# STC SA01851SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aerocet Inc, United States
- Description: Installation of Aerocet Pilatus Porter PC-6 Under Wing Cargo Pods, in accordance with Aerocet Inc, Master Drawing List PC-6-100, Revison F, dated June 23, 2011, or later Federal Aviation Administration (FAA) approved revision.  This installation is maintained in accordance with Aerocet, Inc. Installation and Service Instructions for Continued Airworthiness, Report PC-6-100-MMS, Revision A, dated October 5, 2011, or later FAA-approved revision.
- Applied: April 24, 2008
- Status date: December 12, 2011
- Product: Aircraft
- Certification basis: Part 21
- Data sheets: [TCDS 7A15](https://openairdocs.org/tcds/7A15)
- Certificate PDF: https://openairdocs.org/files/sha256/35/5a/355a008d8c04f7807ecfda6dd25f299ecb1f5156c7a82c4c88733b0dd9829664
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6E3C58DEC80ECD748625796B00680C8E.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01851SE

## ADs that name it (0)

None.

## Approved models (1)

- Pilatus Aircraft Limited PC-6/B2-H4 ([TCDS 7A15](https://openairdocs.org/tcds/7A15))

## 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 SA01851SE

This certificate, issued to Aerocet, Inc.

265 Shannon Lane Priest River, ID 83856 Part 10/3 amdts 3-1 through 3-5 of the Civil Air Regulations.

Original ProductType Certificate Number: 7A15 Make: Pilatus Aircraft Ltd.

Model: PC-6/B2-H4

Description of the Type Design Change: Installation of Aerocet Pilatus Porter PC-6 Under Wing Cargo Pods, in accordance with Aerocet Inc, Master Drawing List PC-6-100, Revison F, dated June 23, 2011, or later Federal Aviation Administration (FAA) approved revision. This installation is maintained in accordance with Aerocet, Inc.

Installation and Service Instructions for Continued Airworthiness, Report PC-6-100-MMS, Revision A, dated October 5, 2011, or later FAA-approved revision.

Limitations and Conditions: Approval of this change applies to the above model only, and should not be extended to other specific models of these airplanes 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, and Airplane Flight Manual Supplement, Revision IR, dated July 5, 2011, or later FAA-approved revision, 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: April 24, 2008 Date reissued:

Date of issuance: December 12, 2011 Date amended:

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- December 12, 2011: Issued, Current. [certificate](https://openairdocs.org/files/sha256/35/5a/355a008d8c04f7807ecfda6dd25f299ecb1f5156c7a82c4c88733b0dd9829664)

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