# STC SA1508CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Avcon Industries, Inc, United States
- Description: Installation of mounting plates in the tail cone for mounting of electrical inverters.
- Applied: February 28, 1979
- Status date: October 18, 2018
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE)
- Certificate PDF: https://openairdocs.org/files/sha256/50/66/5066eebd7acd138f72bf04a3612b27b02ffbe988c2b30bb75633ee6e26d20e76
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D890B2C119CB694186258340004F332B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1508CE

## ADs that name it (0)

None.

## Approved models (4)

- Learjet Inc. Learjet 35 ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))
- Learjet Inc. Learjet 35A (C-21A) ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))
- Learjet Inc. Learjet 36 ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))
- Learjet Inc. Learjet 36A ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))

## 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.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title 1965, as amended by 25-2 and 25-4, plus amendments and special conditions as listed in the type certificate data sheet.

SA1508CE Avcon Industries, Inc.

714 N Oliver Rd Newton, KS 67114 25 Federal Aviation Regulations effective February 1, Learjet 35, 35A, 36, 36A Installation of mounting plates in the tail cone for mounting of electrical inverters per Avcon Drawing List No. 35019-1, stamped FAA Approved on August 14, 1979, or later FAA Approved revision.

1. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

2. Approval of this STC does not constitute authority to produce parts for sale.

2 A10CE February 28, 1979 August 14, 1979 August 17, 1979; April 16, 1990; June 22, 1990;

October 18, 2018 Boyd Rodeman Program Manager Wichita ACO Branch

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

2 SA1508CE

## Every issue (1)

- October 18, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/50/66/5066eebd7acd138f72bf04a3612b27b02ffbe988c2b30bb75633ee6e26d20e76)

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