EFTA01186862Set 9
2014-05-2968p16,750w
Discrepancy: 4.9. Comply with CMP code(s) 236010 / 236011: Static Discharger Wick Resistance (Left and Right) - Functional Test
Resolution: Complied with CMP card 236010, left wing static discharger wick resistance ... functional check per NOM 23-05-00 and CMP
card 236011, right wing static discharger wick resistance-functional check per Mal 23-05-00.
04/2512014 RC
Labor:
Labor Billing Type ... Discrepancy: 4.10. Comply with CMP code(s) 236014 : Left horizontal stabilizer static discharger wick resistance check
Resolution: Complied with CMP card 236014, left horizontal stabilizer static discharger wick resistance-functional
https://www.justice.gov/epstein/files/DataSet%209/EFTA01186862.pdf
EFTA01122767Set 9
2011-03-246p1,612w
PRELIMINARY
*LABOR*
CUSTOMER LABOR: 855.61
ITEM 4 TOTAL AMOUNT: 3,641.81 :*
5 Static ports on LH and RH plugged.: Gained access to static tees and
disconnected at station ... GIIB acft. Purged
pilots, copilots and stby. Found some debris. However alternate
static was completely clogged. Even with 20 psig per acft MM (GIIB
34-01-00) no movement ... flow. Troubleshot to alternate
static line on RH side of acft to static port. After several times,
finally able to get debris in RH alternate static to loosen evidence
https://www.justice.gov/epstein/files/DataSet%209/EFTA01122767.pdf
EFTA00798399Set 9
1994-10-026p1,790w
EVIDENCE SUBMITTED
Test Agency Test Identifier Test Name/Report Date
Redland Technologies 7161-03 Static Uplift Testing Dec. 1991
Appendix III PA 102 & PA 102(A)
The Center for Applied Engineering ... Static Uplift Testing May 1994
Inc. PA 101 (Mortar Set)
The Center for Applied Engineering, 94-060A Static Uplift Testing March, 1994
Inc. PA 101 (Adhesive Set)
The Center ... Applied Engineering, 25-7094-2 Static Uplift Testing PA 102 Oct. 1994
Inc. (4" Headlap, Nails, Direct Deck, New
Construction)
The Center for Applied Engineering, 25-7094-8 Static Uplift
https://www.justice.gov/epstein/files/DataSet%209/EFTA00798399.pdf
EFTA02412011Set 11
2010-11-2360p15,075w
TOTAL AMOUNT: . 00 **
38 Comply with CMP Code 234555 wick, check L wing static (G-IIR).:
Complied with CMP Code ... TOTAL AMOUNT: .00 **
39 Comply with CMP Code 234560 wick, check R wing static (G-IIB).:
Complied with CMP Code ... TOTAL AMOUNT: .00 **
40 Comply with CMP Code 234565 wick, ck L h/stab static (G-TTB).:
Complied with CMP 234565 IAW CMP 234565 and GAC MM 23-05-00.
*LAB0R
https://www.justice.gov/epstein/files/DataSet%2011/EFTA02412011.pdf
EFTA01122622Set 9
24p7,830w
DADC), which are devices used in many systems in this
aircraft, take pitot and static information from pilot or copilot systems and converts it, with
corrections, into static, airspeed ... various components
which require this information. One of the DADC outputs is a corrected static signal which is
fed into the pressurization transducer for static reference. The transducer receives ... function. There is one tubing connection to this valve which is attached to a
static port located in the skin just above valve. Other than the above connection, unit
https://www.justice.gov/epstein/files/DataSet%209/EFTA01122622.pdf