# SDR CALA2015030493205

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 28, 2015
- Submitted: March 4, 2015
- Operation: Air carrier
- Aircraft: [N402UA](https://openairdocs.org/aircraft/N402UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 439
- Aircraft time: 69,019 hours, 26,152 cycles
- Engine: Iae V2527A5
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Door Frame
- Condition: Cracked
- 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/CALA2015030493205

## Discrepancy

AFT PAX DOOR CUT OUT, DOOR STOP FITTING HOLES AT FRAME 68 WEB RT POSITION 7 LOWER INBD HOLE IS CRACKED AT APPROX 6 O'CLOCK & 12 O'CLOCK POSITIONS.  HOLE WAS OPENED UP TO .417 & CRACK FREE VIA NTM51-10-01-PB6.  FINAL REAM TO .438 & FREEZE PLUG INSTALLED IAW SRM 53-41-12 PG 223 FIG 204 SH 1.  THIS SRM REFERS TO SRI 53-41-12-2-004-00 PARA 3D TABLE 207 TO INSPECT EVERY 7200C OR 14400T FROM REPAIR EMBODIMENT.  THIS REPAIR AT R2 DOOR FRAME 68 STOP 7 LOWER INBD HOLE.

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