What it approves
Installation of a Send Solutions in Flight Entertainment System
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.
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate Number: SA01104DE This certificate issued to: Pilatus Business Aircraft, LTD
12300 Pilatus Way Broomfield, CO 80021 23 of Title 14 Code of Federal Regulations .
Original Product rrype Certzfzcate :Num6er: A78EU Make: Pilatus
Model: PC-12/47E Description of Type Design Change:
Installation of a Send Solutions in Flight Entertainment System in accordance with Master Document List, Doc no. 2E-2203-01-0001, Rev “-“, dated 5/22/2023, FAA approved 7/23/2023 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. 2E-2203-64-0000, Revision “-“ dated 3/3/2023, FAA accepted 7/24/2023, or later FAA accepted revision is required to be made available at installation.
Continued Page 3 of 3 Limitations and Conditions:
1. This STC is applicable to all Serial Numbers of the Pilatus PC-12/47E.
Continued Page 3 of 3
Date of Application: July 13, 2022 Date Reissued:
Date of Issuance: July 24, 2023 Date Amended:
By Direction of the Administrator Signature: - Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC ODA Title: ODA No. ODA(AIR)-833887-NM
This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.4 . 3ossession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC¶s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder.
FAA Form 110 2 ( /20) S83(RS(D(S 3R(9,28S (D,T,21 3age 1 of BB3B
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate Number: SA01104DE
This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.4 . 3ossession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller.
FAA Form 110 2 ( /20) S83(RS(D(S 3R(9,28S (D,T,21 3age 2 of B3BB
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate
(Continuation Sheet) Number: SA01104DE Description of Type Design Change Continued:
Doc. No. 2E-2203-65-0000, FAA Approved Flight Manual Supplement, revision “-“ dated 4/4/2023, FAA Approved 7/19/2023 or later FAA approved revision, is required for this installation.
2. The installer must determine whether this design change is compatible with previously approved modifications.
3. 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.
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the installation of the Send Solutions in Flight Entertainment System is as follows:
a. The type certification basis for Pilatus PC-12/47E is shown on TCDS A78EU for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application, 7/13/2022, is based upon 14 CFR Part 23, effective February 1, 1965 plus Amendments 23-1 through 23-42. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:
Regulations at latest amendment; None Regulations at an intermediate amendment; None Regulations at the amendment level in TCDS A78EU;
14 CFR Sections: 23.301(a-c) Amdt. 23-48; 23.303 Amdt. - ; 23.305(a,b) Amdt. 23-45; 23.307(a) Amdt.
- ; 23.337(a,b) Amdt. 23-48; 23.341 Amdt. 23-48; 23.561(a)(b)(3)(c)(e) Amdt. 23-48; 23.601 Amdt. - ;
23.603 Amdt. 23-23; 23.605(a) Amdt. 23-23; 23.609(a) Amdt. - ; 23.611 Amdt. 23-7; 23.613 Amdt. 23-45;
23.615(a) Amdt. 23-7; 23.619 Amdt. 23-7; 23.625 Amdt. 23-7; 23.771(a) Amdt. 23-14; 23.773(a)(1)(2) Amdt. 23-45; 23.777(a,b) Amdt. 23-33; 23.853(a) Amdt. 23-34; 23.1301 Amdt. 23-20; 23.1309(a),(c) Amdt. 23-62; 23.1322 Amdt. 23-43; 23.1351(a)(1)(2)(i), (b)(1)(i, ii, iii) Amdt. 23-34; 23.1359(c) Amdt.
23-49; 23.1365(a),(b), (d), (e) Amdt. 23-49; 23.1381(a,b) Amdt. - ; 23.1529 Amdt. 23-26; 23.1541(a,b) Amdt. 23-21; 23.1581 Amdt. 23-34
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This certificate may be transferred or made available to third persons by licensing agreements in accordance with Title 14 of the Code of Federal Regulations, part 21, section 21.4 (14 CFR 21.4 ).
FAA Form 110 2 683(56('(6 35(9,286 (',7,21 3age B3BB of BB3B
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Pilatus Aircraft Ltd. | PC-12/47E | A78EU |