# STC SA00400BO - Type: Supplemental type certificate - Status: Current, Amended - Holder: Innovative Solutions & Support Inc, United States - Description: Installation of an Autothrottle System (ATS) - Applied: December 14, 2017 - Status date: April 28, 2025 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/29/05/290586d645b5b113d3964edabf408a8540c871ea55e8a6e6d15e4dd6dd010c03 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118877578520250429162208.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00400BO ## ADs that name it (0) None. ## Approved models (8) - Textron Aviation Inc. B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300C (MC-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Textron Aviation Inc. B300C (UC-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) ## 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 SA00400BO Innovative Solutions & Support, Inc. 1500 District Avenue Burlington, MA 01803 Part 23 of the Federal Aviation Regulations. Original Product - Type Certificate Number: A24CE Make: Textron Aviation Inc. (Previous holder: Beechcraft) Model: see Limitations and Conditions 1 Description of Type Design Change: Installation of an Autothrottle System (ATS) in accordance with never more than one Supplemental Type Certificate (STC) Configuration per Original Product model. See Limitations and Conditions 2 for STC Configuration definitions and details. Date of Application: December 14, 2017 Date reissued: Date of Issuance: April 23, 2019 Date amended: December 09, 2019; June 30, 2020; December 11, 2020; December 13, 2022; April 28, 2025 Anthony Pigott for Signature Christina Underwood Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service Title 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 SA00400BO 1. Installation eligibility is as follows: STC Configuration 1: B200GT, B200CGT. All Original Product models must be equipped with Rockwell Collins Pro Line 21™ Avionics. STC Configuration 2: 2.A: B200, B200C, B200GT, B200CGT. All Original Product models must be equipped with Rockwell Collins Pro Line 21™ Avionics. 2.B: B200, B200C, B200GT, B200 CGT, B300, B300C, B300C (MC- 12W), B300C (UC-12W). All Original Product models must be equipped with Rockwell Collins Pro Line 21™ Avionics. 2.C: B200C (C-12R). All Original Pr oduct models must be equipped with Rockwell Collins Pro Line 21™ Avionics modified to display engine torque in percentage (%). STC Configuration 3: B200, B200C, B200GT, B200CGT, B300, B300C, B300C (MC-12W), B300C (UC-12W). All Original Product models must be equipped with Rockwell Collins Pro Line Fusion™ Avionics. STC Configuration 4: B200, B200C, B300, B300C, B300C (MC-12W), B300C (UC-12W). All Original Product models must be equipped with Garmin G1000® Avionics per STC SA01535WI-D and must be equipped with a Mid-Continent MD302® Electronic Standby Indicator per STC SA03289CH. 2. STC Configuration definitions and details are as follows: STC Configuration 1: Innovative Solutions & Support, Inc. (IS&S) Autothrottle Control Panel (ATCP) with ATS, Dual Engine. ATCP Part Number 9K-88121-7, loaded with top level software 7H-13569-03 (or later FAA approved top level software), in accordance with IS&S Master Data List (MDL) 1D-13153, Revision 2, dated April 12, 2019, or later FAA approved revision. ATS, Dual Engine, provides no ENGINE OUT mode. (continued on Page 4 of 8) (Continuation Sheet) Number SA00400BO FAA Form 8110-2 (10/24) Page 4 of 8 Limitations and Conditions: (continued from Page 3 of 8) STC Configuration 2 2.A: Innovati ve Solutions & Support, Inc. (IS&S) Integrated Standby Unit (ISU) with ATS, Dual Engine. ISU Part Number 9K-88130-1, loaded with top level software 7H-13683-09 (or later FAA approved top level software), in accordance with IS&S MDL 1D-13860, Revision 1, dated November 12, 2019, or later FAA approved revision. ATS, Dual Engine, provides no ENGINE OUT mode. OR 2.B: Innovative Solutions & Support, Inc. (IS&S) Integrated Standby Unit (ISU) with ATS, Dual Engine. ISU Part Number 9K-88130-1, loaded with top level software 7H-13683-25 (or later FAA approved top level software), in accordance with IS&S MDL 1D-13700, Revision 20, dated January 21, 2025, or later FAA approved revision. ATS, Dual Engine, provides ENGINE OUT mode. OR 2.C: Innovative Solutions & Support, Inc. (IS&S) Integrated Standby Unit (ISU) with ATS, Dual Engine. ISU Part Number 9K-88130-1, loaded with top level software 7H-13683-25 (or later FAA approved top level software), in accordance with IS&S MDL 1D-15153, Revision 2, dated April 24, 2025, or later FAA approved revision. ATS, Dual Engine, provides ENGINE OUT mode. STC Configuration 3: Innovative Solutions & Support, Inc. (IS&S) Standby Display Unit (SDU)/Remote Standby Controller (RSC) with ATS, Dual Engine. SDU/RSC Part Number 9K-88129-23 or Part Number 9K-88129-25, loaded with top level software SDU 7H-13903-17B/RSC 7H-13906-09 (or later FAA approved top level software), in accordance with IS&S MDL 1D-13780, Revision 30, dated April 18, 2024, or later FAA approved revision. ATS, Dual Engine, provides ENGINE OUT mode. (continued on Page 5 of 8) (Continuation Sheet) Number SA00400BO FAA Form 8110-2 (10/24) Page 5 of 8 Limitations and Conditions: (continued from Page 4 of 8) STC Configuration 4: Innovative Solutions & Support, Inc. (IS&S) Integrated Standby Unit (ISU) with ATS, Dual Engine. ISU Part Number 9K-88130-3, loaded with top level software 7H-13683-23 (or later FAA approved top level software), in accordance with IS&S MDL 1D-14058, Revision 5, dated March 29, 2023, or later FAA approved revision. ATS, Dual Engine, provides ENGINE OUT mode. 3. Operation must be in accordance with Innovative Solutions & Support Aircraft Flight Manual Supplement (AFMS): STC Configuration 1: AFMS Document 1D-13155, Revision IR, FAA approved on April 23, 2019, or later FAA approved revision. STC Configuration 2: 2.A and 2.B: AFMS Document 1D-13764, Revision 3, FAA approved on September 29, 2022, or later FAA approved revision. 2.C: AFMS Document 1D-15152, Revi sion IR, FAA approved on April 23, 2025, or later FAA approved revision. STC Configuration 3: AFMS Document 1D-13792, Revision 4, FAA approved on September 15, 2022, or later FAA approved revision. STC Configuration 4: AFMS Document 1D-13863, Revision IR, FAA approved on December 12, 2022, or later FAA approved revision. The applicable AFMS must be carried in the aircraft during all flights. 4. Maintenance must be in accordance with Innovative Solutions & Support Instructions for Continued Airworthiness (ICA): STC Configuration 1: ICA Document 1D-13154, Revision 1, dated March 27, 2019, or later FAA accepted revision. STC Configuration 2: 2.A and 2.B and 2.C: IC A Document 1D-13704, Revision 8, dated August 03, 2022, or later FAA accepted revision. STC Configuration 3: ICA Document 1D-13791, Revision 5, dated June 28, 2022, or later FAA accepted revision. (continued on Page 6 of 8) (Continuation Sheet) Number SA00400BO FAA Form 8110-2 (10/24) Page 6 of 8 Limitations and Conditions: (continued from Page 5 of 8) STC Configuration 4: ICA Document 1D-13865, Revision 2, dated November 01, 2022, or later FAA accepted revision. The applicable ICA 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. Refer to FAA Advisory Circular (AC) 20-188. (continued on Page 7 of 8) (Continuation Sheet) Number SA00400BO 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 not significant in FAA Order 8110.48, the certification basis for Textron Aviation Inc. B200GT, B200CGT aircraft is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A24CE. b. The modification certification basis for parts changed or affected by the change since the reference application date, December 14, 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, 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), 23.691, 23.699, 23.771(a), 23.773(a)(2), 23.777(a)(b), 23.779(b)(1), 23.853(a)(f), 23.867(a)(b), 23.1301, 23.1305(c)(1)(e)(1), 23.1306, 23.1307, 23.1308, 23.1309, 23.1311, 23.1321(a)(c)(d)(e), 23.1322, 23.1329(h), 23.1331(a)(b)(1)(c)(1), 23.1335, 23.1351(a)(1)(2)(i)(b)(1)(2)(3), 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(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 level None Regulations at the amendment level in TCDS A24CE None Special Condition 23-291-SC, Autothrust System (continued on Page 8 of 8) (Continuation Sheet) Number SA00400BO FAA Form 8110-2 (10/24) Page 8 of 8 Certification Basis: (continued from Page 7 of 8) Certification Basis STC Configuration 2, STC Configuration 3 and STC Configuration 4: 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 Textron Aviation Inc. aircraft models listed in Limitations and Conditions 1 is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A24CE. b. The modification certification basis for parts changed or affected by the change since the amendment application date, March 03, 2025, corresponding to the reference amendment date April 28, 2025, is based upon part 23 as amended by Amendment 23-63 as follows: Regulations at the latest amendment 23-0 through 23-63 23.1, 23.21, 23.23, 23.29, 23.143(a)(b), 23.149, 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), 23.691, 23.699, 23.771(a), 23.773(a)(2), 23.777(a)(b), 23.779(b)(1), 23.853(a)(f), 23.867(a)(b), 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)(c), 23.1325(a)(b)(1)(2)(ii), 23.1327(a), 23.1329(h), 23.1331(a)(b)(1)(c)(1), 23.1335, 23.1351(a)(1)(2)(i)(ii)(b)(1)(2)(3), 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(b)(c), 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 level None Regulations at the amendment level in TCDS A24CE None Special Condition 23-291-SC, Autothrust System ------------------------------------------------------------END------------------------------------------------------- ## Every issue (5) - April 28, 2025: Amended, Current. [certificate](https://openairdocs.org/files/sha256/29/05/290586d645b5b113d3964edabf408a8540c871ea55e8a6e6d15e4dd6dd010c03) - December 13, 2022: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/2e/2e/2e2e1074bdbbacbc2de03c1a3286cae9a89cf0a75c179c82a9c042bb2244ef22) - December 11, 2020: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/5e/bb/5ebbbc38175341c5441698663a5b9c3bc1d0929672cd90040d23bbb14c183627) - June 30, 2020: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/43/77/43778bf16c5a081f0d5171bc6a1b98adfd9206773bc345bb844c388df7d43f84) - December 9, 2019: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/82/90/829046efe8915734f7f0a3132233c43178ca7fa7f614be237647a0f5275ab5b8) --- 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.