Service difficulty report · Fitting · Boeing 7377CT

Difficulty date
July 12, 2013
Submitted
September 14, 2015
Operation
General aviation
Make and model
Boeing 7377CT
Aircraft time
20,030 hours
Engine
Ge CFM567B24
Part
Fitting
Part number
113A135Y1
Condition
Sheared
Location
Lt Wing Te Flap
Stage of operation
IN
How discovered
9
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) DURING HEAVY MAINTENANCE, WASHER WAS FOUND CRACKED ON LT OTBD FLAP FITTING. IT WAS NOTED DURING WASHER REPLACEMENT IAW 27-51-23 THAT THE REMOVAL OF THE NUT WAS ABNORMALLY HIGH. DURING A WALK AROUND AFTER THE AIRPLANE HAD BEEN REPAINTED THE LT FITTING STUD WAS FOUND SHEARED. THE FITTING WAS REPLACED AND THE ACFT RETURNED TO SERVICE. FAILURE OF THE STUD IS BELIEVED TO BE CAUSED BY THE ABNORMALLY HIGH BREAKING TORQUE ON THE ASSOCIATED NUT.

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