# STC SA02536SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Luma Technologies LLC, United States
- Description: Installation of a Luma Technologies LT-4208 LED Display Panel
- Applied: August 8, 2016
- Status date: June 12, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE)
- Certificate PDF: https://openairdocs.org/files/sha256/ee/85/ee855538253c600f5cc8bfe6aa019063fbead02c912e951910fcbca7aec8df77
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0DD098BE2578DA408625813F004418CE.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA02536SE

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- Textron Aviation Inc. 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))

## 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.

Un i te d St ate s of Am e ri ca Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SA02536SE

This certificate, issued to Luma Technologies LLC 13226 SE 30th St, B3 Bellevue, WA 98005

Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A37CE Make: Textron Aviation Inc. (formerly Cessna Aircraft Company) Model: 208, 208B

Description of the Type Design Change: Installation of a Luma Technologies LT-4208 LED Display Panel in accordance with Luma Master Data List (MDL) DB1607002, Revision A, dated April 3, 2017, or later Federal Aviation Administration (FAA) approved revision. Maintained in accordance with Luma Instructions for Continued Airworthiness (ICA) DB1607003, Revision IR, dated December 16, 2016, or later FAA-accepted revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this certificate and ICA must be maintained as part of the permanent records for the modified aircraft.

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.

Date of application: August 8, 2016 Date reissued:

Date of issuance: June 12, 2017 Date amended:

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- June 12, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ee/85/ee855538253c600f5cc8bfe6aa019063fbead02c912e951910fcbca7aec8df77)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
