# STC SA2495CE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Learjet Corporation, United States
- Description: Installation of computer-to-engine shielded wire harness.
- Applied: April 19, 1989
- Status date: May 4, 1989
- 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/ad/78/ad781afa24c5fed3ab8b8e56884bcd43669cb0657a68877226d2d5c26013807a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6C1FE18A37FF553285256CC200015EF0.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2495CE

## ADs that name it (0)

None.

## Approved models (2)

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

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Lumber • SA2495CD This certificate issued to: Learjet Corporation P.O. Box 7707 Wichita, Kansas 67277-7707 Certifies that the change in the type design for the filewing product with the limitations und conditions Original Product -Type tertificate Number: ALOCE Regulations paragraph 25.571 (d) of amendment 25-10 with special conditions and other thorefer as specified heren meets the airesthiness requirements s/ Punt 25 at thet ederal Aviation Effective February 1, 1965, as amended by 25-2, 25-4, 25-7, 25-18, and amendments as listed on Type Certificate Data Sheet A1OCE. Make: Learjet Model: 35 and 36 Description of Type Design Change: harness in accordance with Learjet Master Document List No. T100056, Revision Installation of computer-to-engine shielded wire None or later FAA approved revision.

Limitations and Conditions: 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 these other previously approved modifications will introduce This approval should not be extended to other specific no adverse effects upon the airworthiness of that airplane.

FEDERAL AVIATION May 4, 1989 By Direction of the Administrator Laurence A Hesson ( Signature ) Lawrence A. Herron, Manager FEMINIST RELOA Wichita Aircraft Certification Office (Titie ) 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- May 4, 1989: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ad/78/ad781afa24c5fed3ab8b8e56884bcd43669cb0657a68877226d2d5c26013807a)

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