SDR 2011F00121

Service difficulty report · Blade · Airbus A310300

Difficulty date: March 6, 2010
Submitted: May 27, 2011
Operation: General aviation
Make and model: Airbus A310300
Engine: Ge CF680C2A8
Engine time: 43,619 hours, 13,874 cycles
System (JASC): 7250 · Turbine Section
Part: Blade
Part number: 1538M90P12
Part serial: PCMFFEP4
Condition: Broken
Location: Hpt Stage 1
Part time: 9,195 hours, 3,380 cycles
Stage of operation: IN
How discovered: B
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

HPT STAGE 1 BLADE FOUND BROKEN AND MISSING DURING ROUTINE BSI, ON FOLLOWING CF6-80C2A8 ENGINES SN 659611, 659399, 659526, 659392, 659408, 659612, 659414. SECONDARY DAMAGE WAS ALSO OBSERVED ON NUMBER OF BLADES. ALL THE BLADES WAS NEW WHEN INSTALLED.

More about the Airbus A310-300