Service difficulty report · Boot · Bell 212

Difficulty date
July 31, 2015
Submitted
April 22, 2016
Operation
General aviation
Make and model
Bell 212
Aircraft time
6,615 hours
Engine
Pwa PT6T3B
Part
Boot
Part number
212040176101
Condition
Torn
Location
M/R Drive Shaft
Part time
1 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) THIS DRIVE SHAFT WAS INSTALLED AS A REPLACEMENT FOR THE PREVIOUS DRIVE SHAFT THAT HAD A LEAKING BOOT. THERE WAS NO GREASE LEAKAGE AFTER THE MANDATORY GROUND RUN LEAK CHECK. THE ACFT HAD A 1.2 HR FERRY FLIGHT AND ON A POST FLIGHT INSPECTION THE ENGINEER NOTICED THE GREASE LEAKAGE, OVER HALF THE GREASE HAD LEAKED OUT. THE YELLOW TEMP INDICATORS HAD TURN BLACK AND FALLEN OFF. THE RED INDICATORS HAD 2 OF THE 4 DOTS TURN BLACK. WHEN STILL INSTALLED THE BOOT LOOKED LIKE IT HAD 2 SMALL TEARS BUT AFTER A DETAILED INSPECTION ON REMOVAL THE BOOT HAD TORN HALFWAY AROUND. ON FURTHER INSPECTION IT WAS NOTED THAT THE COVER PLATE HAD A RUBBER WARE MARK THAT DID NOT COMPLETELY GO AROUND THE ENTIRE INNER CIRCUMFERENCE LIKE MOST INSTALLATIONS. THE AREA WITH NO RUBBER WARE MARK LINED UP WITH THE TEAR. THIS BOOT WAS BRAND NEW WITH A MFG DATE OF FEB 26 2014.

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