# STC ST09832DS - Type: Supplemental type certificate - Status: Current, Issued - Holder: United Airlines, United States - Description: PSCP: ER2500R01724, ODA Project 98320. (1) B737-800 (HIC) Interior Reconfiguration & eX1 IFE Installation - Applied: September 3, 2024 - Status date: December 11, 2024 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/65/9d/659deb239b24a861116b4c8b34d7923c095dd5a02438a23ffe1765d0944fdd19 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174023687020241220151528.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST09832DS ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 737-800 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. ST09832DS United Airlines 4933 Wright Road Houston, TX 77032 25 & 26 the Federal Aviation Regulations A16WE The Boeing Comapny 737-800 Series (1) The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. (continued on page 3) 09/03/2024 12/11/2024 Raju Tumarada, STC Administrator United Airlines Organization Designation 3 PSCP: ER2500R01724, ODA Project 98320. (1) B737-800 (HIC) Interior Reconfiguration & eX1 IFE Installation in accordance with MDL 2500DA16090 Rev A, dated 11/22/2024, or later FAA approved revision (2) Supplemental Instructions for Continued Airworthiness, Document Number 2500R01725C Rev -, dated 10/22/2024 or later FAA approved revision (contd on page 3) ST09832DS 3 ST09832DS --- Description of Type Design Change (continued): (3) AFM Supplement, Document N0696-D85, Rev D, dated 09/26/2023. (4) No EWIS ICA is required for this modification. (2) 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. (3) Concurrent installation of BE Aerospace Inc., FSI ODA STC: ST02739SE for LED lighting installations in B737-700 and B737-800 series airplane. (4) Concurrent installation of Boeing Service Bulletin: 737-25-1890 for installation of overhead stowage bins is required for all Boeing 737-800 aircraft modified by this STC. Certification Basis: Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are not significant in FAA Order 8110.48, the certification basis for this modification is as follows: a. The type certification basis for parts not changed or not affected by the change is shown in TCDS A16WE, Rev 76. b. The certification basis for parts changed or affected by this modification since the reference application date September 03, 2024, is based upon the type certification basis shown in TCDS A16WE, Rev 76 with the following exceptions: 14 CFR Part Amdt 14 CFR Part Amdt 25.899 25-123 25.853 (a) 25-83 25.981 25-146 25.571 (a)(b) 25-86 25.1431(c) 25-113 c. The modification certification basis also includes Special Conditions Number 25-358-SC, dated August 9, 2007. ST09832DS issued December 11, 2024. ---END--- 3 3 Add Page ## Every issue (1) - December 11, 2024: Issued, Current. [certificate](https://openairdocs.org/files/sha256/65/9d/659deb239b24a861116b4c8b34d7923c095dd5a02438a23ffe1765d0944fdd19) --- 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.