# SDR DALA2019040752271

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 3, 2019
- Submitted: April 7, 2019
- Operation: Air carrier
- Aircraft: [N352NW](https://openairdocs.org/aircraft/N352NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 778
- Aircraft time: 63,688 hours, 29,157 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Beam
- Condition: Cracked
- Location: Frames 35-36
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DALA2019040752271

## Discrepancy

CRACK INDICATION ON FRAME 35 TO FR 36 LH SIDE LOCATED AT LONGITUDINAL BEAM AT HOLE ''A'' PRESSURE FLOOR PANEL ON LOWER FUSELAGE (1 EA) .(CR ACK POSITION AT 9 O'CLOCK. REPAIR IN ACCORDANCE WITH WORK CARD 5311-01 171-04A PRIOR TO FURTHER FLIGHT,"AA 5311-01171","SB A320-53-1264 ", "AD-2018-06-04".) PERFORMED REPAIR ON FR35 TO FR36 4H SIDE LOC. AT LONGITUDINAL BEAM PRESSURE FLOOR PANEL ON LOWER FUSELAGE. HOLE "A". REPAIR WAS ACCOMPLISCHED IN ACCORDANCE WITH WORK CARD 5311-01171-04A, AA5311-01171, SBA320-53-1264: AD-2018-06-04.

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