# STC SA2819CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Markair Express, Inc, United States
- Description: The use of 20 degree flaps for take-off with the gross weight reduced to 3600 lbs.
- Applied: November 5, 1991
- Status date: June 8, 1992
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A16CE](https://openairdocs.org/tcds/A16CE)
- Certificate PDF: https://openairdocs.org/files/sha256/52/c6/52c69d480052d6c25c4ea16080258e16171ac4ac9cbaf3e376b32be93b1eeea7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3B7BC67CC95EA44885256CC20008C991.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2819CE

## ADs that name it (0)

None.

## Approved models (2)

- The Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- The Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))

## What the certificate says

The certificate is a scan without a text layer; open the PDF to read it.

## Every issue (1)

- June 8, 1992: Amended, Current. [certificate](https://openairdocs.org/files/sha256/52/c6/52c69d480052d6c25c4ea16080258e16171ac4ac9cbaf3e376b32be93b1eeea7)

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