# SDR UALA2012080704256

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 6, 2012
- Submitted: September 20, 2012
- Operation: Air carrier
- Aircraft: [N465UA](https://openairdocs.org/aircraft/N465UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1341
- Aircraft time: 38,588 hours, 16,495 cycles
- Engine: Iae V2527A5
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Liner
- Condition: Damaged
- Location: Rt Engine
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/UALA2012080704256

## Discrepancy

RIGHT ENGINE HAS A HOLE IN THE ACCOUSTIC LINER AT THE 6 O'CLOCK POSITION.  ATTRITION LINER DAMAGED AT THE 6 O'CLOCK POSITION, 1 INCH HOLE BY 3  INCH DELAMINATION.  RT ENGINE HAS A THREE QUARTER INCH CHUNK OF HONEYCOMB MISSING AT THE 1730 POSIT NEXT TO FAN. OK TO CONTINUE IN SERVICE FOR UP TO 20 CYCLES. -INF-  :LCL MAINT RE-CHECKED THE EXISTING REPAIR AT 6"0 CLK, REPAIR MEASURE APROX 8.0"W X 3.0"AXIALLY, EXISTING REPAIR IS CRACKED APROX 1.0"W X 0.875 AXIALLY. STILL WITHIN LIMITS OF AMM MT78-017.

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