# STC SA2526CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc., United States
- Description: Installation of a seat for a third occupant.  Remove cargo barrier and close-out nets.  Remove partition nets (2 each).  Install aft single seat assembly
- Applied: August 7, 1989
- Status date: March 9, 2018
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE)
- Certificate PDF: https://openairdocs.org/files/sha256/05/17/0517d025bee2e8e5ee93c406bfd34177eb415a942bb8d08561aa97309e2fa39a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F5DDBDA03A46E2428625829F0055450C.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2526CE

## ADs that name it (0)

None.

## Approved models (3)

- The Cessna Aircraft Company 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- The Cessna Aircraft Company 208A ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- The Cessna Aircraft Company 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.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title by 23-1 through 23-28 and Special Condition 23-ACE-3.

SA2526CE Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 23 Federal Aviation Regulations as amended Cessna 208 (with Cargomaster Option), 208A and 208B 2 A37CE Installation of a seat for a third occupant. Remove cargo barrier and close-out nets, Part Number 2613334-1, 2613334-17, or 2613334-34 (208 and 208A), 2613334-17 or 2613334-31 (208B), 2613337-1, and 2613337-2 (2 each).

Remove partition nets (2 each) 2601174-1, 9910573-1 or 9910573-6. Install aft single seat assembly 2614041-1. All part numbers are Cessna Aircraft Company numbers.

1. Airplane Flight Manual (AFM) Supplement dated August 21, 1989, is required equipment when this modification is installed.

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.

March 9, 2018 August 7, 1989 August 21, 1989 Mark Fuller STC ODA administrator ODA-100129-CE

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

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- March 9, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/05/17/0517d025bee2e8e5ee93c406bfd34177eb415a942bb8d08561aa97309e2fa39a)
- August 21, 1989: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/1a/de/1ade71312a7c8f261e764fa2d558b6e07589aca652f85a46ce713f6c5131d418)

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