# SDR SWAA2025061674209

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 22, 2025
- Submitted: June 16, 2025
- Operation: Air carrier
- Aircraft: [N940WN](https://openairdocs.org/aircraft/N940WN), registered now
- Make and model: Boeing 737-7H4
- Registry model: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (OpenAirDocs)
- Aircraft serial: 36900
- Aircraft time: 51,407 hours, 31,575 cycles
- System (JASC): [5350 · Aerodynamic Fairings](https://openairdocs.org/jasc/5350)
- Part: Access 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/SWAA2025061674209

## Discrepancy

CRACK ACCESS PANEL 194GR BODY FAIRING AT LOWER FUSELAGE 2025-340197<[01] REJECT STEP 10. BECAUSE THE REPAIR PLIES INSTALLED DO NOT MEET THE OVERLAP REQUIREMENTS IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2>CURED THE REPAIR PLIES AND PERFORMED POST REPAIR INSPECTION (TAP TEST) ON REPAIRED AREA AND FOUND IN GOOD CONDITIONS IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2 PARAGRAPH 4.I;J AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARAGRAPH 4.N AND O.(1); B737-700 NDT MANUAL PART1 51-05-01. TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18196021 DUE DATE: 22-FEB-26. CURED TIME: 220 MINUTES AT 200 DEGREES FAHRENHEIT.;[03] VERIFIED CORRECTION IN C/A # 2 HUGO TEJADA ( TECHNICIAN). REMOVE AND INSTALL NEW REPAIR PLIES. THE PROCESS IS DOCUMENTED IN PARTIAL WORK STEPS 11 TO 14.<BR> <BR>CURED THE REPAIR PLIES AND PERFORMED POST REPAIR INSPECTION (TAP TEST) ON REPAIRED AREA AND FOUND IN GOOD CONDITIONS IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2 PARAGRAPH 4.I;J AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARAGRAPH 4.N AND O.(1); B737-700 NDT MANUAL PART1 51-05-01. TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18196021 DUE DATE: 22-FEB-26. CURED TIME: 220 MINUTES AT 200 DEGREES FAHRENHEIT.;[04] REPAIRED ACCESS PANEL 194GR BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] REPAIRED ACCESS PANEL 194GR BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.

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