/2017 03/27/2017 Description: 27 170-01-01: LUBRICATE THE LEFT WING TRAILING EDGE FLAP ACTUATION MECHANISM. 80-2-Maintenance 1999M.1B.80-2 5094039 12/1212016 03/27/2017 03/27/2017 Description: 27170-02-01: LUBRICATE ... RIGHT WING TRAILING EDGE FLAP ACTUATION MECHANISM. 80-3-Maintenance 1999M.1B.80-3 5094040 12/1212016 01/12/2018 01/16/2018 Description: 28115-0-01: FUNCTIONALLY CHECK THE CENTER TANK BOOST PUMP AUTO SHUTOFF SYSTEM. NOTE ... Opened RTS Closed Task Card: 18.80-2.NR-1 Drawing: N/A 04/05/2017 01/10/2018 Description: RT VB FLAP OfB FLAP FAIRING SEAL IS TORN. 80-23-Maintenance 1999M.18.80-2.NR-1.80-23 5097835 04/05/2017 01/09/2018

https://www.justice.gov/epstein/files/DataSet%209/EFTA00798623.pdf

EFTA00809904Set 9

42p71,955w

LEFT WING TRAILING EDGE FLAPS 4A 0 0 240 DT 0 0 0 0 68.469 10.208 0 0 -327 0 09.10.2015 322302008 05.06.2016 2-27005012A RIGHT WING TRAILING EDGE ... FLAPS 4A 0 0 240 DT 0 0 0 0 68.605 10.289 0 0 -180 0 04.03.2016 322788665 30.10.2016 2-27005031A LEFT WING TRAILING EDGE FLAPS ... RIGHT WING TRAILING EDGE FLAPS - OB 4A 0 0 240 DT 0 0 0 0 68.605 10.289 0 0 -180 0 04.03.2016 322788665 30.10.2016 2-27005051A LEFT WING TRAILING

https://www.justice.gov/epstein/files/DataSet%209/EFTA00809904.pdf

EFTA01117652Set 9

2013-04-1849p14,045w

JEGE, INC. WO #: SC13175 Invoice Number: 7113001424 Discrepancy: 8.8 RII - Squawk from flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: RII - Verified discrepancy. Found all four ... actuators to be out of limits, two bad flap roller bearings and two flap tracks with play in them. REF items ... Removal and installations and work performed. Rigged and ran flaps as required. No defects noted IAW GIV MM 27-06-00. Discrepancy: 8.10 RH - Squawk from flight test

https://www.justice.gov/epstein/files/DataSet%209/EFTA01117652.pdf

EFTA01080493Set 9

2012-03-1598p30,578w

wing wedge panel IAW G-IIB AMM 5140.00. Discrepancy: 8,7 Left wing flap tracts A,B,C, and D have corrosion on roller bearing surfaces. Resolution: Removed corrosion from ... flap track bearing surfaces on tracks A,B,C and D JAW (MB CPCM 20.50.01.Measured tracks A,B,C and D for thickness as required JAW Gulftream drawing SE05811901 ... others check good. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D IAW Gulftream drawing SE05811901.Cleaned and protected tracks and surrounding area

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

EFTA01117701Set 9

2013-04-1835p11,822w

Flat Rate $57.50 Total USD: $57.50 Discrepancy: 8.8 RII - Squawk from flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: RH - Verified discrepancy. Found all four actuators ... limits, two bad flap roller bearings and two flap tracks with play in them. REF items 8.29, 8.30, 8.31, 8.32, 8.34, 8.35, 8.44, 8.45, 15.40, 15.41 for all Removal ... installations and work performed. Rigged and ran flaps as required. No defects noted IAW GIV MM 27-06-00. Billing Method Howl Rate Total Labor USD: Time and Material

https://www.justice.gov/epstein/files/DataSet%209/EFTA01117701.pdf

EFTA01734227Set 10

2012-03-1598p30,604w

wing wedge panel IAW 6-IIB AMM 51-40-00. Discrepancy: 8.7 Left wing flap tracts A,B,C, and D have corrosion on roller hearing surfaces. Resolution: Removed corrosion ... from flap track bearing surfaces on tracks A,B,C and D IAW GLIB CPCM 20-50-01.Measured tracks A,B,C and D for thickness as required IAW Gulftream drawing SE05811901 ... others check good. Performed brush cadmium plating repair to all exposed surfaces of flap tracks A,B,C and D LAW Gulftream drawing SE05811901.Cleaned and protected tracks and surrounding area

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

EFTA01122646Set 9

78p28,263w

cooling doors will remain open while the airplane is on the ground or the flaps are not up. Once flaps are retracted, the associated pack temperature will be automatically regulated ... System Descriptions This fan will operate when the pack is on and the inboard flaps are not fully retracted, or when a pack is on and the airplane ... auto pack trip system, the airplane must be on the ground, the flaps must be out of the up position, the auto pack trip switch must be in the normal

https://www.justice.gov/epstein/files/DataSet%209/EFTA01122646.pdf

EFTA00609734Set 9

2013-04-0157p13,185w

SC13175 Invoice Number: Total USD: $200.60 Discrepancy: 8.8 Squawk front flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: Discrepancy: 8.9 Squawk from flight test - screw needs ... Total USD: $59.00 Discrepancy: 8.10 Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. Resolution: Billing ... work done IAN' GAMPS 2507. Discrepancy: 8.29 While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH outboard flap actuator failed the Ballnut End Play check

https://www.justice.gov/epstein/files/DataSet%209/EFTA00609734.pdf

EFTA01114993Set 9

2013-04-0157p13,147w

SC13175 Invoice Number: Total USD: $200.60 Discrepancy: 8.8 Squawk front flight test - Flaps shudder felt when flaps selected to 39 degrees Resolution: Discrepancy: 8.9 Squawk from flight test - screw needs ... Total USD: $59.00 Discrepancy: 8.10 Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. Resolution: Billing ... work done IAN' GAMPS 2507. Discrepancy: 8.29 While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH outboard flap actuator failed the Ballnut End Play check

https://www.justice.gov/epstein/files/DataSet%209/EFTA01114993.pdf

EFTA01201855Set 9

3p817w

PEDESTAL ESS SWITCHES FLAP EMER FLAP DC CONTROL a HANDLE OI FLAP FOLLOW UP Bus EMER VALVE T SWITCHES CONT • EXT -• C) C FLAP SHUTOFF VALVE A (DEENERGIZEDCLOSED) MANUAL FLAP ... CONT FLAP INFORMATION CONTROL AUXILIARY RELAY PRESSURE COMBINED (OR UTILITY) O PRESSURE O O O O FLAP POSITION FOR TRAINING PURPOSES ONLY TRANSMITTEFt LEGEND - - - MECHANICAL STAB/FLAP INDICATOR STABILIZER INFORMATION FLAP/STAB ... BREAK CIRCUIT IF ACTUAL FLAP LINEAR TRAVEL EXCEEDS APPROX 1/4 INCH. ONE FROM THE OTHER C Figure 27-37. Flap Control System Block Diagram „5. EFTA01201855 FlightSafety GULFSTREAM GIV/G300/6400 MAINTENANCE

https://www.justice.gov/epstein/files/DataSet%209/EFTA01201855.pdf

EFTA00593629Set 9

3p817w

PEDESTAL ESS SWITCHES FLAP EMER FLAP DC CONTROL a HANDLE OI FLAP FOLLOW UP Bus EMER VALVE T SWITCHES CONT • EXT -• C) C FLAP SHUTOFF VALVE A (DEENERGIZEDCLOSED) MANUAL FLAP ... CONT FLAP INFORMATION CONTROL AUXILIARY RELAY PRESSURE COMBINED (OR UTILITY) O PRESSURE O O O O FLAP POSITION FOR TRAINING PURPOSES ONLY TRANSMITTEFt LEGEND - - - MECHANICAL STAB/FLAP INDICATOR STABILIZER INFORMATION FLAP/STAB ... BREAK CIRCUIT IF ACTUAL FLAP LINEAR TRAVEL EXCEEDS APPROX 1/4 INCH. ONE FROM THE OTHER C Figure 27-37. Flap Control System Block Diagram „5. EFTA00593629 FlightSafety GULFSTREAM GIV/G300/6400 MAINTENANCE

https://www.justice.gov/epstein/files/DataSet%209/EFTA00593629.pdf

EFTA01092968Set 9

2013-04-2315p6,110w

safetied (D-ring) 8.8 Open RH - Squawk from flight test - Raps shudder felt when flaps selected to 39 degrees 8.9 Completed Squawk from flight test - screw needs tightening on panel ... panel 8.10 In Progress RH - Squawk from flight test - on the ground the flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. 8.11 Open ... CAMPS 2507. 8.29 In Progress RII - While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH outboard flap actuator failed the Ballnut End Play check. Endplay

https://www.justice.gov/epstein/files/DataSet%209/EFTA01092968.pdf

EFTA01063411Set 9

2016-07-0926p3,975w

WING AILERON BALANCE BAY SEALS OPEN 737.27.056.00.01 STANDBY RUDDER POWER CONTROL UNIT OPEN 737.27.132.00.01 FLAP POWER DRIVE UNIT OPEN 737.27.136.01.01 LEFT WING FLAP SKEW SENSOR MECHANISM LUBRICATION OPEN 737.27.136.02.01 RIGHT ... WING FLAP SKEW SENSOR MECHANISM LUBRICATION OPEN 737.27.138.00.01 LEFT WING FLAP DRIVE TORQUE TUBES OPEN 737.27.138.00.02 RIGHT WING FLAP DRIVE TORQUE TUBES OPEN 737.27.140.01.01 LEFT WING FLAP TRANSMISSION OIL LEVEL ... Task Card Priority Description Signature Stamp 737-27-140-02-01 RIGHT WING FLAP TRANSMISSION OIL LEVEL OPEN 737.27.144.00.01 LEFT WING FLAP TRANSMISSION UNIVERSAL JOINTS OPEN 737.27.144.00.02 RIGHT WING FLAP

https://www.justice.gov/epstein/files/DataSet%209/EFTA01063411.pdf

EFTA01114167Set 9

2013-04-236p2,407w

ASSOC STATUS DISCREPANCY 8.8 Open RII - Squawk from flight test - Raps shudder felt when flaps selected to 39 degrees 8.10 In Progress RII - Squawk from flight test - on the ground ... flaps would intermittenly move from 20 to 39 degrees and 10 to 20 when selected. GAC_WOAssociationspt Page: 2 of 6 Culfstream Proprietary• Printed: 4/23/2013 10:23:17Als EFTA01114168 Gulfstreame ... Progress RH - While T/S the squawk (8.10) for the flaps moving intermittenly found that the LH outboard flap actuator failed the Ballnut End Play check. Endplay is .038in., limit

https://www.justice.gov/epstein/files/DataSet%209/EFTA01114167.pdf

EFTA00804136Set 9

2019-02-2126p9,911w

Cycknd Mfg#: 27-01-00-SE Quote Notes: 18 May 2017 275019 Wing Flap (Left) - Lubrication 9801.3 Not Available 0.50 Airframe MAN 150 Cyclnd 4451 4502 Cyclnd 144 Cycknd ... Quote Notes: 06 Nov 2018 275020 Wing Flap (Right) - Lubrication 9801.3 Not Available 0.50 Airframe MAN 150 Cyc'Lnd 4451 4502 Cyclnd 144 Cycknd Mfg#: 27.06.00 Quote Notes ... Wing Flap Traveling Nut (Left) - Lubrication 9528.6 Not Available 0.50 Airframe MAN 150 Cyclnd 4352 4502 Cyclnd 45 Cycknd Mfg#: 27.0600 Quote Notes: 18 May2017 275024 Wing Flap Traveling

https://www.justice.gov/epstein/files/DataSet%209/EFTA00804136.pdf

EFTA00811205Set 9

2017-12-1263p23,789w

Plan D, LLC. WO Si: SC521661 Invoice Number: 5517132452 Discrepancy: 8.6 CMP G550 275019 Flap Actuator Travel Nut (Left)- Lubrication Resolution: COMPLIED WITH CMP G550 275019 Flap Actuator navel ... Total Labor USD: Flat Rate $146.00 Total USD: 5146.00 Discrepancy: 8.7 CMP GSM 275020 Flap Actuator Travel Nut (Right) - Lubrication Resolution: COMPLIED WITH CMP 6550 275020 Flap Actuator navel ... 1159CS3450558-00I PLUG, HORIZONTAL STABILIZER 2 5378.18 $75636 HOISTING STOP Discrepancy: 813 L/H Flap "B" Track Aft I/B Roller is worn beyond limits per G550

https://www.justice.gov/epstein/files/DataSet%209/EFTA00811205.pdf

EFTA00811141Set 9

2017-12-1264p23,904w

dated August 31105. Discrepancy: 8.6 CMP G550 275019 Flap Actuator Travel Nut (Left) - Lubrication Resolution: COMPLIED WITH CMP G550 275019 Flap Actuator Travel Nut (Lea)- Lubrication Billing Method Hours Rate ... fowl Labor USD: Flat Rate 5146.00 Total USD: 5146.00 Discrepancy: 8.7 CMP 6550 275020 Flap Actuator Travel Nut (Right) - Lubrication Resolution: COMPLIED WITH CMP 6550 275020 Flap Actuator Travel ... Bill To: Plan D, LLC. WO At: SC521661 Invoice Number: 5517132452 Discrepancy: 8.23 L/II Flap "B" Track Aft I/B Roller is worn beyond limits

https://www.justice.gov/epstein/files/DataSet%209/EFTA00811141.pdf

EFTA01055655Set 9

2017-01-282p379w

From: Lany Visoski To: "Jeffrey E." <jeevacation@gmail.com> Subject: Re: IV flap Date: Sat, 28 Jan 2017 14:14:05 +0000 Yes,. I could takeoff and land Flaps ... think that's my problem, if I get the flaps moving I think everything will work normal it's when I select flaps zero to flaps 10 is when ... nonmovement comes into play, I'll check performance for runway length required for Flaps 20 landing„ Since flaps appeared locked out or would not extend from zero to flaps

https://www.justice.gov/epstein/files/DataSet%209/EFTA01055655.pdf