# SDR CIEA200500004

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 14, 2005
- Submitted: May 14, 2005
- Operation: Air carrier
- Aircraft: [N222BE](https://openairdocs.org/aircraft/N222BE), registered now
- Make and model: Lear 35A
- Registry model: [Lear 35A](https://openairdocs.org/model/gates-learjet-35a) (OpenAirDocs)
- Aircraft serial: 35A489
- Aircraft time: 10,033 hours, 7,660 cycles
- System (JASC): [1420 · Electrical Connectors](https://openairdocs.org/jasc/1420)
- Part: Connector
- Part number: PT06SE106S
- Condition: Broken
- Part time: 10,033 hours, 7,660 cycles
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CIEA200500004

## Discrepancy

THE STALL WARNING ACCELEROMETER WAS BEING USED TO TROUBLESHOOT A PROBLEM ON ANOTHER AIRCRAFT.  DURING THE REMOVAL OF THE ACCELEROMETER, THE WIRE BROKE ON PIN B OF THE CANNON PLUG.  AS PART OF THE TROUBLESHOOTING IT WAS DETERMINED THE PROBLEM ON THE OTHER AIRCRAFT WAS ALSO A BROKEN WIRE ON THE CANNON PLUG FOR THE ACCELEROMETER AS WELL.  THE WIRES TO THE CANNON PLUG ARE VERY SMALL.  DURING COMPLIANCE OF AD 82-01-05 R2, THE WIRES ARE FLEXED AS PART OF THE CHECK.  THIS AD HAS A RECURRING INTERVAL OF 220 HOURS.  THE CONTINUED TESTING OF THE ACCELEROMETER IS GOING TO RESULT IN MORE WIRE FAILURES.

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