# SDR AWXA0001532

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 23, 2001
- Submitted: March 23, 2001
- Operation: Air carrier
- Aircraft: [N167AW](https://openairdocs.org/aircraft/N167AW), registered now
- Make and model: Boeing 737-33A
- Registry model: [Boeing 737-33A](https://openairdocs.org/model/boeing-737-33a) (OpenAirDocs)
- Aircraft serial: 23628
- Aircraft time: 48,478 hours, 34,597 cycles
- System (JASC): [2782 · Leading Edge Slat Actuator](https://openairdocs.org/jasc/2782)
- Part: Actuator
- Part number: 6544517
- Part serial: 1587
- Condition: Failed
- Location: L/E Flap
- Part time: 56,913 hours, 45,269 cycles
- Stage of operation: CR
- How discovered: O
- Nature of condition: J
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AWXA0001532

## Discrepancy

IAH - EMERGENCY LANDING - 3/18/01 - EN ROUTE FROM PHX TO IAH PRIOR TO DESCENT THE L/E FLAP TRANSIT AMBER LIGHT CAME ON AND REMAINED ILLUMINATED; THE CREW LANDED IN IAH W/ FLAPS 15 PER THE QRH.  MAINTENANCE FOUND THE SLAT CONTROL VALVE CABLE TENSIONS HIGH AND ADJUSTED IAW AMM 27-51-22 PG 406; AFTER THE AIRCRAFT RETURNED TO PHX ON A MAINTENANCE FERRY A COMPLETE TEST WAS PERFORMED ON THE L/E SLAT SYSTEMS.  THE NR 1 KRUEGER FLAP ACT WAS REPLACED DUE TO EXCEEDING LEAK DOWN AND DROOP LIMITS AND CABLES WFFA & WFFB ADJUSTED IAW AMM 27-51-00 PG 509; THE FOLLOWING COMPONENTS WERE ALSO REPLACED AS A PRECAUTION: HYD FUSE - PNEUDRAULICS INC. - P/N 6273-5 - LOC: MLG W/W; HYD.FUSE - DOWTY AEROSPACE - P/N 10-62204-5.

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