# SDR CA031103006

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 28, 2003
- Submitted: January 5, 2004
- Operation: General aviation
- Make and model: Bell 206B-3
- Registry model: [Bell 206B-3](https://openairdocs.org/model/bell-helicopter-textron-206b-3) (OpenAirDocs)
- Engine: Allsn 250C20B
- System (JASC): [6410 · Tail Rotor Blades](https://openairdocs.org/jasc/6410)
- Part: Blade
- Part number: 206016201131
- Condition: Oversized
- Location: Tail Rotor
- 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/CA031103006

## Discrepancy

(CAN) CHAMFERS 44 DEG 30 INCHES - 45 DEG 30 INCHES (2 PLACES) X .395 - .415 DIMENSION ARE ACTUALLY OVERSIZE TO .450. BLADES CAN BE REWORKED BY RE-MACHINING THE CHAMFERS TO THE REQUIRED DIMENSION.  THE CHAMFERS ARE LOCATED AT THE ROOT END OF THE BLADE WHERE IT MATES WITH THE PITCH HORN 206-011-809.

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