# STC SA00215SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Spoilers Inc, United States
- Description: Installation of aerodynamic spoilers to the wing.
- Applied: January 6, 1995
- Status date: July 9, 2013
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A10](https://openairdocs.org/tcds/3A10)
- Certificate PDF: https://openairdocs.org/files/sha256/68/6f/686f31f425e63916042fc3062833251113a8852cd200eb839eed45756e7ad4ea
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C4B792D1AF298C4486257BA5005176F6.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00215SE

## ADs that name it (0)

None.

## Approved models (2)

- The Cessna Aircraft Company 310R ([TCDS 3A10](https://openairdocs.org/tcds/3A10))
- The Cessna Aircraft Company T310R ([TCDS 3A10](https://openairdocs.org/tcds/3A10))

## 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.

Number SA00215SE

This certificate, issued to Spoilers, Inc.

1202 26th Avenue NW Gig Harbor, WA 98335 Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: 3A10 Make: Cessna Model: 310R and T310R

Description of the Type Design Change: Installation of aerodynamic spoilers to the wing, per Master Drawing List for SP13,000 spolilers, Revision A, dated May 1, 1995, and Installation Instructions for SP13,000 dated March 27, 1995, or later FAA approved revisions.

Limitations and Conditions : Approval of this change in type design applies to the above model aircraft only. This approval should not be exteded to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. Additionally, this modification must be installed along with a Vortex Generator Kit per Aeronautical Testing Services STC SA5163NM, or Micro Aerodynamics STC SA4980NM or SA5668NM. A copy of the FAA Approved Flight Manual Supplement dated July 7, 1995, or later FAA approved revision, and a copy of this Certificate must be maintained as part of the permanent records for the modfied aircraft.

Date of application: January 6, 1995 Date reissued: July 9, 2013 Date of issuance: July 7, 1995 Date amended:

(Signature) Manager, Seattle Aircraft Certification Office (Title)

## Every issue (2)

- July 9, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/68/6f/686f31f425e63916042fc3062833251113a8852cd200eb839eed45756e7ad4ea)
- July 7, 1995: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/5a/d5/5ad58c246c73a70639f05a6fe4b4235336eba11513b12fb73f9c1274371b2207)

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