Service difficulty report · Blade · Bell 205A1

Difficulty date
September 11, 2012
Submitted
September 14, 2015
Operation
General aviation
Make and model
Bell 205A1
Engine
Hnywl T5313BHNYWL
Part
Blade
Part number
204011250001
Condition
Damaged
Location
Main Rotor
Part time
722 hours
Stage of operation
HO
How discovered
O
Nature of condition
E
Precautionary procedure
A

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

What was found

(CAN) MAIN ROTOR BLADE CRACKED FROM L/E TO T/E UPPER AND LOWER SURFACE AT APPROXIMATELY 77" FROM BLADE TIP. ACFT LANDED SAFELY, MAIN ROTOR BLADE INTACT AS 1 PIECE. BLADE WAS REPAIRED IN 2004 APPROXIMATELY 319 HOURS AGO.

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