What it approves
Installation of non-essential communications equipment.
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.
FAA Form 8110-2 (8/13) Page 1
Part of the Federal A viation Regulations.
Original Product – Type Certificate Number: MDNH:
MRGHO:
Signature
Title
SA00117MC Sierra Nevada Corporation 11551 E. Arapahoe Road Centennial, CO 80112 23 A78EU Pilatus Aircraft Ltd.
PC-12/47E Installation of non-essential communications equipment. Data required includes:
1) Sierra Nevada Corporation Master Data List (MDL), 0232-00-9436, Rev A, Dated 08/14/2014 or later FAA approved revision.
2) Sierra Nevada Corporation Airplane Flight Manual Supplement (AFMS) 0232-00-9414, Rev A, Dated 08/14/2014 or later FAA approved revision.
3) Sierra Nevada Corporation Instructions for Continued Airworthiness (ICA) 0232-00-9415, Rev A, Dated 06/18/2014 or later FAA approved revision.
1) Compatibility of this design change with previously approved modifications must be determined by the installer.
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 above model of airplane only.
4) A copy of this certificate and the ICA shall be maintained in the airplane permanent records.
5) Supplemental Type Certificate (STC) SA00102MC must be installed as a prerequisite to installation of this STC.
2/28/2014 8/15/2014 06/17/2015 William Eckler ODA administrator, ODA(AIR)-833355-CE
FAA Form 8110-2 (8/13) Page 2
To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):
SA00117MC
FAA Form 8110-2 (8/13) Page 3
SA00117MC 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 Pilatus Model PC-12/47E Non-Essential Communications Equipment is as follows:
a. The type certificate basis for Pilatus PC-12/47E is shown on 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 the application, 02/28/2014, is based upon 14 CFR Part 23 as amended by Amendment 23-42 and additional selected rules at later amendments as listed on the TCDS. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in the FAA Order 8110.48, the certification basis for this modification was determined to be:
Regulations at the latest amendment 23-0 through 23-62
23.305(b) [Amdt. 23-45], 23.573(b) [Amdt. 23-48], 23.575 [Amdt. 23-48], 23.607(a)(b) [Amdt. 23-48], 23.1351(a)
(1)(2)(i)(b)(1)(i) [Amdt. 23-49], 23.1357(b)(c) [Amdt. 23-43], 23.1365(a)(c)(2) [Amdt. 23-49]
Regulations at the amendment level in the TCDS A78EU
23.23 [Amdt. 23-17], 23.25 [Amdt. 23-34], 23.45(a)(b)(c)(e) [Amdt. 23-34], 23.65(a)(c) [Amdt. 23-34], 23.77 [Amdt. 23-34], 23.171 [Amdt. 23-0], 23.177(a) [Amdt. 23-21], 23.251 [Amdt. 23-0], 23.301(a)(b)(c) [Amdt.
23-48], 23.303 [Amdt. 23-0], 23.305(a) [Amdt. 23-45], 23.307(a)(b) [Amdt. 23-0], 23.321 [Amdt. 23-0], 23.333 [Amdt. 23-34], 23.335(a)(b)(c) [Amdt. 23-48], 23.337(a)(1)(b)(1)(c) [Amdt. 23-34], 23.341(b) [Amdt. 23-42],
23.365 [Amdt. 23-0], 23.441 [Amdt. 23-42], 23.443 [Amdt. 23-42], 23.561(b)(3) [Amdt. 23-48], 23.562 (d)(1) [Amdt. 23-50], 23.571(a) [Amdt. 23-45], 23.601 [Amdt. 23-0], 23.603 [Amdt. 23-23], 23.605(a) [Amdt. 23-23],
23.607(c) [Amdt. 23-48], 23.609 [Amdt. 23-0], 23.611 [Amdt. 23-7], 23.613 [Amdt 23-45], 23.615(a) [Amdt.
23-7], 23.619 [Amdt. 23-7], 23.623(a) [Amdt. 23-7], 23.625(a)(b)(c) [Amdt. 23-7], 23.627 [Amdt. 23-0], 23.853(a) [Amdt. 23-34], 23.863 [Amdt. 23-34], 23.867(a)(b)(1)(2) [Amdt. 23-7], 23.967(e)(2)(i) [Amdt. 23-36], 23.994 [Amdt. 23-29], 23.1301(a)(b)(c)(d) [Amdt. 23-20], 23.1351(g) [Amdt. 23-49], 23.1353(h) [Amdt. 23-49], 23.1357
(a) [Amdt. 23-43], 23.1359(a)(c) [Amdt. 23-49], 23.1365(b)(c)(1)(d)(e)(f) [Amdt. 23-49], 23.1419(b) [Amdt.
23-14], 23.1431(b) [Amdt. 23-49], 23.1529 [Amdt. 23-26], 23.1581(a)(b)(d) [Amdt. 23-34], 23.1583(c)(1) [Amdt.
23-34], 23.1587(a)(7) [Amdt. 23-34] Regulation at an intermediate amendment
23.571(b)(c) [Amdt. 23-45], 23.1309(a)(1)(2)(b)(1)(2)(4)(c)(1)(e)(f) [Amdt. 23-49]
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 Limited | PC-12/47E | A78EU |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| June 17, 2015 | Amended, current | Certificate |
| August 15, 2014 | Issued, earlier issue | Certificate |