What it approves
Installation of a Flat Panel Display System (FPDS)
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.
Number SA00349BO
FAA Form 8110-2 (8/13) Page 1 of 4 This certificate issued to:
Innovative Solutions & Support 720 Pennsylvania Drive Exton, PA 19341 Part 23 of the Federal Aviation Regulations.
Original Product Type Certificate Number: A78EU Make: Pilatus Aircraft Limited Model: PC-12, PC-12/45, PC-12/47
Installation of a Flat Panel Display System (FPDS) in accordance with Master Drawing List, 1D- 10407, Rev. 2, dated November 14, 2013
1. Operation must be in accordance with the Airplane Flight Manual Supplement (AFMS), 1D- 09976, Rev. 1, dated August 13, 2013 or later FAA-approved revision. This AFMS must be carried on the aircraft during all flights.
Continued on Page 3
Date of Application: February 14, 2013 Date reissued:
Date of Issuance: December 5, 2014 Date amended:
Signature Robert G. Mann
Manager, Boston Aircraft Certification Office Title
SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)
FAA Form 8110-2 (8/13) Page 2 of 4
TRANSFER
ENDORSEMENT
To (Name of transferee)
(Address of transferee)
(Number and street)
(City, State, and ZIP Code)
From (Name of grantor)
(Address of grantor)
(Number and street)
(City, State, and ZIP Code)
Number SA00349BO December 5, 2014
FAA Form 8110-2 (8/13) Page 3 of 4
Limitation and Conditions (continued):
2. Maintenance must be in accordance with Instructions for Continued Airworthiness 15.6-Inch Flat Panel Display Instructions Pilatus PC-12, 1D-09979, Rev. 2, dated July 11, 2013 or later FAA- approved revision.
3. The FAA has not evaluated the airworthiness of this installation with any video image displayed on the flight displays. Additional approvals are necessary to make use of that feature of the FPDS.
4. Compatibility of this design with previously approved modifications must be determined by the installer.
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 the Make Model aircraft is as follows:
a. The type certification basis for parts not changed or not affected by the change is shown on the applicable TCDS.
b. The modification certification basis for parts changed or affected by the change since the reference application date, February 14, 2013, is based upon part 23 as amended by Amendment 23-62 as follows:
Regulations at the latest amendment 23-0 through 23-62
23.29(a)(b), 23.301(a)(b)(c)(d), 23.303, 23.305(a)(b), 23.307(a), 23.337(a)(1)(2)(b)(1),
23.561(a)(b)(3), 23.601, 23.603(a), 23.607(a)(b)(c), 23.613(a)(b)(c)(d), 23.619(a)(b)(c),
23.623(a), 23.625(a)(b)(c), 23.773(a)(2), 23.853(a)(d)(3)(f), 23.867(a)(b)(c), 23.1301,
23.1303, 23.1306, 23.1308(a), 23.1309(a)(c)(d), 23.1310(a)(1)(2)(4)(b), 23.1311(a)(b),
23.1321(a)(c)(d)(e), 23.1322, 23.1329(h), 23.1331, 23.1335, 23.1351(a)(b), 23.1353(h)(1)(ii),
23.1357(a)(b)(c)(d), 23.1359(c), 23.1365(a)(b)(d)(e)(f), 23.1381(a), 23.1431(a)(b),
23.1523(b), 23.1529, 23.1543(b)(c), 23.1545(a)(b)(1)(2)(3)(4)(c)(d), 23.1555(a),
23.1581(a)(b)(1)(3)(c)(f), 23.1583(h)(m), 23.1585(j)
Number SA00349BO December 5, 2014
FAA Form 8110-2 (8/13) Page 4 of 4 Regulations at an intermediate amendment None Regulations at the amendment level in the applicable TCDS None ------------------------------------------------------------END-------------------------------------------------------
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