SDR CA020628004

Service difficulty report · Blade · Airbus A310300

Difficulty date: August 5, 2001
Submitted: July 8, 2002
Operation: Air carrier
Make and model: Airbus A310300
Aircraft time: 36,575 hours
Engine: Ge CF680C2A5
System (JASC): 7200 · Engine (Turbine/Turboprop)
Part: Blade
Condition: Damaged
Location: Compressor
Stage of operation: TO
How discovered: O
Nature of condition: C, J
Precautionary procedure: C

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN) COMPRESSOR STALL ON TAKE OFF IN LRM, ON ENGINE NR 2 , MTCE FOUND AFTER VISUAL INSPECTION, 2 BLADES DAMAGED. FURTHER INSPECTION C/OUT IN ACCORDANCE WITH AMM 72-00-00 P.600, REVEALED DAMAGE ON HIGH PRESSURE COMPRESSOR. NUMEROUS BLADES NICKED, CURLED, TORN OR PARTIALLY MISSING. DAMAGE NOT WITHIN LIMITS I.A.W. AMM 72-31-00 P.602. MAINTENANCE REPLACED THE ENGINE I.A.W. AMM 71-00-00.

More about the Airbus A310-300