Service difficulty report · Bolt · Bell 205A1

Difficulty date
July 9, 2002
Submitted
September 6, 2002
Operation
General aviation
Make and model
Bell 205A1
Engine
Lyc T5313A
Part
Bolt
Part number
204011151001
Condition
Cracked
Location
Main Rotor Head
Part time
2,514 cycles
Component
Main Rotor Head · Bell · 205812001
Stage of operation
IN
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 BOLT SUSPECT CRACKED. FOUND DURING FLUORESCENT MAGNETIC PARTICLE INSPECTION.

More about the Bell 205A-1