SDR AU981036

Service difficulty report · Blade · Hughes 269C

Difficulty date
July 24, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Hughes 269C
Engine
Lyc HIO360D1A
Part
Blade
Part number
269A603523
Condition
Delaminated
Location
Tail Rotor
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) TAIL ROTOR BLADE LEADING EDGE ABRASION STRIP DEBONDED. AREA OF DELAMINATION APPROXIMATELY 50.8MM BY 25.4MM (2 INCHES BY 1 INCH). PART TC: 2,267.

More about the Hughes 269C