# STC SA8726SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: RAM Aircraft Limited Partnership, United States
- Description: Increase maximum ramp weight from 6750 to 7140 pounds and maximum takeoff weight to 7105 pounds, and addition of optional McCauley model 3AF32C515/82NLA-4.0 propellers.
- Applied: May 20, 1993
- Status date: September 11, 2008
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A7CE](https://openairdocs.org/tcds/A7CE)
- Certificate PDF: https://openairdocs.org/files/sha256/20/2b/202b8f3b3503b940f0c7b7df96ec92ba4dd59ebfac10b7303cedd84905e5ec0b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/07492AE2621183BA8625793E006AB334.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA8726SW-D

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company 414A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))

## What the certificate says

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

## Every issue (1)

- September 11, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/20/2b/202b8f3b3503b940f0c7b7df96ec92ba4dd59ebfac10b7303cedd84905e5ec0b)

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