# SDR CALA2023063002080

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 28, 2023
- Submitted: June 30, 2023
- Operation: Air carrier
- Aircraft: [N468UA](https://openairdocs.org/aircraft/N468UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1363
- Aircraft time: 71,736 hours, 29,476 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Frame
- Part number: D5348008225200
- Condition: Cracked
- Location: Fr 68 Lh, Door
- 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/CALA2023063002080

## Discrepancy

FR 68 LH, DOOR STOP 1, LOWER IB HOLE HAS 2EA CRACK INDICATIONS IN FRAME LAYER @ 12 AND 7 OCLOCK DIRECTION ( AD RELATED SUPPORT T ASK) (AD2022-22-04) GENERATED AT HAECO LCQ PER NR 9296381 (26381 ) BY MECH V892444 N IAW SRM 53-41-12-300-010. PERFORMED ROTOSCAN, NO DEFECTS NOTED LS OF 10700FC (FH NOT RELEVANT). INSPECTION METHOD IS HFEC (REFE INSPECTIONS AT INTERVALS OF 10700FC (FH NOT RELEVANT). (REFER TO AMM 53-41-00). . INSTALLED REPAIR BUSHING AND PERFORMED AND FINAL REAMED TO 2ND R TO NTM 51-10-08) AND ROTOTEST (REFER TO AMM 53-41-00). INSPECTION METHOD IS HFEC (REFER TO NTM 51-10-08) AND ROTOTEST OVERSIZE OF 0.2810IN IAW SRM 53-41-12-300-010. PER SRI 5.-41-12-205-009, TABLE 002, INSPECTION THRESHOLD IS FROM TIME OF ADL EMBODIMENT24500FC (FH NOT RELEVANT), SUBSEQUENT ADD EMP:HAECO EMPL V934655 REPAIRED HOLE AT FR68 DOORSTOP #1 LWD IAW SRM 53-41-12-300-010. PERFORMED COLDWORK OF NON-DISCREPANT HOLES AND REAMED TO 2ND OVE REAMED HOLE FROM 0.2810IN TO 0.3470IN IAW SRM 53-41-12-12-300-00 RSIZE OF 0.2810IN IAW SRM 53-41-12-300-010. PER SRI 5.-41-12-205 8. PERFORMED ROTOSCAN IAW NTM 51-10-01, NO DEFECTS NOTED. COLDWO -009, TABLE 002, INSPECTION THRESHOLD IS FROM TIME OF ADL EMBODI RKED HOLE IAW SRM 53-41-12-300-010. FINAL REAMED HOLE TO 0.4210I MENT24500FC (FH NOT RELEVANT), SUBSEQUENT INSPECTIONS AT INTERVA ADD EMP:HAECO EMPL V934655 OK TO CARRY FR 68 LH, DOOR STOP 1, LOWER IB HOLE REPAIR FOR TOMC-APPROVAL FROM SC1ELBYC COMMENT 24500 FLT CYC (FLT HRS NOT RELEVANT) FROM TIME OF R

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
