EFTA01080493Set 9
2012-03-1598p30,578w
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 ... PRI440-B-1/2 SEALANT, PRC,CARTRIDGE 4 538.28 $153.12
Step: 8.7.1 Completed Removed corrosion front flap track bearing surfaces on tracks A,B,C and D IAW GIIB
CPCM ... CAMPS 4000.
Discrepancy: 8.8 Right wing flap tracts A,B,C, and D have corrosion on roller bearing surfaces.
Resolution: Removed corrosion from flap track bearing surfaces on tracks
https://www.justice.gov/epstein/files/DataSet%209/EFTA01080493.pdf
EFTA01117701Set 9
2013-04-1835p11,822w
pitting horizontal stabilizer skin at panel 3S-I'PR-S.
Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 38-UPR-S, cadmium plat ... Total USD: $1,101.70
Step: 8.21.1 Completed Nlechanicaly removed minor surface corrosion and pitting front panel opening
mounting flange and cadmium plated exposed surface. All work done ... pitting horizontal stabilizer skin at panel 39-UPR-5.
Resolution: Removed minor surface corrosion and pitting from panel opening mounting flange of panel 39-UPR-S, cadmium plated
exposed surface
https://www.justice.gov/epstein/files/DataSet%209/EFTA01117701.pdf
EFTA00011669Set 8
2018-11-30442p72,450w
Cessna
Aircraft Company.
The defects identified by this method are incipient fatigue or corrosion stress cracks in bores,
machining radii, shoulders and countersunk holes, and in the actual skin ... case of fatigue stress cracks, or perpendicular to
internal stresses for stress corrosion cracks. This method also detects minor corrosion-induced surface
damage.
Table 5 Manual List
Document
Aircraft Manual ... glasses. A 10x magnifying glass is recommended
for positive identification of suspected cracks.
6.1.3 Corrosion Treatment
Before attempting a close, visual inspection of any selected part or structural area
https://www.justice.gov/epstein/files/DataSet%208/EFTA00011669.pdf
EFTA00802185Set 9
2018-11-0589p32,816w
Compartment —
Inspection, found L/H MLG Follow Up Door to have multiple spots of surface corrosion
20 that will require further evaluation. 50019421
Est 8 hr
While Complying with ... Compartment —
Inspection, found R/H MLG Follow Up Door to have multiple spots of surface corrosion
31 50019424
that will require further evaluation.
Est 10 firs
While Complying with ... Gear Wheel Well Compartment -
Inspection, found MLG Torque Box surface to show signs of corrosion that will require
48 50019924
further evaluation.
Est 10 hrs
While C/W CMP 571005 Wing
https://www.justice.gov/epstein/files/DataSet%209/EFTA00802185.pdf
EFTA01105727Set 9
2013-02-0113p5,441w
Aeroglaze, buff and polish of leading edge "brite work", and sanding to remove surface corrosion. An
application of Teflon coating is also available to enhance the life of your paint ... Labor $13,000.00
Task:
Perform Engine Runs and Borescopes.
4. Option: Landing Gear Corrosion Inspection (Exhibit 4 Dunlop /Exhibit 5 ABS)
Labor $25,500.00
Task
Landing Gear Corrosion Inspection (Exhibit ... actuals.
AIRFRAME CONTINGENCIES
This proposal does not include correction/clearing of any discrepancies and/or corrosion that may be found, outside services.
additional due items (i.e. customer requirements. completion/outfitter requirements
https://www.justice.gov/epstein/files/DataSet%209/EFTA01105727.pdf
EFTA00597256Set 9
13p5,010w
from damage under surge and transient conditions.
EFTA00597264
of the
J. To guard against corrosion due to extremely harsh environmental conditions, the exterior
compartment/enclosure shall be fabricated from Type 304L ... cables.
PART 4 - SWITCHGEAR STYLE
4.1 Pad-Mounted Style
A. To guard against corrosion due to extremely harsh environmental conditions, the gas-tight tank
shall be made of Type ... EFTA00597266
I I. Non-removable lifting tabs shall be provided.
12. To guard against corrosion due to extremely harsh environmental conditions, the entire
exterior of the enclosure shall be fabricated
https://www.justice.gov/epstein/files/DataSet%209/EFTA00597256.pdf
EFTA00779567Set 9
2010-05-197p1,683w
compatible with all of them.
The engine coolant is designed to transfer heat, stop corrosion, and provide a lubricant
for the water pump seal. Old antifreeze can become acidic ... cooling system actually creates a crude battery. This
condition can cause accelerated corrosion of these materials. Changing the coolant
according to a preventative maintenance schedule will prevent this acidic condition ... engine coolant
help prevent corrosion, and expensive future repairs. (antifreeze)
Advantage:
Replacing the engine coolant as a part of a scheduled maintenance program is essential
to your vehicle's reliability
https://www.justice.gov/epstein/files/DataSet%209/EFTA00779567.pdf
EFTA00718344Set 9
2013-01-293p841w
firm.
I will verify, but to my knowledge the landing gear corrosion is not looked at hard. This is a 5000 landing
requirement but has a calendar due date also ... number, chances are we'll have $250,000+ worth of findings with landing gear corrosion they'll have
to pay if we remove the repair cap. You will ALWAYS have ... axle replacement in landing gear inspection
types, the is ZERO tolerance for corrosion, pitting, scratches or any blemish on axle and barrel of struts,
when you remove them
https://www.justice.gov/epstein/files/DataSet%209/EFTA00718344.pdf
EFTA01084314Set 9
33p3,917w
Cracked I Spoiled Brick Masonry, Stone or Terra Cotta
Thermal expansion and contraction, corrosion of underlying or adjacent
steel, deteriorated joints.
Cracked I Spoiled Stucco
Thermal expansion and contraction, corrosion ... underlying or adjacent steel.
a Cracked I Spoiled Window Sill
Thermal expansion and contraction, corrosion of underlying steel, deteriorated
joints.
a Deflected Steel Lintells)
Corrosion of steel.
a Peeling Paint
https://www.justice.gov/epstein/files/DataSet%209/EFTA01084314.pdf
EFTA02598657Set 11
2014-12-063p518w
18th is what we are shooting for.
Updates:
Below emergency exit window frame corrosion inspection was good, no corrosi=n found.
Completing the software update to DU885's to prevent ... tone during fl=ght. (no charge).
Gear corrosion:
We have shipped "main gear inner race" to Savanah Engineers for e=aluation to make sure the core is
repairable, we will ... flight, all parts we are changing are a necessity.
At this time gear corrosion repair estimate $120k to $150k depending =n core value of parts we are
going to exchange
https://www.justice.gov/epstein/files/DataSet%2011/EFTA02598657.pdf