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SDR WGEA200800048

Open the Markdown

Service difficulty report · Flap System · Eclips ECLIPSEEA500

FAA SDR system

Difficulty date
March 13, 2008
Submitted
March 24, 2008
Operation
Air carrier
Aircraft
N142DJ
Make and model
Eclips ECLIPSEEA500
Aircraft serial
000056
Aircraft time
82 hours, 109 cycles
System (JASC)
2750 · Trailing Edge Flap Control System
Part
Flap System
Condition
Out Of Adjust
Location
Te Flaps
Stage of operation
CR
How discovered
O
Nature of condition
F, J
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

AIRCRAFT REQUIRES 12 PERCENT LWD WITH 7 PERCENT RUDDER AT 160 KTS, 88 PERCENT LWD WITH 0 PERCENT RUDDER AT 160 KTS. REFERENCE DAYJET WORK ORDER 1600, NR-00001. TEMPORARILY INSTALLED 2 EACH GURNEY TABS ON THE RT WING FLAP IAW SEM 500-0096 REVISION B DATED 3/20/2008. UPON COMPLETION OF TEST FLIGHT, IF PROBLEM IS CORRECTED, RETURN AIRCRAFT TO GNV SERVICE CENTER FOR PERMANENT ATTACHMENT OF GURNEY TABS IAW SEM 500-0096 REVISION B DATED MARCH 20, 2008. REFERENCE LOGBOOK PAGE 0902, ITEM 1. EVALUATION FLT COMPLETED, DATA FORWARDED TO MAINTENANCE ENGINEERING FOR REVIEW. REFERENCE WORK ORDER 1676, NR-00001. INSTALLED 2 GURNEY TABS ON RIGHT OUTBOARD FLAP TRAILING EDGE IAW SEM 500-0096 REVISION B.