Service difficulty report · Blade · Hughes 369D

Difficulty date
July 4, 2002
Submitted
August 7, 2002
Operation
Air carrier
Make and model
Hughes 369D
Aircraft time
8,153 hours
Engine
Allsn 250C20B
Part
Blade
Part number
500P2100101
Condition
Cracked
Location
Main Rotor
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

(CAN) CRACK IN LOWER SKIN DISCOVERED AT STN 36.5. BLADE REMOVED FROM SERVICE. FURTHER ANALYSIS OF THE BLADE REVEALED THAT THE CRACK STARTED AT THE FIRST LIGHTENING HOLE OF THE "C" CHANNEL AND MOVED TO LOWER SKIN. THE CRACK THEN RAN LATERALLY TO THE TE AND TOWARD THE LE. THE "V" CHANNEL AT THE TE HAD CRACKED LONGITUDINALLY FOR APPROX 2 INCHES. FURTHER ANALYSIS REVEALED SURFACE PITS WERE DETECTED ON THE INNER RADIUS OF THE LIGHTENING HOLE. THESE PITS WERE ANODIZED, INDICATING THAT THESE PITS WERE FORMED DURING THE CONSTRUCTION PROCESS.