# STC SA3810WE - Type: Supplemental type certificate - Status: Current, Surrendered - Holder: Aircraft Tank Service Inc, United States - Description: Installation of a maximum of eight auxiliary fuel tanks in forward and aft cargo compartments. (727-51, -30, -23, -35, -46, -193, -22, -29C) - Status date: September 12, 2008 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS A3WE](https://openairdocs.org/tcds/A3WE) - Certificate PDF: https://openairdocs.org/files/sha256/8c/9a/8c9a2e0fbcf4e895708d7722d91f84339752ba55353f3cee5382f32d7b4d1b91 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6BF27FCBD8855BC4862574CF007B783D.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA3810WE ## 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 (3) - The Boeing Company 727 ([TCDS A3WE](https://openairdocs.org/tcds/A3WE)) - The Boeing Company 727 Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE)) - The Boeing Company 767 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM)) ## 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 SA3810WE Certificate SURRENDERED This certificate issued to: Aircraft Tank Service, Incorporated on 9/12/08 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hercerts the in sabine segui Tent Prype CertIcate Data Sheet Regulalions: AWE Revision 12 Original Product - Type Certificate Number: АЗWE Make: Boeing Model: 727-100 Series (SEE PAGE 4) Description of Type Design Change: SEE PAGE 3 Limitations and Conditions: SEE PAGE 3 Date of Application: . June 9, 1978 Jule wissued: April 17, 1979 Date of Issuance: . December 15, 1978 Date Amended: SEE PAGE 3 FEDERAL AVIATION a lovel Centrie TO MINISTRATO Aclung certification office ( Title) TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (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): **C FAA AC 69-5536** United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA3810WE Description of Type Design Change: Installation of a maximum of eight auxiliary fuel tanks in the forward and aft cargo compartments in accordance with FAA approved Drawing List TA-18-1004, or later FAA approved revisions, as shown on Page 4 for each configuration. An FAA approved Airplane Flight Manual Supplement, or later FAA approved revisions, is required as part of this installation as shown on Page 4 for each configuration. Limitations and Conditions: The approval of this change in type design applies basically to the Boeing 727-100 advanced or upgraded models with maximum gross weight capabilities, as indicated in table on Page 4. This approval should not be extended to other specific airplanes of these models 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 introduce no adverse effect upon the airworthiness of the above listed airplanes. Approval of each configuration is applicable only to the airplane serial numbers shown on Page 4. AMENDMENT LISTING 1-4-80 (A) Added 727-17, Serial Number 20512, ATS Drawing List TA-18-1004, Rev. P, dated 11-7-79 (A) Added 727-76, Serial Number 20228, ATS Drawing List TA-18-1004, Rev. R, dated 4-23-80 (A) Added 727-29C, Serial Number 19987, ATS Drawing List TA-18-1004, Rev. T, dated 11-14-80 (A) Added 727-76, Serial Number 19254, ATS Drawing List TA-18-1004, Rev. R, dated 4-23-80 (A) Added 727-76, Serial Number 20371, ATS Drawing List TA-18-1004, Rev. R, dated 4-23-80 6-17-81 (A) Added 727-23, Serial Number 20045, ATS Drawing List TA-18-1004,, 11-10-81 (A) Added 727-35, Serial Number 19835, ATS Drawing List TA-18-1004, Rev. V, dated 8-31-81 11-10-81 (A) Added 727-193, Serial Number 19620, ATS Drawing List TA-18-1004, Rev. V, dated 8-31-81 12-4-81 (A) Added 727-46, Serial Number 19282, ATS Drawing List TA-18-1004, Rev. V, dated 8-31-81 **FAA FORM 8110-2-1 (10-69) PAGE 3 OF 4PAGES C FAA AC 73-2651** United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3B20NE Max. Taxi (1) Aux. Tank (2) Boeing ATS Boeing Model Wt. Lb/BAC Configuration & Boeing Wt. &Bal. Wt. & Bal. & Eligible Master Master Dwg. List AFM AFM (2) & Loading & Ldg.Man. Serial No.'s Chg. No. TA-18-1004 DC-8727 Supplement Manual Supplement 727-51 -503 TA 7-3 TA 7-1 19121/ 161,000 Rev C 12-8-78 • 14 1-30-81 D6-7693 2-2-81 -503 TA 7-3 TA 12-2 19123 161,000 Rev C 12-7-78 • 14 1-30-81 D6-7693 2-2-81 127-17 -504A TA 116 D6- TA 122 20512 170,000 Rev P 11-7-79 • 57 1-4-80 21100.57 12-26-79 727-76 170,000 -504 TA 128 TA 130 20228 2400-152k Rev R 4-23-80 - 6 9-12-80 D6-7692 8-25-80 19254 170,000 -504 TA 128 TA 130 2400-187 Rev R 4-23-80 ~ 6 Rev A D6-7692 Rev F 20371 170,000 -504 TA 128 TA 130 2400-152k Rev R 4-23-80 - 6 Rev A D6-7692 Rev F 727-29C 170,000 -504C TA 169 D6- TA 170 19987 Rev T 11-14-80 • 31 5-1-81 21000. 31C 11-3-80 727-23 170,000 -504 TA 128 TA 130 20045 2400-207k Rev R 4-23-80 - 3 Rev A D6-21100.3 Rev F 727-35 161,000 -504A TA 116.1 TA 122 19835 Rev V 8-31-81 . 43 D6-21100.43 Rev C 727-193 161,000 -504 TA 128 TA 130 19620 Rev V 8-31-81 • 30 Rev B D6-21000.30 Rev H 727-46 163,801 -504 TA 128 TA 130 19282 Rev V 8-31-81 • 65 Rev C D6-21100.65 Rev I Note: (1) If aircraft is certificated for operation at 170,000 lbs. by incorporation of the appropriate Boeing Master Change the STC approval is extended to this configuration. Refer to applicable section of weight and balance supplement. (2) Consulting Aerospace Engineers, Inc. for the -503 configuration; Aircraft Tank Service, Inc. for all other configurations. END **FAA FORM 8110-2-1 (10-69) PAGE4 OF 4 PAGES C FAA AC 73-2651** ## Every issue (1) - September 12, 2008: Surrendered, Current. [certificate](https://openairdocs.org/files/sha256/8c/9a/8c9a2e0fbcf4e895708d7722d91f84339752ba55353f3cee5382f32d7b4d1b91) --- 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.