# STC SA00381BO - Type: Supplemental type certificate - Status: Current, Amended - Holder: Innovative Solutions & Support Inc, United States - Description: Installation of a Flat Panel Display System (FPDS) with Authrottle System or of an Integrated Standby Unit (ISU) with Autothrottle System - Applied: November 10, 2015 - Status date: February 14, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) - Certificate PDF: https://openairdocs.org/files/sha256/75/a3/75a3996173dc35790c040c21c9ed84a7deea4f702f3a4462569dae6d15ed9d38 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4ABD225D9D3DD9F28625854B00547BC9.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA00381BO ## ADs that name it (0) None. ## Approved models (4) - Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/47E ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. Number SA00381BO FAA Form 8110-2 (5/14) Page 1 of 7 This certificate issued to: Innovative Solutions & Support 1500 District Avenue Burlington, MA 01803 Part 23 of the Federal; Aviation Regulations. Original Product - Type Certificate Number: A78EU Make: Pilatus Model: see Limitations and Conditions 1 Installation of STC configuration 1 only or of STC Configuration 2 only, never both: STC Configuration 1: Flat Panel Display System (FPDS) with Autothrottle System in accordance with Master Data List, 1D-12590, Revision 3, dated May 26, 2017, or later FAA approved revision and Integrated Standby Unit (ISU) in accordance with Master Data List, 1D-11041, Revision 1, dated March 10, 2017, or later FAA approved revision. STC Configuration 2: Integrate d Standby Unit (ISU) with Autothrottle System, see Limitations and Conditions 2. Date of Application: November 10, 2015 Date reissued: June 15, 2017 Date of Issuance: March 22, 2017 Date amended: June 05, 2017; M arch 22, 2018; February 14, 2019 Anthony Pigott for Signature Kevin Dickert Manager, Boston ACO Branch Title FAA Form 8110-2 (5/14) Page 2 of 7 To (Name and address of transferee) Name: Address (Number and Street, City, State, and ZIP Code): From (Name and address of grantor) Name: Address (Number and Street, City, State, and ZIP Code): (Continuation Sheet) Number SA00381BO FAA Form 8110-2 (5/14) Page 3 of 7 1. Installation eligibility is as follows: STC Configuration 1: P C-12, PC-12/45, PC-12/47 STC Configuration 2: PC-12, PC- 12/45, PC-12/47, PC-12/47E 2. STC Configuration 2 is as follows: STC Configuration 2.A being an I ntegrated Standby Unit (ISU) with Autothrottle System and Engine Data Concentrator Unit (EDCU), in accordance with Master Document List, 1D-13058, Revision 2, dated March 21, 2018, or later FAA approved revision. OR STC Configuration 2.B being an I ntegrated Standby Unit (ISU) with Autothrottle System, in accordance with Master Document List, 1D-13455, Revision 1, dated November 30, 2018, or later FAA approved revision. 3. Operation must be in accordance with: STC Configuration 1: Innovative S olutions & Support FPDS Aircraft Flight Manual Supplement (AFMS) Document 1D-12594, Revision 2, dated June 05, 2017, or later FAA approved revision and Innovative Solutions & Support ISU AFMS, Document 1D-11051, Revision 1, dated March 22, 2017, or later FAA approved revision. STC Configuration 2.A: Innovative Solutions & Support AFMS Document 1D-13068, Revision IR, FAA approved on March 21, 2018, or later FAA approved revision. STC Configuration 2.B: Innovative Solutions & Support AFMS Document 1D-13466, Revision IR, FAA approved on February 14, 2019, or later FAA approved revision. The applicable AFMS(s) must be carried in the aircraft during all flights. (continued on Page 4 of 7) (Continuation Sheet) Number SA00381BO FAA Form 8110-2 (5/14) Page 4 of 7 Limitations and Conditions: (continued from Page 3 of 7) 4. Maintenance must be in accordance with: STC Configuration 1: Innovative S olutions & Support FPDS Instructions for Continued Airworthiness (ICA), Document 1D-12592, Revision 3, dated March 17, 2017, or later FAA accepted revision and Innovative Solutions & Support ISU ICA, Document 1D-11054, Revision 2, dated March 04, 2017, or later FAA accepted revision. STC Configuration 2.A: Innovative Solutions & Support ICA Document 1D-13069, Revision 3, dated February 13, 2018, or later FAA accepted revision. STC Configuration 2.B: Innovative Solutions & Support ICA Document 1D-13467, Revision 2, dated September 28, 2018, or later FAA accepted revision. The applicable ICA(s) must be made available to the operator at the time of installation. 5. Compatibility of this design with previously approved modifications must be determined by the installer. Certification Basis STC Configuration 1: Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as significant in FAA Order 8110.48, the certification basis for the Pilatus PC-12, PC-12/45, PC- 12/47 aircraft is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A78EU. (continued on Page 5 of 7) (Continuation Sheet) Number SA00381BO FAA Form 8110-2 (5/14) Page 5 of 7 Certification Basis STC Configuration 1: (continued from Page 4 of 7) b. The modification certification basis for parts changed or affected by the change since the reference application date, November 10, 2015, corresponding to the reference issuance date March 22, 2017, is based upon part 23 as amended by Amendment 23-62 as follows: Regulations at the latest amendment 23-0 through 23-62 23.1(a)(b), 23.21(a)(b), 23.23(a)(b), 23.29(a)(b), 23.143(a)(b), 23.301, 23.303, 23.305(a)(b), 23.307(a)(b), 23.337, 23.341(b), 23.365(a)(b)(c)(d)(e), 23.561(b)(3), 23.572(a)(b), 23.573(b), 23.575, 23.601, 23.603(a)(b), 23.605(a)(b), 23.607(a)(b)(c), 23.609(a)(b), 23.611, 23.613(a)(b)(c)(d)(e), 23.619, 23.625(a)(b)(c), 23.627, 23.672(a), 23.683(a), 23.685(a)(b)(c), 23.693, 23.699, 23.771(a), 23.773(a), 23.777(a)(b), 23.853(a)(f), 23.867(a)(b), 23.1301(a)(b)(c), 23.1303(a)(b)(c)(d)(e)(f)(g), 23.1305(a)(e), 23.1306(a)(b), 23.1307, 23.1308(a)(b)(c)(d), 23.1309(a)(b)(c)(d)(e)(f), 23.1310(a)(b), 23.1311(a)(b)(c), 23.1321(a)(c)(d)(e), 23.1322(a)(b)(c)(d)(e), 23.1323(a)(b)(c)(d), 23.1325(a)(b)(c), 23.1327(a), 23.1329(h), 23.1331(a)(b)(c), 23.1335, 23.1337(a)(b)(c), 23.1351(a)(b), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365(a)(b)(c)(d)(e)(f), 23.1367(a)(b)(c)(d), 23.1419(a)(b)(c)(d), 23.1431(a)(b), 23.1501(a)(b), 23.1519, 23.1523(b), 23.1529, 23.1541(a)(b), 23.1543(a)(b)(c), 23.1549(a)(b)(c), 23.1553, 23.1555(a), 23.1581(a)(b)(c)(d)(e)(f), 23.1585(a)(c)(d)(e)(f)(g)(j), 23.1587 Regulations at an intermediate amendment 23.251(b) at 23-45, 23.571(c) at 23-48, 23.1545(a)(b) at 23-50, 23.1583(m) at 23-50 Regulations at the amendment level in the applicable TCDS 23.1419 Special Condition 23-281-SC, Autothrust System (Continuation Sheet) Number SA00381BO FAA Form 8110-2 (5/14) Page 6 of 7 Certification Basis STC Configuration 2.A: 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 Pilatus PC-12, PC-12/45, PC- 12/47, PC-12/47E aircraft is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A78EU. b. The modification certification basis for parts changed or affected by the change since the amendment application date, April 21, 2017, corresponding to the reference amendment date March 22, 2018, is based upon part 23 as amended by Amendment 23-62 as follows: Regulations at the latest amendment 23-0 through 23-62 23.1, 23.21, 23.23, 23.29, 23.143(a)(b), 23.207(a)(b)(c)(d)(e), 23.301, 23.303, 23.305, 23.307, 23.341(b), 23.365, 23.561(b)(3), 23.571(c), 23.573(b), 23.575, 23.601, 23.603, 23.605, 23.607, 23.609, 23.611, 23.613, 23.619, 23.625(a)(b)(c), 23.627, 23.672(a)(b), 23.683, 23.685(a)(b)(c), 23.691, 23.693, 23.699, 23.771(a), 23.773(a), 23.777(a)(b), 23.779(b)(1), 23.853(a)(f), 23.867(a)(b), 23.933(b), 23.1141, 23.1301, 23.1303, 23.1305(a)(c)(e), 23.1306, 23.1307, 23.1308, 23.1309, 23.1310, 23.1311, 23.1321(a)(c)(d)(e), 23.1322, 23.1323(a)(b)(c)(d), 23.1325(a)(b)(c), 23.1327(a), 23.1329(h), 23.1331, 23.1335, 23.1337, 23.1351(a)(b), 23.1353(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365, 23.1367, 23.1381, 23.1431(a)(b), 23.1501, 23.1519, 23.1529, 23.1541(a)(b), 23.1543, 23.1545(a)(b), 23.1549(a)(b)(c), 23.1553, 23.1555(a), 23.1581, 23.1583(m), 23.1585(a)(c)(d)(e)(f)(g)(j), 23.1587 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS A78EU None Special Condition 23-281-SC, Autothrust System (Continuation Sheet) Number SA00381BO FAA Form 8110-2 (5/14) Page 7 of 7 Certification Basis STC Configuration 2.B: 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 Pilatus PC-12, PC-12/45, PC- 12/47, PC-12/47E aircraft is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A78EU. b. The modification certification basis for parts changed or affected by the change since the amendment application date, May 01, 2018, corresponding to the reference amendment date February 14, 2019, is based upon part 23 as amended by Amendment 23-62 as follows: Regulations at the latest amendment 23-0 through 23-62 23.1, 23.21, 23.23, 23.29, 23.143(a)(b), 23.207(a)(b)(c)(d)(e), 23.301, 23.303, 23.305, 23.307, 23.561(b)(3), 23.601, 23.603, 23.605, 23.607, 23.609, 23.611, 23.613, 23.619, 23.625(a)(b)(c), 23.627, 23.672(a)(b), 23.683, 23.685(a)(b)(c), 23.691, 23.693, 23.699, 23.771(a), 23.773(a), 23.777(a)(b), 23.779(b)(1), 23.853(a)(f), 23.867(a)(b), 23.933(b), 23.1141, 23.1301, 23.1303, 23.1305(c)(1)(e)(1), 23.1306, 23.1307, 23.1308, 23.1309, 23.1310, 23.1311, 23.1321(a)(c)(d)(e), 23.1322, 23.1323(a)(b)(c)(d), 23.1325(a)(b)(c), 23.1327(a), 23.1329(h), 23.1331, 23.1335, 23.1351(a)(b), 23.1353(h), 23.1357(a)(b)(c)(d), 23.1359(c), 23.1365(a)(b)(d)(e)(f), 23.1367, 23.1381, 23.1431(a)(b)(e), 23.1501, 23.1519, 23.1529, 23.1541(a)(b), 23.1543, 23.1545(a)(b)(c), 23.1555(a), 23.1581, 23.1583(m), 23.1585(a)(c)(d)(e)(f)(g)(j), 23.1587 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS A78EU None Special Condition 23-281-SC, Autothrust System ------------------------------------------------------------END------------------------------------------------------- ## Every issue (5) - February 14, 2019: Amended, Current. [certificate](https://openairdocs.org/files/sha256/75/a3/75a3996173dc35790c040c21c9ed84a7deea4f702f3a4462569dae6d15ed9d38) - March 22, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/44/c3/44c3c88fa5c38afa77e152417178fcd30559a11878729e3f6349679abf58c269) - June 15, 2017: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/67/ef/67efc8321aab487c0a73e2af0c66fc359b185d2ef802d686a5e00a6c4f695a28) - June 5, 2017: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/6a/11/6a1112bcb5cb375d2922d67c769b4dd56345a5766986344dbe7d3f461ba51e94) - March 22, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/f1/a4/f1a4dde73e675214357ba835cae1d7088d13cd25fc763331e8c716b5ba9ec2bc) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.