Service difficulty report · Clamp · Grob G120A

Difficulty date
November 9, 2011
Submitted
January 23, 2013
Operation
General aviation
Make and model
Grob G120A
Engine
Lyc AEIO540D4D5
Part
Clamp
Part number
RSGU11312W5
Condition
Out Of Position
Location
Wire Bundle
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

(CAN) THE UPPER AFT SCREW RETAINING PANEL 120A-2812 WAS FOUND TOUCHING A WIRING BUNDLE LOCATED BEHIND THE CENTER CONSOLE PANEL (120A-2880). REPLACED AND REPOSITIONED THE CLAMP (RSGU 1.13/12-W5-SILICON) WITH CLAMP (RSGU-15/15-W6). THIS ALLOWED THE SCREW TO BE INSTALLED WITHOUT TOUCHING THE WIRING BUNDLE.

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