# SDR SWAA2025082296425

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 30, 2025
- Submitted: August 22, 2025
- Operation: Air carrier
- Aircraft: [N8699A](https://openairdocs.org/aircraft/N8699A), registered now
- Make and model: Boeing 737-8H4
- Registry model: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (OpenAirDocs)
- Aircraft serial: 36923
- Aircraft time: 29,624 hours, 14,712 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Panel
- Condition: Cracked
- Location: Zone 100
- 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/SWAA2025082296425

## Discrepancy

PANEL 193AR HAS CRACK ON UPPER FWD EDGE.<[01] REMOVED PANEL 193AR TO F.O.M. PER AMM 53-51-21;[02] DISREGARD CORRECTIVE ACTION STATEMENT #1. SEE FAULT ID TTG8Q014A0P9 FOR REMOVAL AND REINSTALLATION OF PANEL 193AR.;[03] REMOVED DAMAGE PER SRM 51-70-05.;[04] VERIFIED DAMAGE REMOVAL. CA #3.;[05] PARTS UPDATE;[06] REPAIRED PER SRM51-70-05-2R-9-BOO393.;[07] INSPECTION C/W CA #6;[08] REFINISHED PANEL PER AMM 51-21-99.;[09] COMPLETED;[10] CW INSPECTION OF STEP #8;[11] PANEL REPAIRED PER SRM 51-70-05-2R-9;[12] REJECT: MEASUREMENT #3 FAULT ASSOCIATED TO FAILURE TYPE (WHEEL/BRAKE/DAMAGE/CORROSION)? (IF YES; SELECT FAILURE TYPE) IS NOT CORRECT. SHOULD BE YES AS FAULT IS BEING WORKED UNDER FAILURE TYPE 05 DAMAGE.;[13] REMOVED DAMAGE PER SRM 51-70-05. UPDATED MEASURMENT #3 TO CHANGE FROM NO TO YES.;[14] REJECT INSPECTION C/W. FOR CA #12.;[15] ALL STEPS COMPLETE;[16] VERIFIED THE CARD IS COMPLETE AND SIGNED OFF AS REQUIRED PER THE MPM 52.2.2

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