Service difficulty report · Blade · Bell 212

Difficulty date
August 2, 2001
Submitted
September 5, 2001
Operation
General aviation
Make and model
Bell 212
Engine
Pwa PT6T3B
Part
Blade
Part number
212015501115
Condition
Delaminated
Location
Main Rotor
Stage of operation
CR
How discovered
O
Nature of condition
O
Precautionary procedure
O

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

What was found

(AUS) MAIN ROTOR BLADE SKIN DELAMINATED AT THE BLADE TIP JUST AFT OFTHE D' SPAR. AREA OF DELAMINATION 55MM BY 75MM (2IN BY 3IN).

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