# SDR DALA2016081606037

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 15, 2016
- Submitted: August 17, 2016
- Operation: Air carrier
- Aircraft: [N959AT](https://openairdocs.org/aircraft/N959AT), registered now
- Make and model: Boeing 717-200
- Registry model: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (OpenAirDocs)
- Aircraft serial: 55021
- Aircraft time: 43,956 hours, 30,214 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Cracked
- Location: Fuselage
- 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/DALA2016081606037

## Discrepancy

CRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 RT, CARD 14, ZONE 200.  REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14 AD REV ORIGINAL. LENGTH CRACK 0.150".  REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY.  ADDITIONAL ER/A REV WITH AMOC IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER 24 MONTHS FROM REPAIR ACCOMPLISHMENT.  DAMAGE TOLERANCE ANALYSIS AND A NEW AMOC IS REQUIRED IAW PROCEDURES ESTABLISHED BY ADVISORY CIRCULAR 120-43 UNDER LOG 2634653.  AMOC APPROVAL TO AD 2007-11-13 IS REQUIRED FOR SERVICE BEYOND 60,000 TOTAL FLIGHT CYCLES.

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