SDR AU010268

Service difficulty report · Blade · Bell 206L

Difficulty date
March 20, 2001
Submitted
April 4, 2001
Operation
General aviation
Make and model
Bell 206L
Engine
Allsn 250C30
Part
Blade
Part number
206015001117AS
Condition
Corroded
Location
Main Rotor
Part time
862 cycles
Stage of operation
IN
How discovered
V
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

(AUS) MAIN ROTOR BLADE CORRODED IN AREA BETWEEN PAINT AND LEADING EDGESTRIP ON UNDERSIDE OF BLADE. CORROSION DEPTH APPROXIMATELY 1.52MM (0.060IN). FOUND BEFORE FITMENT.

More about the Bell 206L