# STC SA00945SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Western Aircraft, United States
- Description: Installation of a Ladder Bracket in accordance with Western Aircraft Drawing 00-G2295-1, Revision B, dated June 26, 2001 or later FAA approved revision.
- Applied: May 22, 2001
- Status date: August 3, 2011
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU)
- Certificate PDF: https://openairdocs.org/files/sha256/0f/fb/0ffb6b0431c592a6c48859a888665f18f13555ff332b60a2c629980070df99e1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3E743E02FC1F14A286257959006E7A80.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00945SE

## ADs that name it (0)

None.

## Approved models (2)

- Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))

## 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 SA00945SE

This certificate, issued to Western Aircraft 4444 W. Aeronca Street Boise, ID 83705 Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A78EU Make: Pilatus Model: PC-12, PC-12/45

Description of the Type Design Change: Installation of a Ladder Bracket in accordance with Western Aircraft Drawing 00-G2295-1, Revision B, dated June 26, 2001 or later FAA approved 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 on which other previously approved modifications are incorporated unless it is determined 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. A copy of this Certificate 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: May 22, 2001 Date reissued:

Date of issuance: July 20, 2001 Date amended: August 3, 2001

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

## Every issue (1)

- August 3, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/0f/fb/0ffb6b0431c592a6c48859a888665f18f13555ff332b60a2c629980070df99e1)

---
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.