# STC SA01523NY

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerigo Solutions Inc, Canada
- Description: Installation of a Feather Inhibit System
- Applied: April 23, 2002
- Status date: August 27, 2015
- 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/c1/ee/c1ee4863cc9a20dd3858c17c0824d5edd2f621273dbf27a47520f56578966dde
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7B94C22DD4422BE186257EBB0067C5E0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01523NY

## 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.

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

Part of the

Signature

Title SA01523NY Aerigo Solutions Inc.

2039 Derek Burney Dr.

Thunder Bay, Ontario P7K 0A1 Canada Federation Aviation Regulations 23

1. Installation of a Feather Inhibit System in accordance with ACS-NAI Modification Data Summary Document Number G504000, Revision A, dated December 10, 2010 or later approved revision.

2. Operation must be in accordance with ACS-NAI Operation Handbook and ACS-NAI Airplane Flight Manual Supplement G504091, Revision N/C, approved October 6, 2010 or later Transport Canada approved revision.

3. Maintenance must be in accordance with ACS-NAI Aircraft Maintenance Manual Supplement G504071 Revision A, dated December 10, 2010 or later Transport Canada accepted revision.

1. The installer must determine whether the design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Gaetano Sciortino Manager New York Aircraft Certification Office Pilatus PC 12, PC12/45, PC12/47, and PC12/47E September 13, 2002; March 24, 2015, August 27, 2015 November 30, 2006; January 21, 2011 April 23, 2002 August 6, 2002 IMPORT A78EU 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SA01523NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date Reissued: August 27, 2015

Certificated Basis:

Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA order 8110.38, the certification basis for Pilatus PC 12, PC12/45, PC12/47, and PC12/47E is as follows:

a) For Parts not changed or not affected by the change: The existing type certification basis for the aircraft models are as shown on FAA Type Certificate Data Sheet A78EU

b) For parts changed or affected by the change: The existing type certification basis for the aircraft models are as shown on the FAA Type Certificate Data Sheet A78EU, in addition to FAR 23 Paragraphs at the indicated amendment levels: 23.301(a)-(c) Amdt 23-48, 23.305 (a) Amdt 23-45, 23.613 Amdt 23-45 Amdt 23-1322 Amdt 23-43, 23.1351 (a)-(c) Amdt 23-49, 23.1365 Amdt 23-49 and 23.1555(a) Amdt 23-50.

---------END--------- SA01523NY

## Every issue (2)

- August 27, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c1/ee/c1ee4863cc9a20dd3858c17c0824d5edd2f621273dbf27a47520f56578966dde)
- November 30, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/42/9c/429c6f8a12fd34474c353f4d6ecbdd14e99902b1d10e2de408fe307e956b60b1)

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