# STC SA3495NM - Type: Supplemental type certificate - Status: Current, Surrendered - Holder: Rogerson ATS, United States - Description: Installation of a 2,250 gallon auxiliary fuel system installed in the forward and aft cargo compartments. - Applied: March 29, 1986 - Status date: September 12, 2008 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) - Certificate PDF: https://openairdocs.org/files/sha256/1c/04/1c0448c923ca4b95d9f36b67cd165ed5738e0bcc21d1d223045b4cd15645ee33 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F8C14C239FE69FCF862574CF007B788E.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA3495NM ## ADs that name it (1) - [AD 2008-12-03](https://openairdocs.org/ad/2008-12-03): Auxiliary fuel tanks · Airbus BAC 1-11 400 Series, 707-100 Long Body, 707-100B Long Body and 15 more. Effective Jul 9, 2008. Named in the applicability ## Approved models (1) - McDonnell Douglas Corporation DC-9-30 Series ([TCDS A6WE](https://openairdocs.org/tcds/A6WE)) ## 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: SA3495NM Certificate This certificate issued to: ROGERSON ATS SURRENDERED 2201 ALTON AVENUE IRVINE, CALIFORNIA 92714 on - 9/12/08 Sart 25 of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet AGWE Original Product Type Certificate Number: AGWE Make: McDonnell Douglas Model: DC-9-30 series Description of Type Design Change: Installation of a 2,250 gallon auxiliary fuel system installed in the forward and aft cargo compartments in accordance with FAA approved Aftermarket Technologies Master Drawing List MDL 245000, Revision C, dated July 22, 1990, or later FAA approved revisions. FAA approved Airplane Flight Manual (AFM) Supplement FMS 245000 dated November 3, 1987, or later FAA approved revision is required. Limitations and Conditions: The approval of this change in type design applies basically to the above listed model series. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the those airplanes. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. (See continuation on page 3). Date of Application: March 29, 1986. Date Reissued: April 12, 1991 Date of Issuance: November 25, 1987 Date Amended: September 12, 1990, February 13, FEDERAL AVIATION 2007 TOMINSTRATO (Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Zip code) Extent of Authority (if licensing agreement): Date of Transfer:_ Signature of grantor (In ink): United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3495NM Limitations and Conditions: Continued: The Partial Grant of Exemption Regulatory Docket No. FAA-2002-14093 issued to Rogerson ATS on September 29, 2005, is contingent upon the approval of this amended STC and the revised AFM supplement dated December 15, 2006, and that required Rogerson ATS to comply as follows: a Prodder a. Prohibit the exercise of the privileges of an STC holder defined in 14 CFR, part 21, unless the STC holder has complied with SFAR No. 88; b. Limit the applicability of the STC to only airplane serial numbers 47041, 47221, 47410, 47428, 47474, 47476, 47477, 47496, 47545, or 47565, unless the STC holder has complied with SFAR 88; c. Revise the AFM supplement to state that STC No. SA3495NM has not been shown to comply with SFAR 88, and that a fuel tank system M&I program for compliance with §§ 91.410(b), 121.370(b), 125.248(b), or 129.32(b) has not been developed; d. In the event any of the Boeing Model DC-9-30 airplanes, serial numbers 47041, 47221, 47410, 47428, 47474, 47476, 47477, 47496, 47545, or 47565, modified in accordance with this STC, are issued a standard airworthiness certificate, Rogerson ATS must comply with the requirements of SFAR No. 88 within 18 months of that issuance; e. This exemption does not provide relief to operators of airplanes modified in accordance with this STC from the requirements in their respective operating rule (§§ 91.140, 121.370, 125.248, or 129.32). -END- 47. ## Every issue (2) - September 12, 2008: Surrendered, Current. [certificate](https://openairdocs.org/files/sha256/1c/04/1c0448c923ca4b95d9f36b67cd165ed5738e0bcc21d1d223045b4cd15645ee33) - February 13, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3f/7e/3f7eef29d4a10ac390507b143fcb50397ae065860b8c4765f97b5b03ddfc2a63) --- 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.