STC SA01946WI

Supplemental type certificate · Pilatus Business Aircraft, LTD

Holder
Pilatus Business Aircraft, LTD · United States
Status
Current · Reissued
Status date
April 5, 2024
Applied
November 28, 2018
Product
Aircraft · Small Airplane
Certification basis
Part 23
Data sheet
TCDSA78EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of multi-mission equipment, antennas, and interior configurations

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

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Original Product 7\SH&HUWLILFDWH1XPEHU Make:

SA01946WI Pilatus Business Aircraft, LTD 12300 Pilatus Way Broomfield, CO 80021 PT 23 Code of Federal Regulations A78EU Pilatus Aircraft Ltd.

PC-12/47E Installation of multi-mission equipment, antennas and interior configurations.

1. Sierra Nevada Corporation (SNC), Master Data List (MDL) 0431-0200-0008, Revision A, dated July 29, 2020, or later FAA approved revision.

(Description continued on Page 3)

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

(Limitations continued of Page 3) November 28, 2018 November 22, 2021, April 5, 2024 August 6, 2020 March 27, 2024 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 5

$Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&’s supporting documentation (drawings, instructions, SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  3DJH RIBBB United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Too (Name and address of transferee):

Date oI transfer:

SA01946WI 5

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nited States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01946WI Date Reissued: April 5, 2024 Description of Type Design Change (continuation)

2. SNC, Airplane Flight Manual Supplement (AFMS), Document Number 0431-0200-0006, Revision B, FAA approved August 6, 2020, or later FAA approved revision.

3. SNC, Instructions for Continued Airworthiness (ICA), Document Number 0431-0200-0007, Revision A, dated May 1, 2020. FAA accepted August 6, 2020, or later FAA accepted revision, shall be made available to the operator at the time of installation.

Limitations and Conditions (continuation)

2. 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.

3. Approval of this change in type design applies to the model of airplane shown in page 1 of this STC.

4. A copy of this certificate, the AFMS, and the ICA shall be maintained as part of the permanent records for the modified airplane.

5. This STC includes provisions for future equipment installations. The FAA has not certified the equipment for which these provisions are intended. You must get additional FAA approval to install the equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards.

6. The following are prerequisites to the installation of this STC: Installation of STCS SA00028MC (configuration 0126.4390.4000.01), SA02801NY, SA01715WI, and SA00634DE.

7. This STC is intended for military, public, or government use only.

8. Laser operation is not FAA approved for civil aircraft operation. The laser is disabled.

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the applicable 14 CFR Part 23 aircraft affected is as follows:

a. As specified on the applicable Type Certificate Data Sheet (TCDS) of the aircraft for parts not changed or not affected by this STC.

b. Regulations at the amendment levels defined within the below table for parts changed or affected by the STC since the reference date of STC application, 11/28/2018.

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Regulations at the amendment level in TCDS A78EU:

45 Section

23.71

23.305(b)

23.479(a)

23.573(b)

23.575

23.867(a)(b)(c)

23.1306(a)(b)

23.1308(a)(b)(c)

23.1322(a)(b)(c)(d)

23.1357(c)

23.1365(a)(c)(2) Amdt.

23-50 23-45 23-45 23-48 23-48 23-49 23-61 23-57 23-43 23-43 23-49 Section

23.21

23.23

23.25

23.29

23.45(a)(b)(c)(e)

23.49(a)(b)

23.49(c)

23.51(a)(1)

23.65(a)(1)(2)(3)(c)

23.75(a)

23.77(a)(b)

23.233(a)

23.251

23.301

23.303

23.305(a)

23.307(a)(b) Amdt.

23-0 23-17 23-34 23-21 23-34 23-21 23-44 23-34 23-34 23-42 23-34 23-0 23-0 23-48 23-0 23-45 23-0 Section

23.331

23.333

23.335(a)(b)(c)

23.337(a)(1)(b)(1)(c)

23.341(b)

23.347

23.365(a)(b)(c)(d)

23.421

23.423

23.425(a)(c)(d)

23.441(a)(c)

23.443

23.471

23.473

23.477

23.479(b)(c)

23.481(a)(2)(b) Amdt.

23-42 23-34 23-48 23-34 23-42 23-0 23-0 23-42 23-42 23-42 23-42 23-42 23-0 23-28 23-0 23-45 23-0

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Regulations at an intermediate amendment level:

23.1351(a)(1)(2)(i) [Amdt. 23-49].

---------------------------------------END------------------------------------- 55 Section

23.483

23.561(a)(b)(1)(c)(1)(2)(e)

23.561(b)(2)(3)(c)(3)

23.562(d)(1)

23.571(a)

23.572(a)(1)(b)(1)

23.601

23.603

23.605(a)(b)

23.607(c)

23.609

23.611

23.613

23.615(a)(b)(c)

23.619

23.623(a)

23.625

23.627

23.771(a)

23.773(a)(1)(2)

23.777(a)(b)

23.785(i)

23.787(a)(b)(e)

23.853(a)

23.863

23.901(a)(e) Amdt.

23-0 23-36 23-48 23-50 23-45 23-45 23-0 23-23 23-23 23-48 23-0 23-7 23-45 23-7 23-7 23-7 23-7 23-0 23-14 23-45 23-33 23-36 23-36 23-34 23-34 23-34 Section

23.1301(a)(b)(c)(d)

23.1309(a)(1)(2)(b)(c)(1)(e)

23.1321(a)(c)(d)

23.1322(e)

23.1351(a)(b)(1)(i)

23.1351(g)

23.1353(h)

23.1357(a)

23.1359(a)(c)

23.1365(b)(c)(1)(d)(e)(f)

23.1367

23.1381(a)(b)

23.1419(b)

23.1431(a)(b)(e)

23.1441(b)

23.1447(d)

23.1501

23.1529

23.1541(a)(b)

23.1555(a)

23.1557(a)

23.1581(a)(b)(d)

23.1583(d)(h)(l)

23.1585(a)

23.1587(a)(5)(6)(7)(8)

23.1589 Amdt.

23-20 23-41 23-41 23-43 23-34 23-49 23-49 23-43 23-49 23-49 23-0 23-0 23-14 23-49 23-9 23-30 23-21 23-26 23-21 23-21 23-23 23-34 23-34 23-34 23-34 23-13

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Pilatus Aircraft LimitedPC-12/47EA78EU

Every issue · 4

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
April 5, 2024Reissued, currentCertificate
March 27, 2024Amended, earlier issueCertificate
August 6, 2020Issued, earlier issueCertificate
August 6, 2020Reissued, earlier issueCertificate