Service difficulty report · Blade · Bell 205A1

Difficulty date
December 20, 2011
Submitted
September 14, 2015
Operation
General aviation
Make and model
Bell 205A1
Aircraft time
20,451 hours
Engine
Lyc T5317A
Part
Blade
Part number
212015501115
Condition
Cracked
Location
Main Rotor
Part time
3,522 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) 3 CRACKS DEVELOPED ON BOTTOM SIDE OF BLADE SKIN, PN 212-015-501-115, SN A6009 (TSN) 3521.9, 1 CRACK 5.5", THE OTHER 2 CRACKS ARE 2.5" - 3.5" RESPECTIVELY. MEASURING FROM TRIM TAB EDGE INBD 41.5" IS THE LONG, 5.5. THE OTHER 2 CRACKS ARE OTBD A FEW INCHES OF THE LONG 5.5" CRACK. THE CRACKS ARE COMING OUT OF DEEP CORROSION PITS. DYE PEN PIN INSP CARRIED OUT TO CONFIRM DEFECT.

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