# STC SA01660WI

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Pilatus Business Aircraft, United States
- Description: Installation of equipment console and inflatable restraint
- Applied: April 7, 2011
- Status date: September 9, 2014
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU)
- Certificate PDF: https://openairdocs.org/files/sha256/48/59/48594fb3aea790aaf4b669350c29755615474b949213a3d45f6797c7a264b1d1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AC753D4A6A53D53886257D5C004E514F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01660WI

## ADs that name it (0)

None.

## Approved models (4)

- 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))
- Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/47E ([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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate N umber SA01660WI This certificate, issued to Pilatus Business Aircraft, Ltd.

11755 Airport Way Broomfield, CO 80021 P art 23 of th e F ederal A viation R egulations .

Original Product Type Certific ate N umber: A78EU M ake: Pilatus M odel: PC-12; PC-12/45; PC-12/47; PC-12/47E Description of the Type Design Change:

Installation of equipment console and inflatable restraint in accordance with Master Data List, A082811-01 MDL, Revision A, dated December 7, 2011, or later FAA approved revisions.

1. STC SA03469AT and STC SA02046LA must be installed on the aircraft prior to installing this STC.

2. FAA approved Airplane Flight Manual Supplement A082811-01FMS, Revision IR, dated December 19, 2011, or later FAA approved revisions. is required for this installation.

3. Compatibility of this design change with previously approved modifications must be determined by the installer.

4. If the STC 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.

Thi s certificate and the supporting data which is the basis for approval s hall remain in effect until sur rendered, suspended, revoked, or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministration.

Date of applic ation: April 7, 2011 Date reissued: January 20, 2012 Date of issuance: January 12, 2012 Date amended: September 9, 2014

(Signature) Gregory K. Johnson, Acting Manager Denver Aircraft Certification Office Northwest Mountain Region (Title)

## Every issue (2)

- September 9, 2014: Amended, Current. [certificate](https://openairdocs.org/files/sha256/48/59/48594fb3aea790aaf4b669350c29755615474b949213a3d45f6797c7a264b1d1)
- January 20, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b7/36/b7361ad9298c2e947b1bacfcab57f18ed3164ad9df730c05ea3fb159dc9f539d)

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