Service difficulty report · Panel · Airbus A319114

Difficulty date
November 9, 2013
Submitted
September 14, 2015
Operation
General aviation
Make and model
Airbus A319114
Aircraft time
52,685 hours
Engine
Cfmint CFM565A5
Part
Panel
Part number
D553700260100
Condition
Cracked
Location
Vertical Stab
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) VERTICAL STABILIZER L/E PANELS, HAS BEEN FOUND WITH SOME CRACKS, FROM WHAT APPEARS TO BE IMPACT AND WATER INGESTION. MFG HAS IDENTIFIED A MANUFACTURING PROCESS AS THE ROOT CAUSE. THE LAY-UP PROCESS CAUSES A NON-UNIFORM PRESSURE DISTRIBUTION AT THE PERIPHERY OF THE HONEYCOMB CORE WHICH RESULTS IN 2 FORMS OF DEFECTS: OUTER SKIN TELEGRAPHING, AND BULGING HOWEVER, THESE 2 DEFECTS DO NOT AFFECT THE PERFORMANCE. OVER THE SERVICE LIFE OF THE ACFT, PAINTING PREPARATION AND SANDING, MAY EXPOSE THE SKIN AND CORE CELLS, MAKING IT SUSCEPTIBLE TO SURFACE BREAKS, CRACKING, AND POSSIBLE WATER PENETRATION IN THE HONEYCOMB CORE. SIL 55-031 HAS BEEN ISSUED, BUT MAY NOT BE ENOUGH FOR ALL CASES. AN SPECIFIC INSPECTION.

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