# STC ST00369BO - Type: Supplemental type certificate - Status: Current, Issued - Holder: Innovative Solutions & Support Inc, United States - Description: Installation of an Innovative Solutions & Support, Inc. (IS&S) Integrated Standby Unit (ISU), Part Number 9D-80190-13, loaded with top level software 7H-80190-17 - Applied: February 17, 2016 - Status date: August 3, 2016 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25, Part 26 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/3e/d3/3ed37376b9ad9e508fb695fb1239e7d1c6093fc8a69f64100b7ecdfe6c91e531 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E4E06BF052AE4F6886258004006F0F46.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST00369BO ## ADs that name it (0) None. ## Approved models (3) - The Boeing Company 737-300 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-400 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-500 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) ## 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. Supplemental Type Certificate Number: ST00369BO FAA Form 8110-2 (5/14) Page 1 of 4 This certificate issued to: Innovative Solutions & Support, Inc. 1500 District Avenue Burlington, MA 01803 Part 25 of the Federal; Aviation Regulations. Original Product - Type Certificate Number: A16WE Make: The Boeing Company Model: 737-300 Series, 737-400 Series, 737-500 Series Installation of an Innovative Solutions & Support, Inc. (IS&S) Integrated Standby Unit (ISU), Part Number 9D-80190-13, loaded with top level software 7H-80190-17 as defined in Limitations and Conditions 3 (or later FAA approved top level software), in accordance with IS&S Master Document List (MDL) 1D-11030, Revision 3, dated July 29, 2016, or later FAA approved revision. 1. Operation must be in accordance with IS&S Aircraft Flight Manual Supplement (AFMS) 1D- 12290, Revision 1, FAA approved on August 03, 2016, or later FAA approved revision. The AFMS must be carried in the aircraft during all flights. (continued on Page 3 of 4) Date of Application: February 17, 2016 Date reissued: Date of Issuance: August 03, 2016 Date amended: Signature Anthony Pigott Acting Manager, Boston Aircraft Certification Office Title Supplemental Type Certificate Number: ST00369BO FAA Form 8110-2 (5/14) Page 2 of 4 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: ST00369BO FAA Form 8110-2 (5/14) Page 3 of 4 Limitations and Conditions: (continued from Page 1 of 4) 2. Maintenance must be in accordance with: a) IS&S Instructions for Continued Airworthiness (ICA) 1D-12275, Revision 1, dated May 26, 2016, or later FAA accepted revision. b) IS&S Electrical Wiring Interconnection Systems (EWIS) ICA 1D-12280, Revision 4, dated July 21, 2016, or later FAA approved revision. These ICAs must be made available to the operator at the time of installation. 3. IS&S ISU, Part Number 9D-80190-13, loaded with top level software 7H-80190-17, is defined as: Article Part Number Article Description 9D-80190-13 with Integrated Standby Unit (ISU) Software Part Number Software Description 7H-09848-1 Boot Software 7H-10227-17 OFP Software 7H-10228-13 Service Software 10H-10041-1 FPGA Firmware 4. Modification of and equipage of the Captain’s Main Instrument Panel P1 per STC ST03125NY is a prerequisite requirement in order to accomplish this STC. 5. 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 Boeing Company 737-300 Series, 737-400 Series, and 737-500 Series aircraft is as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A16WE. b. Regarding 14 CFR § 26.47 (Amdt. No. 26-1), this change does not affect or create fatigue critical structure. (continued on Page 4 of 4) (Continuation Sheet) Number: ST00369BO FAA Form 8110-2 (5/14) Page 4 of 4 Certification Basis: (continued from Page 3 of 4) c. The modification certification basis for parts changed or affected by the change since the reference application date, February 17, 2016, is based upon part 25 as amended by Amendment 25-141 as follows: Regulations at the latest amendment 25-0 through 25-141 25.1(b), 25.21(a)(1), 25.29, 25.301(a), 25.303, 25.305(a)(b), 25.307(a), 25.365(a)(b)(c)(d), 25.561(a)(b)(3)(c)(d), 25.571(a)(b), 25.581(a)(b)(1), 25.601, 25.603, 25.605(a), 25.607(a)(2)(b)(c), 25.609, 25.611, 25.613(a)(c)(f), 25.619, 25.625(a)(b), 25.771(a)(c), 25.773(a), 25.831(b)(c), 25.853(a), 25.869(a), 25.899, 25.1301, 25.1302, 25.1303(a)(c), 25.1309, 25.1310, 25.1316(b), 25.1317(b)(c), 25.1321(a)(b)(d)(e), 25.1322, 25.1323(a)(b)(c)(f)(g)(h)(i), 25.1325(a)(d)(e), 25.1327, 25.1331, 25.1333(b)(c), 25.1351(a)(b)(2)(d), 25.1353(a)(c), 25.1357, 25.1360, 25.1381, 25.1431, 25.1501, 25.1523(b), 25.1529, 25.1541, 25.1543(b), 25.1545, 25.1547(a)(b)(d), 25.1555(a), 25.1581(a)(b)(d), 25.1583(c)(1), 25.1585(a)(b), 25.1703(a)(b)(d), 25.1705(a)(b)(4)(5)(6)(7)(9)(12), 25.1707(a)(b)(c)(d)(g)(h)(i)(j)(k)(l), 25.1709, 25.1711, 25.1713, 25.1715, 25.1717, 25.1719, 25.1721(b), 25.1729 Regulations at an intermediate amendment level None Regulations at the amendment level in TCDS A16WE None ------------------------------------------------------------END------------------------------------------------------- ## Every issue (1) - August 3, 2016: Issued, Current. [certificate](https://openairdocs.org/files/sha256/3e/d3/3ed37376b9ad9e508fb695fb1239e7d1c6093fc8a69f64100b7ecdfe6c91e531) --- 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.