Service difficulty report · Reinforcement · Snias AS350B3

Difficulty date
June 24, 2019
Submitted
June 25, 2019
Operation
General aviation
Aircraft
N267A
Make and model
Snias AS350B3
Aircraft serial
7222
Aircraft time
4,798 hours, 4,532 cycles
Engine
Tmeca ARRIEL2B1
Engine time
1,298 hours, 1,568 cycles
Part
Reinforcement
Part number
704A34415250
Condition
Debonded
Location
Engine
Part time
4,798 hours, 1,568 cycles
Component
Bypass Valve · Tmeca
Component part number
0292950780
Stage of operation
IN
How discovered
O
Nature of condition
C
Precautionary procedure
K

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

What was found

AIRCRAFT WAS IN THE PROCESS OF UNDERGOING A CUSTOMER CONFORMITY INSPECTION WHEN A PIECE OF FOD WAS NOTICED IN THE ENGINE BYPASS VALVE OVERBOARD DUCTING. THE DUCT WAS REMOVED AND THE FOREIGN OBJECT WAS IDENTIFIED AS A PART OF THE DUCT REINFORCEMENT THAT HAD BECOME DISBANDED FROM THE PARENT PART. IT WAS DISCOVERED THAT THE REINFORCEMENT PIECE WAS BONDED WITH A CLEAR SILICONE. THIS IS A HIGH HEAT DUCT MATERIAL WHICH IS RED IN COLOR, THE SILICONE BEING CLEAR IS NOT FOR USE IN HIGH HEAT APPLICATION. UPON FURTHER INSPECTION OF THE PART, THERE WERE MULTIPLE AREAS WHERE THIS REINFORCEMENT WERE DISBONDING. I WOULD SUGGEST A DIFFERENT METHOD OF BONDING THIS REINFORCEMENT WITH THE USE OF A SUBSTANCE MORE OIL AND HEAT TOLERANT.