# STC SA04220NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Trine Aerospace & Defense, United States
- Description: Installation of Retractable Camera Mount System
- Applied: July 8, 2022
- Status date: September 24, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU)
- Certificate PDF: https://openairdocs.org/files/sha256/78/93/789330e0376871a20c5cc3ebdb7511329a1eeec6b5ac7df48c0f8814447606b6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187520416220260506171746.0001
- DRS record last changed: May 6, 2026
- Page: https://openairdocs.org/stc/SA04220NY

## 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 Ltd. 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.

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SA04220NY Trine Aerospace & Defense 7565 Taxi Way Colorado Springs, CO 80916 23 14 CFR A78EU Pilatus Aircraft Ltd.

PC-12, PC-12/45, PC-12/47, PC-12/47E Installation of Retractable Camera Mount System in accordance with: (1) Master Data List (MDL) G3-A0000-A22-R01, Rev A, dated January 12, 2023, or later FAA approved revision. (2A) Airplane Flight Manual Supplement (AFMS) -101 & -103 Configurations G3-A0000-A22-R10, Rev A, dated September 23, 2024, or later FAA approved revision.

(Description of Type Design Change Continued on Page 3 of 5)

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

(Limitations and Conditions Continued on Page 3 of 5) July 8, 2022 January 17, 2023 January 16, 2023 September 24, 2024 ODA administrator, ODA-834634-NE 5

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Date oI transfer:

SA04220NY 5

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nited States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA04220NY Date of Amendment: September 24, 2024 Description of Type Design Change (Continued):

(2B) Airplane Flight Manual Supplement (AFMS) -105 & -107 Configurations G3-A0000-A22-R44, Rev IR, dated September 23, 2024, or later FAA approved revision.

The Configuration applicable AFMS must be carried during all flights.

(3A) Instructions for Continued Airworthiness (ICA) -101 & -103 Configurations G3-A0000-A22-R24, Rev IR, dated November 15, 2022, or later FAA accepted revision.

(3B) Instructions for Continued Airworthiness (ICA) -105 & -107 Configurations G3-A0000-A22-R43, Rev IR, dated July 31, 2024, or later FAA accepted revision.

The Configuration applicable ICA shall be made available to the operator at the time of installation and be incorporated into the operator's maintenance program.

(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.

(3) -101 & -103 STC Configuration is applicable to all serial numbers of the Pilatus Aircraft Ltd. model, PC-12, PC-12/45 and PC-12/47 only and -105 & -107 STC Configuration is applicable to all serial numbers of the Pilatus Aircraft Ltd. model, PC-12, PC-12/45, PC-12/47 and PC-12/47E only.

(4) This approval is limited to only the installation of the Retractable Camera Mount and door provisions. The FAA has not evaluated or certified the camera and the related performance and handling qualities of the full installation, for which these provisions are intended. Additional FAA approval to install full equipment, aircraft performance and handling qualities will be required. The FAA must evaluate the installation to ensure it complies with the applicable Airworthiness Standards.

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nited States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA04220NY Date of Amendment: September 24, 2024 Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for all eligible airplane models is as follows:

(1) The type certification basis for Pilatus Aircraft Ltd. Models PC-12, PC-12/45, PC-12/47 and PC-12/47E airplane is shown on the TCDS A78EU for parts not changed or not affected by the change.

(2) The certification basis for parts changed or affected by the change since the reference date of application July 8, 2022, is based upon part 23 as amended by Amendment 23-42 except for those above amendment 23-42, listed following.

Regulations at later amendment than 23-42:

14 CFR Part 23.251 amdt 23-45 14 CFR Part 23.301(a)(b)(c) amdt 23-48 14 CFR Part 23.305 amdt 23-45 14 CFR Part 23.337 amdt 23-48 14 CFR Part 23.341 amdt 23-48 14 CFR Part 23.561 amdt 23-48 14 CFR Part 23.571 amdt 23-62 14 CFR Part 23.573(b) amdt 23-48 14 CFR Part 23.575 amdt 23-48 14 CFR Part 23.611 amdt 23-48 14 CFR Part 23.613(a)(b)(c)(d) amdt 23-45 14 CFR Part 23.629 amdt 23-48 14 CFR Part 23.773(a)(2) amdt 23-63 14 CFR Part 23.777(a)(b) amdt 23-62 14 CFR Part 23.853(a)(d)(3) amdt 23-49 14 CFR Part 23.1307(b)(2)(3) amdt 23-43 (Applicable to Config -101 & -103 only) 14 CFR Part 23.1322(c)(d)(e) amdt 23-43 14 CFR Part 23.1351(a)(b)(1)(i)(ii)(iii)(3)(4)(i)(ii) amdt 23-49 (Certification Basis Continued on Page 5 of 5) 45

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Regulations at later amendment than 23-42 (Continued):

14 CFR Part 23.1357(a)(c) amdt 23-43 14 CFR Part 23.1359(c) amdt 23-49 14 CFR Part 23.1365(a)(d)(e) amdt 23-49 14 CFR Part 23.1431(a)(b) amdt 23-43 (Applicable to Config -101 & -103 only) 14 CFR Part 23.1431(a)(b) amdt 23-49 (Applicable to Config -105 & -107 only) 14 CFR Part 23.1525 amdt 23-45 14 CFR Part 23.1555(a) amdt 23-62 14 CFR Part 23.1581(a)(b)(1)(3)(d)(f) ----------------------------------------------------------------- -------------------------------------- amdt 23-50 (Applicable to Config -101 & -103 only) 14 CFR Part 23.1581(a)(b)(1)(2)(3)(d)(f) -------------------------------------------------------------- -------------------------------------- amdt 23-50 (Applicable to Config -105 & -107 only) 14 CFR Part 23.1583(h) amdt 23-62 (Applicable to Config -101 & -103 only) 14 CFR Part 23.1583(h)(m) amdt 23-62 (Applicable to Config -105 & -107 only) 14 CFR Part 23.1585(j) amdt 23-62 --- END --- 55

## Every issue (2)

- September 24, 2024: Amended, Current. [certificate](https://openairdocs.org/files/sha256/78/93/789330e0376871a20c5cc3ebdb7511329a1eeec6b5ac7df48c0f8814447606b6)
- January 17, 2023: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f8/3b/f83b443fa2870601f5ff8b1446a2988c4da58dcf8434fd27808ed536a1c42da8)

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