# STC SA01066WI

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: B & C Specialty Products Inc, United States
- Description: Installation of B&C Specialty Products BC410-1 Standby Alternator System.
- Applied: June 7, 2001
- Status date: November 6, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS A3SO](https://openairdocs.org/tcds/A3SO)
- Certificate PDF: https://openairdocs.org/files/sha256/33/17/3317c797cb99e76de0f873ab97d6e82a183850f8cf93a8725c032c5723ed8f34
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5905C4EE1CB9941C862572810059D522.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01066WI

## ADs that name it (0)

None.

## Approved models (13)

- The New Piper Aircraft Inc. PA-32-260 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32-301 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32-301FT ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32-301T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32-301XTC ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32R-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32R-301 (HP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32R-301 (SP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32R-301T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32RT-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32RT-300T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32S-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Part 3 of the Civil Air Regulations.

Description of Type Design Change: Installation of B&C Specialty Products BC410-1 Standby Alternator System. Data Required: (1) B&C Specialty Products, Inc. Drawing List No. 410LST3.DOC, Revision (-), dated June 4, 2001; (2) B&C Specialty Products Document No. FMS410-3, FAA Approved Airplane Flight Manual Supplement, dated April 3, 2002; or later FAA Approved Revisions to (1) or (2).

Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

B & C Specialty Products, Inc.

123 E. 4th Street Newton, KS 67114-0894 A3SO Make : Piper Model : PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, PA-32R-301, PA-32-301, PA-32R-301T, PA-32-301T, PA-32RT- 300T, PA-32-301XTC, PA-32-301FT Date of application : June 7, 2001

Date of issuance : April 3, 2002

Date amended : November 6, 2006

Original signed by HEN

( Signature) Harvey E. Nero FAA Program Manager Wichita Aircraft Certification Office

( Title)

## Every issue (1)

- November 6, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/33/17/3317c797cb99e76de0f873ab97d6e82a183850f8cf93a8725c032c5723ed8f34)

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