# SDR NOCA06111

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 10, 2011
- Submitted: June 15, 2011
- Operation: Air carrier
- Aircraft: [N768NA](https://openairdocs.org/aircraft/N768NA), registered now
- Make and model: Boeing 767-36N
- Registry model: [Boeing 767-36N](https://openairdocs.org/model/boeing-767-36n) (OpenAirDocs)
- Aircraft serial: 29898
- System (JASC): [7830 · Engine Thrust Reverser](https://openairdocs.org/jasc/7830)
- Part: Fitting
- Condition: Damaged
- Location: Thrust Reverser
- 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/NOCA06111

## Discrepancy

DAMAGE FOUND ON NR 2 ENGINE THRUST REVERSER LATCH AREA.  AS PER SRM 54-52-90/101 SHEETS 3 AND 5 FIGURE 3, STA 188.42 HAS A DAMAGED FITTING.  WIDTH  1.75 INCHES, WITH DAMAGED AREA AT .125 WHICH IS LESS THAN 10 PERCENT AS PER SRM DETAIL V AND DEPTH .125 WHICH IS AT 50 PERCENT OF THICKNESS AND IS OUT OF TOLERANCE AS PER SRM SECTION A-A OF DETAIL V.  10 PERCENT OF FLANGE WIDTH IS OK, FLANGE THICKNESS IS OUT OF TOLERANCE.  REPLACED FAN COWL BEAM AS PER SRM 54-52-90 AND DRAWING 311U2510.

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