# STC SA2526SO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: B/E Aerospace Inc., United States - Description: Installation of oven P/N 2510-0032-01, 02, 03, and 04. - Applied: August 8, 1988 - Status date: June 29, 2002 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) - Certificate PDF: https://openairdocs.org/files/sha256/f3/02/f302951cd62669bb72a1d222c08b51df4638183e2629911145a737054229868e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2BC28BEDEAFBA95B85256CC200015F5D.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA2526SO ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 747 Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA252650 This certificate issued to: B/E Aerospace, Inc. 10800 Pflumm Road Lenexa, KS 66215 Certifies that the change in the type design for the following product with the linvitations and conditions therefor as specified hereon meeks the airverthiness requirenvents of Part 25 of the Federal Aviation Poegulation Original Product --Type Berlificate Number: A20WE Make: Boeing Model: 747 Series Description of Type Design Change: Installation of oven P/N 2510-0032-01, 02, 03 and 04, in accordance with Aircraft Products Division Drawing 2505-0007, dated February 21, 1989, or later FAA approved revision. Sivlations and benditions: This approval should not be extended to other airplanes of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give suspended, revcked or a ternination date is otherwise established by the Administrator of the Federal Soviation Administration. Date of Application: August 8, 1988 Date Reissued: July 26, 1989; April 3, 2001; June 29, 2002 Date of Issuance: March 21, 1989 Date Amended: FEDERAL AVIATION Bon Bucater (Signature) A Melvin D. Taylor TOMINISTRATO Manager, Atlanta Aircraft Certification Office (Title) PAA FORM 8110-2 (10-68) PAGE 1 Of 1 PAGES ## Every issue (1) - June 29, 2002: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f3/02/f302951cd62669bb72a1d222c08b51df4638183e2629911145a737054229868e) --- 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.