# SDR CALA2014082192002

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 20, 2014
- Submitted: August 21, 2014
- Operation: Air carrier
- Aircraft: [N855UA](https://openairdocs.org/aircraft/N855UA), registered now
- Make and model: Airbus A319-131
- Registry model: [Airbus A319-131](https://openairdocs.org/model/airbus-industrie-a319-131) (OpenAirDocs)
- Aircraft serial: 1737
- Aircraft time: 41,770 hours, 17,218 cycles
- Engine: Iae V2522A5
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Dented
- 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/CALA2014082192002

## Discrepancy

DENT REPORTED BY FLIGHT CREW & CATERING AFT OF DOOR 2L.  FUSELAGE DENTED BETWEEN FRAME 69 & 70 AT STRINGER 21.  DENT ABOVE STRINGER IS .040 INCHES DEEP, .23 INCHES FROM NEAREST RIVET ROW, 2.66 INCHES  X 1.24 TOTAL AREA.  DENT BELOW STRINGER IS 3 X 1.25, .010 INCHES DEEP.  STRINGER ALSO APPEARS TO BE DENTED IN APPROX 020 INCHES.  CHECK SRM 53-00-11 FIG 04, PG 223 FOR POSSIBLE REPAIR SCHEME.  DAMAGE WITHIN LIMITS IAW SRM 53-41-11 PG 111.  ACCOMPLISHED HFEC IAW SEQ 1422001.  NO DEFECTS FOUND.  DAMAGE AREA IS 2.5 INCHES WIDE, 3.5 INCHES HIGH & .064 INCHES DEEP.

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