# SDR SWAA2022100549662

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 2, 2022
- Submitted: October 5, 2022
- Operation: Air carrier
- Aircraft: [N952WN](https://openairdocs.org/aircraft/N952WN), registered now
- Make and model: Boeing 737-7H4
- Registry model: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (OpenAirDocs)
- Aircraft serial: 36667
- Aircraft time: 39,061 hours, 23,816 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Door Frame
- Part number: 141A8181U51
- Condition: Cracked
- Location: Pax Doorway
- 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/SWAA2022100549662

## Discrepancy

PASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. MARKED. / [01] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK WAS NOTED IN AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23;[02] VERIFIED APPLICABILITY OF SRM 53-10-15-01-1 FOR IDENTIFICATION AND SRM 53-10-15-1A-1 FOR ALLOWABLE LIMIT;[03] DAMAGE FOUND AT PASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB BS295 S-16L. CRACK FOUND 6'LONG FOUND TO OUT OF LIMIT IAW SRM 53-10-15-1A-1; 4G FIG 108-C;[04] VERIFIED CORRECTIVE ACTION #2; #3.;[05] REMOVED CRACKED WEB FROM FWD ENTRY DOOR BS 295 STR 16 IAW SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW WEB P/N 141A8181-51 IAW SRM 51-40-05-0G-0 AND DWG#141A8181 REV-3 OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION #5.<BR>VERIFIED OK TO INSTALL REPAIR PARTS.;[07] INSTALLED THE NEW PASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB BS295 STR-16L IAW SRM 51-40-02-0G-0 AND DWG#141A8180;[08] VERIFIED CORRECTIVE ACTION 7 AND THE MEASUREMENT TABLE.;[09] VERIFIED WORKSCOPE IS COMPLETE.

---
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.
