# SDR CA031217006

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 29, 2003
- Submitted: January 5, 2004
- Operation: General aviation
- Make and model: Bombdr DHC8400
- Engine: Pwc PW150A
- Propeller: Rotol CR4086123F17
- System (JASC): [3297 · Landing Gear System Wiring](https://openairdocs.org/jasc/3297)
- Part: Wire Harness
- Part number: 461651
- Condition: Shorted
- Location: Mlg
- Stage of operation: LD
- How discovered: O
- Nature of condition: O
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA031217006

## Discrepancy

(CAN) UPON LANDING PILOT GOT IB ANTI SKID CAUTION LIGHT ON FOR APPROX. 5 SEC. AFTER LANDING. CAUTION LIGHT THEN DISAPPEARED. WHEN PARKED PILOT FOUND RT MAIN INNER TIRE TO BE TOTALLY BLOWN. PAX TOLD US THAT THEY SAW A TIRE THAT NEVER HAD ANY ROTATION AND EXPLODED SHORTLY AFTER LANDING ROLL WAS STARTED. WHEELS NR 3 AND NR 4 REPLACED IAW AMM 32-41-01. AIRCRAFT WAS THEN RELEASED FOR FLIGHT IAW MEL 32-40-2. DURING FURTHER TROUBLESHOOTING WIRES TO RT IB/OB WHEEL SPEED TRANSDUCERS FOUND SHORTED TO GROUND. WIRES REPLACED AND SYSTEM TESTED IAW AMM 32-46-00.

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