What it approves
Installation of an ARINCDirect XPLORE 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.
Part 23 of the Federal Aviation Regulations. (See Page 3 for complete certification basis)
Installation of an ARINCDirect XPLORE System in accordance with StandardAero Master Data List 1028462, Revision ( C), dated August 19, 2016 or later FAA approved revision.”
1. The installer must determine whether this design change is compatible with previously approved modifications .
2. FAA Approved Airplane Flight Manual Supplement document number 1028711, Rev (C) dated August 4, 2016, or later FAA approved revision is a required part of this modification.
3. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.
StandardAero Business Aviation Services, LLC 1200 North Airport Drive Springfield, IL 62707 A78EU Make: PILATUS AIRCRAFT LTD.
Model: PILATUS PC-12, PC-12/45, PC-12/47, PC-12-47E
Date of application : June 09, 2015
Date of issuance: August 19, 2016 Date reissued :
(Signature) Tim Winiesdorffer, ODA Administrator Standard Aero, Springfield, IL ODA-100079-CE
(Title)
Transfer the ownership of Supplemental Type Certificate Number
to (Name of transferee)
(Address of transferee)
(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)
Signature of grantor (In ink):
Supplemental Type Certificate Number: SA03477CH Date of issuance: August 19, 2016 Date of amendment:
Date of reissue:
Certification Basis (continued)
Based on 14 CFR §§ 21.15, 21.101 and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the PILATUS AIRCRAFT LTD PILATUS PC-12, PC-12/45, PC-12/47, PC-12-47E Installation of a, ARINCDirect XPLORE System is as follows:
a. The type certification basis for PILATUS AIRCRAFT LTD PILATUS PC-12, PC-12/45, PC-12/47, 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, June 09, 2015, is based upon TCDS A78EU. 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 the amendment level in TCDS A78EU
23.1(a, b)(23-34), 23.301(a-c)(23-48), 23.303(Org), 23.305(b)(Org), 23.305(a)(23-45) 23.307(a, b)(Org)
23.561(a, b1)(23-36), 23.561(b2, b3)(23-48), 23.601(Org), 23.603(a, b)(23-23), 23.605(a, b)(23-23)
23.609(a, b)(Org), 23.611(23-7), 23.613(a-e)(23-45), 23.615(a-c)(23-7), 23.619(23-7), 23.625(a)(23-7)
23.1301(a-d)(23-20), 23.1309(a1, a2, b1, b2, b4, e)(23-41), 23.1351(a)(23-34), 23.1357(a)(23-43), 23.1365(a)(23-14),
23.1367(a-d)(Org), 23.1431(a, b)(23-49), 23.1519(Org), 23.1529(23-26), 23.1581(a, b3)(23-34).
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ADs that name this STC · 0
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