# STC ST12295IB - Type: Supplemental type certificate - Status: Current, Issued - Holder: JET AVIATION AG - Description: Installation of Cabin Modification - Status date: February 10, 2026 - Data sheets: A16WE - Certificate PDF: https://openairdocs.org/files/sha256/67/46/6746d1ec6c3c0544c9e536f6a9ce4221451c58f21baf21df9dae9d69a781f96c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131058111820260213163039.0001 - Page: https://openairdocs.org/stc/ST12295IB ## ADs that name it None. ## Approved models (1) - The Boeing Company 737-700 Series (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. **IMPORT ST12295IB** **JET AVIATION AG AESCHENGRABEN 6 4051 BASEL** SWITZERLAND Part 25 Title 14 Code of Federal Regulations A16WE The Boeing Company 737-700 1. This STC is applicable to serial number 32805 for the applicable model. (See Limitations and Conditions Continued on Page 3 of 4) 12/15/2025 02/10/2026 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4 1. Installation of Cabin Modification in accordance with Jet Aviation AG Master Data List Number JBSL-M-03920MDL-001, Issue B, dated December 1, 2025, or later EASA approved revisions. This modification reconfigures the existing First Class Area to a Majlis Area and replace previous seats with new ones in the Business Class Area. (See Description of Type Design Change Continued on Page 3 of 4) 2. Maintenance in accordance with Jet Aviation AG Instructions for Continued Airworthiness Document Number JBSL-M-03920ICA-001, Issue B, dated November 11, 2025, or later EASA accepted revision. 3. Operation in accordance with Jet Aviation AG Airplane Flight Manual Supplement Document Number JBSL-M-03920AFM-001, Issue D, dated December 15, 2025, or later EASA approved revision. 2. Embodiment of FAA STC ST12059IB is a prerequisite to the installation of this STC. 3. Operation must be in accordance with the Limitation Section of the Aircraft Flight Manual Supplement listed in the Description of Type Design section of this STC. 4. The installer must determine whether this design change is compatible with previously approved modifications. 5. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. Certification Basis: Based on 14 CFR ยงยง 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA order 8110.48A, the certification basis for this modification are as follows: a. The Type Certification basis for the 737-700 series is shown on TCDS A16WE for parts not changed or not affected by the change. b. The Type Certification basis for the 737-700 series is shown on TCDS A16WE for parts changed or affected by the change with the following additions: (See Certification Basis on Page 4 of 4) 3 4 14 CFR 25 Amendments 25-1 through 25-153 for Sections 25.29, 25.301, 25.302, 25.303, 25.305, 25.307, 25.321, 25.337, 25.341, 25.365, 25.561, 25.562 except (c)(5)(6), 25.601, 25.603, 25.605, 25.609, 25.613, 25.619, 25.625, 25.785, 25.787, 25.789, 25.791, 25.795, 25.811, 25.812, 25.813, 25.815, 25.851, 25.853, 25.856, 25.899, 25.903, 25.1310, 25.1316, 25.1317, 25.1351, 25.1357, 25.1360, 25.1411, 25.1423, 25.1431, 25.1439, 25.1441, 25.1447, 25.1450, 25.1501, 25.1519, 25.1529, 25.1541, 25.1557, 25.1561, 25.1581, 25.1585, 25.1701 Special Federal Aviation Regulation (SFAR) No. 109 Article 2, 4(a), 4(b), 5, 9, 11, 12, 15(b), Effective 06/08/2009 ----------END---------- ## Every issue (1) - February 10, 2026: Issued, Current. [certificate](https://openairdocs.org/files/sha256/67/46/6746d1ec6c3c0544c9e536f6a9ce4221451c58f21baf21df9dae9d69a781f96c) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.