# SDR DALA2024021001842

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 8, 2024
- Submitted: February 10, 2024
- Operation: Air carrier
- Aircraft: [N305DN](https://openairdocs.org/aircraft/N305DN), registered now
- Make and model: Airbus A321-213
- Registry model: [Airbus A321-213](https://openairdocs.org/model/airbus-a321-213) (OpenAirDocs)
- Aircraft serial: 7149
- Aircraft time: 21,425 hours, 10,597 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Part number: UNKNOWN
- Condition: Handler Error
- Location: Frms 70-71
- Stage of operation: IN
- How discovered: 9
- Nature of condition: W
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DALA2024021001842

## Discrepancy

AIRCRAFT 3005, DURING BRIDGE CHECK MSP, A TAIL STAND CONTACTED THE AIRCRAFT RESULTING IN GROUND DAMAGE TO THE AIRCRAFT. THIS ERA COVERS AREAS DAMAGE CONSISTS OF A DENTS TO THE FUSELAGE SKIN. IN AREA OF / FR70-FR71, STR 32L-32R. ACCOMPLISH TRIM OUT OF THE CREASE DAMAGE. FOR STRINGERS 33LH AND 34, ACCOMPLISH STRINGER REPAIRS PER A321 SRM 53-00-13-300-001 BETWEEN FR 71-72 OUTSIDE THE REPAIR STRAP AREA. REF FIGURE 5 BELOW FOR REPAIR STRAP LAYOUT. FURTHER TRIM THE SKIN TO THE BUTT JOINT PER A321 SRM 51-27-11. FABRICATE REPAIR PARTS AND INSTALL REPAIR PARTS PER FIGURE 5 AND SRM 51-70-20 FIGURE 3 AND ER/A 615438-14 (LP 0192874)

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