# SDR DALA2019071204194

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 12, 2019
- Submitted: July 15, 2019
- Operation: Air carrier
- Aircraft: [N341NB](https://openairdocs.org/aircraft/N341NB), registered now
- Make and model: Airbus A319-114
- Registry model: [Airbus A319-114](https://openairdocs.org/model/airbus-a319-114) (OpenAirDocs)
- Aircraft serial: 1738
- Aircraft time: 46,818 hours, 24,581 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Door Frame
- Condition: Cracked
- Location: Fuselage
- Stage of operation: IN
- How discovered: O
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DALA2019071204194

## Discrepancy

CRACK INDICATION ON FRAME 68 IN OPEN LOWER INBOARD HOLE AT DOOR STOP FITTING 1 POSITION RT SIDE CRACK DIRECTION: 12 O'CLOCK AT AFT GALLEY AREA (1 EA) (D1-D2= 0.076 INCHES (1.93MM))AA 5311-01216 AD RELATED ACTION REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED WEB SURFACE FRAME 68 DOOR STOP FITTING 1 POSITION RT AS PER SRM 53-41-12-300-011 THIS REPAIR IS CLASSIFIED CATEGORY "B" AND MUST BE INSPECTED. INSPECTION THERSHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 15600 FC/31,200 FH WICHEVER ACHIEVE FIRST AND SUBSEQUENT INSPECTION AT INTERVARLS OF 4,800 FC/9600 FH INSP ACTION METHOD HFEC AS PER SRI 53-41-12-301 TASK 53-12-205-010 TABLE 04 AND FIGURE 02.

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