# SDR SWAA2025030502296

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 5, 2025
- Submitted: March 5, 2025
- Operation: Air carrier
- Aircraft: [N261WN](https://openairdocs.org/aircraft/N261WN), registered now
- Make and model: Boeing 737-7H4
- Registry model: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (OpenAirDocs)
- Aircraft serial: 32517
- Aircraft time: 60,564 hours, 36,279 cycles
- System (JASC): [2797 · Flight Control System Wiring](https://openairdocs.org/jasc/2797)
- Part: Elec Connector
- Condition: Failed
- Location: Slat Flaps
- Stage of operation: AP
- How discovered: O
- Nature of condition: F
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/SWAA2025030502296

## Discrepancy

LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONNECTOR D275 IAW SWPM 20-61 (E146121)<BR>REF TSR 2025001644 & BOEING SERVICE LETTER 737-SL-27-196-D FOR PART EFFECTIVITY. OPS CHECK GOOD

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