# STC SA00030MC

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Sierra Nevada Corporation, United States
- Description: Installation of non-essential radio rack, communications equipment and antennas.
- Applied: July 24, 2009
- Status date: July 11, 2012
- 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/sha256/32/b6/32b6896bc25a882c77490a31953746c246c34311cdc2bd3b9a14306b1ad73d7a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0600103E4990464A86257C60005671C6.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00030MC

## 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.

Number SA00030MC

This certificate issued to: Sierra Nevada Corporation 11211 E. Arapahoe Road Centennial, Colorado 80112

Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A78EU Make: Pilatus Aircraft Model: PC-12, PC-12/45, PC-12/47 and PC-12/47E Description of Type Design Change:

Installation of non-essential radio rack, communications equipment and antennas in accordance with drawings listed on Sierra Nevada Corporation (SNC) Master Drawing List, Document Number MDL-03030001, Revision E, dated April 18, 2012, FAA approved July 11, 2012 or later FAA approved revision.

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

2. Instructions for Continued Airworthiness, Document 03039305, Rev B, dated July 3, 2012, FAA approved July 11, 2012 or later FAA accepted revision is required for this installation.

3. 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 the permission.

(See continuation sheet 3 of 3 for additional limitations)

Date amended: July 11, 2012

(Signature) Ronald K. Rathgeber Manager Military Certification Office (Title)

Date of application: July 24, 2009 Date of issuance: June 2, 2010

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

Number SA00030MC

4. A copy of this certificate and FAA approved Airplane Flight Manual Supplement, Document 03039312, Revision B, dated July 11, 2012, or later FAA approved revision must be maintained as part of the permanent records of the modified aircraft.

5. This STC is intended for Military, Public, or Government Use Aircraft Only. Installation of this system on aircraft for commercial use is prohibited.

------------------------------------------------------END-----------------------------------------------------------

## Every issue (2)

- July 11, 2012: Amended, Current. [certificate](https://openairdocs.org/files/sha256/32/b6/32b6896bc25a882c77490a31953746c246c34311cdc2bd3b9a14306b1ad73d7a)
- June 2, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/64/8e/648efcb59082e45886c14818148be7377b705e61c2c2e81f6b575c0f5407e292)

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