# STC SA3634SW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Sierra Industries Ltd. - Description: Install three auxiliary bladder type fuel tanks in each wing. - Status date: July 14, 2017 - Data sheets: A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE, A4CE - Certificate PDF: https://openairdocs.org/files/sha256/3c/46/3c4655b6e0350ef2d2b9cb95d82f8ac3defd98d11cfe32d9ba8d0b12e72d0b1a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3472A3F2560BA771862587200054CB24.0001 - Page: https://openairdocs.org/stc/SA3634SW ## ADs that name it None. ## Approved models (13) - Textron Aviation Inc. 206H (TCDS A4CE) - Textron Aviation Inc. P206A (TCDS A4CE) - Textron Aviation Inc. P206B (TCDS A4CE) - Textron Aviation Inc. P206C (TCDS A4CE) - Textron Aviation Inc. P206D (TCDS A4CE) - Textron Aviation Inc. T206H (TCDS A4CE) - Textron Aviation Inc. U206A (TCDS A4CE) - Textron Aviation Inc. U206B (TCDS A4CE) - Textron Aviation Inc. U206C (TCDS A4CE) - Textron Aviation Inc. U206D (TCDS A4CE) - Textron Aviation Inc. U206E (TCDS A4CE) - Textron Aviation Inc. U206F (TCDS A4CE) - Textron Aviation Inc. U206G (TCDS A4CE) ## 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. FAA Form 8110-2 (5/14) Page 1 of 4 Reissued on July 14, 2017 to supersede the original STC, which has been lost or misplaced. Number: SA3634SW Part 3/23 of the CAR/FAR Regulations. Original Product – Type Certificate Number: A4CE Make: Cessna Model: 206H; T206H; P206 A, B, C, D, and E; and U206 A, B, C, D, E, F and G Description of Type Design Change: Install three auxiliary bladder type fuel tanks in each wing according to Sierra Industries, Ltd., Drawing List No. SI 10600, Revision N, dated January 27, 2006, and Installation Instruction No. SI 10665, Revision D, dated July 18, 1986, or Installation Instructions No. SI 10666, Revision A, dated July 18, 1986 or later FAA approved revision. Compatibility of this design change with previously approved modifications must be determined by the installer. 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. Date of Application: October 24, 1985 Date Reissued: July 21, 2005; July 14, 2017 Date of Issuance: July 11, 1986 Date Amended: March 30, 2010; Revision 4 Signature Title James A. Grigg Manager, Fort Worth Aircraft Cer tification Office, Southwest Region Sierra Industries, Ltd. 122 Howard Langford Drive Uvalde, TX 78801 FAA Form 8110-2 (5/14) Page 2 of 4 Transfer the ownership of Supplemental Type Certificate Number: SA3634SW To (Name and address of transferee) From (Name and address of grantor) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3634SW FAA Form 8110-2 (5/14) Page 3 of 4 Date of Issuance: July 11, 1986 Date Amended: March 30, 2010 Date of Reissuance: July 14, 2017 Description of Type Design Change (continued): FAA approved Airplane Flight Manual Supplement (AFMS) requirements are as follows: A. Cessna P206A, B, C, D, and E model landplanes (S/N P206-0161 through P206-00647). • For aircraft with standard range bladder type fuel tank, AFMS No. SI 10681, dated July 24, 1986, or later FAA approved revision is required. • For aircraft with extended range bladder type fuel tanks, AFMS No. SI 10682, dated July 24, 1986, or later FAA approved revision is required. B. Cessna U206A, B, C, D, E, F, and G model landplanes. • (S/N U206-0438 to U206-04649) – For aircraft with standard range bladder type fuel tank, AFMS No. SI 10681, dated July 24, 1986, or later FAA approved revision is required. • (S/N U206-0438 to U206-04649) – For aircraft with extended range bladder type fuel tank, AFMS No. SI 10682, dated July 24, 1986, or later FAA approved revision is required. • (S/N U206-04650 to present) – For aircraft with wet wing fuel tanks, AFMS No. SI 10680, dated July 24, 1986, or later FAA approved revision is required. C. Cessna 206H and T206H model landplanes • (S/N 206-08001 to present and T206-08001 to present) – For aircraft with wet wing fuel tanks, AFMS No. SI 10691, dated March 14, 2006, or later FAA approved revision is required. D. Cessna U206G model landplanes with STC SA2353NM, Soloy Conversions, Ltd. Allison 250 Turboprop Engine installation. • (S/N U206-02589 and U206-04650 to present) – For aircraft with wet wing fuel tanks, AFMS No. 10685, dated July 11, 1986, or later FAA approved revision is required. E. Cessna U206G model landplanes with bladder type fuel tanks and STC SA2353NM, Soloy Conversions, Ltd. Allison 250 Turboprop Engine installation. • (S/N U206-03522 to U206-04649) – For aircraft with standard range bladder type fuel tanks, AFMS No. SI 10683, dated December 12, 1986, or later FAA approved revision is required. • (S/N U206-03522 to U206-04649) – For aircraft with extended range bladder type fuel tanks, AFMS No. SI 10684, dated December 12, 1986, or later FAA approved revision is required. F. Cessna 206H and T206H model landplanes with STC SA2353NM, Soloy, LLC installation of the Soloy Turbine Pac (Rolls-Royce 250-C20S engine modified per Soloy, LLC STC SE2352NM) and related changes in accordance with FAA approved Soloy Master Drawing List Number 763-300, dated May 12, 2003, or later FAA approved revisions. • (S/N 206-08001 to present and T206-08001 to present) – AFMS No. 10692, dated March 30, 2010, or later FAA approved revision is required. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3634SW FAA Form 8110-2 (5/14) Page 4 of 4 Date of Issuance: July 11, 1986 Date Amended: March 30, 2010 Date of Reissuance: July 14, 2017 Description of Type Design Change (continued): G. Cessna 206H and T206H model landplanes with STC SA01878SE, Soloy, LLC installation of Rolls -Royce 250-B17F/2 series engine with a Hartzell Model HC-B3TF-7A/T10173FN(K)-11R Propeller in accordance with Soloy Master Drawing List 766-100, dated September 10, 2008 and maintained in accordance with Maintenance & Overhaul Supplement S2012F, First Edition, Revision 0, dated October 2008, or later FAA approved revisions. • (S/N 206-08001 to present and T206-08001 to present) – AFMS No. 10692, dated March 30, 2010, or later FAA approved revision is required. -END- United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3634SW FAA Form 8110-2 (5/14) Page 5 of 4 ## Every issue (4) - July 14, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3c/46/3c4655b6e0350ef2d2b9cb95d82f8ac3defd98d11cfe32d9ba8d0b12e72d0b1a) - March 30, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/bf/74/bf747759e6b55855cb01345e6f2abe90d92b3ad6dd1a9af270bb1845be7e8dcc) - March 14, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/20/8e/208e3619eb22552b74a1f6a2aa06f1c11a9c878da5d38811df22762066da6f15) - July 21, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c5/34/c5344ee6a7503da6ecd27ae57f4cb54fa430417364fc2a20bb65ec6256a5d7aa) --- 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.