# STC SA01782LA

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: AvSpec Corporation, United States
- Description: Installation of 130 ampere alternator
- Applied: September 4, 2004
- Status date: April 26, 2017
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/5d/a2/5da2d6471d10fc250c461dfe17921f413c3cb55886ab5efbc27cdde0bfe319d8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/70CD1D70ED9A67BE86258117006A1FD1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01782LA

## ADs that name it (0)

None.

## Approved models (2)

- The Cessna Aircraft Company 206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- The Cessna Aircraft Company T206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))

## 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.

AvSpec Corporation 1900 Flightline Drive, Suite 3 Lincoln, California 95648 3

A4CE

Cessna

T206H, 206H

Installation of 130 ampere alternat or in accordance with AvSpec Corporation Master Drawing List (MDL) No. AV4019MDL, Revision B, dated February 3, 2005, or later FAA approved revision and FAA Approved Airplane Flight Manual Supplement No. AV001 or No. AV002, see page 3 for details.

Approval of this change in the type design applies to the above aircraft model(s) only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined the interrelationship between this changed and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this STC must be include d in the permanent records of the modified airplane.

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.

September 4, 2004

April 15, 2005

April 26, 2017

(Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Title)

SA01782LA

FAA Approved Airplane Flight Manual Supplement No. AV001 dated April 14, 2005, or later FAA approved revision: Maximum Takeoff Weight: Reduce by 30 lbs.

FAA Approved Airplane Flight Manual Supplement No. AV002, Rev IR, dated March 28, 2017, or later FAA approved revision: Alternator load meter must be monitored and load kept at or below 95 amps from takeoff to 1,500 ft AGL.

NOTE: Noise characteristics - This modification was determined not to increase the noise level and was not considered an “acoustical change” as defined in § 21.93(b), Amendment 21-73 of the Federal Aviation Regulations.

-END-

## Every issue (2)

- April 26, 2017: Amended, Current. [certificate](https://openairdocs.org/files/sha256/5d/a2/5da2d6471d10fc250c461dfe17921f413c3cb55886ab5efbc27cdde0bfe319d8)
- April 15, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/f7/4b/f74b77bfe2134de892c87a6180b94eb108bb4b4c02703c9a3c623d1529d4fbbf)

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