Service difficulty report · Strut · Cndair CL2156B11215

Difficulty date
August 14, 2015
Submitted
April 22, 2016
Operation
General aviation
Make and model
Cndair CL2156B11215
Engine
Pwa PW123
Part
Strut
Part number
87110016011
Condition
Cracked
Location
Engine Mount
Part time
5,800 hours
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) LAST SUMMER THE SPANISH AIR FORCE HAD AN DISCOVERED A REAR ENGINE MOUNT BROKEN (P/N: 87110016-011) AFTER MULTIPLE PROPELLER BALANCING. AFTER A PROPELLER CHANGE, DYNAMIC BALANCING FLIGHTS BEGAN. - IN SUCCESSIVE BALANCING FLIGHTS THE IPS MEASURED BY THE BALANCING COMPUTER INCREASED FLIGHT AFTER FLIGHT. - THE FOLLOWING MORNING, IN A VISUAL INSPECTION OF THE ENGINE NACELLE AND ENGINE MOUNTS, THE RGB UPPER MOUNT WAS HEAVILY DAMAGED (THE RUBBER ELEMENT) AND ONE REAR ENGINE SIDE MOUNT (THE ONE MENTIONED BEFORE) WAS BROKEN AND THE OTHER ONE WAS BENT. THE SPANISH AIR FORCE THINK THAT THE CHAIN OF FAILURES STARTED WITH A DAMAGED OR AGED UPPER ENGINE MOUNT (WHICH COULD NOT WITHSTAND THE PROPELLER VIBRATION LEVELS), AND THE REAR MOUNT FAILURE MECHANISM WAS FATIGUE. IT IS TO NOTE THAT THIS STRUT HAS TO BE INSPECTED VIA FLUORESCENT LIQUID INSPECTION EVERY 250 HOURS. NO OTHER EVENT HAS EVER BEEN REPORTED ON THE FLEET.