# STC SA2007CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Avcon Industries, Inc, United States
- Description: Installation of 9KVA, 3 phase inverter system, consisting of 3 J.E.T. SI-3000A Inverters
- Applied: July 30, 1984
- Status date: October 18, 2018
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE)
- Certificate PDF: https://openairdocs.org/files/sha256/a8/48/a84849f62730d3d67a59800a10cf1d39d4a1b908a1892908623bc04f7f82b70d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D1A4A0489407574B86258340004F33AA.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2007CE

## 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 25-1, 25-2, 25-4, 25-7, 25-18, plus applicable paragraph of Amendment 25-10 and special conditions per the Type Certificate Data Sheet.

SA2007CE Avcon Industries, Inc.

714 N Oliver Rd Newton, KS 67114 25 Federal Aviation Regulations effective February 1, A10CE Learjet 35, 35A, 36, 36A Installation of 9KVA, 3 Phase Inverter System, consisting of 3 J.E.T. SI-3000A Inverters in accordance with:

1. Gates Learjet Corporation STC Specification Sheet No. T100046, Revision A, and

2. FAA Approved Airplane Flight Manual Supplement dated August 13, 1984, or later FAA approved revision of 1 or 2.

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 July 30, 1983 August 13, 1983 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 SA2007CE

## Every issue (2)

- October 18, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a8/48/a84849f62730d3d67a59800a10cf1d39d4a1b908a1892908623bc04f7f82b70d)
- June 22, 1990: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/54/c6/54c6f4a217a53d43afc49a13d8a452aa2aaf9c0de133502650ba0c34bdb65a6c)

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