Service difficulty report · Access Door · Bell 212

Difficulty date
April 27, 2004
Submitted
June 4, 2004
Operation
General aviation
Make and model
Bell 212
Aircraft time
10,961 hours
Engine
Pwa PT6T3
Part
Access Door
Part number
212060822001
Condition
Cracked
Location
Cowl
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 THE DAILY INSPECTION THE COWL INSPECTION DOOR HINGE WAS FOUND LOOSE ALLOWING THE DOOR TO HANG DOWN. UPON REMOVAL OF THE COWLING IT WAS FOUND THAT THE ATTACH FLANGE FOR THE COWL ACCESS DOOR HINGE WAS CRACKED ACROSS 75 PERCENT OF THE FLANGE LENGTH. THE DOOR WAS REMOVED AND THE FLANGE REPAIRED. IF THE CRACK HAD EVENTUALLY CROSSED THE FLANGE THE DOOR COULD HAVE FALLEN UPON THE MAIN DRIVESHAFT SHAFT, WHICH ROTATES AT 6600 RPM DURING FLIGHT. THERE WAS POTENTIAL FOR SERIOUS DAMAGE.

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