# STC SA02723CH - Type: Supplemental type certificate - Status: Current, Amended - Holder: D'Shannon Products Ltd., United States - Description: Install D Shannon Products, Ltd. 20-gallon fiberglass auxiliary wing-tip fuel tanks DLB1400, Rev. B dated May 14, 2009, in accordance with Installation Manual KB-1401-1, Rev. A, dated May 14, 2009, or later FAA Approved revision for 4010-lb gross weight normal category operation. - Applied: April 13, 2009 - Status date: September 23, 2011 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15) - Certificate PDF: https://openairdocs.org/files/sha256/12/f2/12f2a784778bbcbccd0e979e2ca175abb23561a770231b782fc64544ae576c97 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB542B094B532F4C8625792C0057081A.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02723CH ## ADs that name it (0) None. ## Approved models (4) - Hawker Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation G36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) ## 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 8110-2-1(10-69) PAGE 1 of 3 PAGES Number SA02723CH This certificate issued to Part 3 of the Civil Air Regulations. Install D’Shannon Products, Ltd. 20-gall on fiberglass auxiliary wing-tip fuel tanks DLB1400, Rev. B dated May 14, 2009, in accordance with Installation Manual KB-1401-1, Rev. A, dated May 14, 2009, or later FAA Approved revision for 4010-lb gross weight normal category operation. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. A copy of this Certificate and Flight Manual Supplement for individual aircraft must be maintained as part of the permanent records for the modified aircraft. 3. Airplanes modified pursuant to this STC must be maintained in accordance with D’Shannon Products, Ltd. Instructions for Continued Airworthiness (ICA) Document No. DP-ICA-1400, Rev. IR., dated 4/10/09 or later FAA accepted revision. Airworthiness Limitations, FAA Approved 7/1/09 are contained within the ICA. 4. 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. (See Continuation Sheet 3) This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. D’Shannon Products, Ltd. 1309 County Road 134 Buffalo, MN 55313 3A15 Make : Hawker Beechcraft Corporation Model : 36, A36, A36TC, G36 Date of application: April 13, 2009 Date of issuance : July 1, 2009 Date amended : September 23, 2011 ( Signature) Timothy Smyth Manager, Propulsion Branch Chicago Aircraft Certification Office ( Title) Limitations and Conditions: (Continued from Page 1 of 3) 5. D’Shannon Products, Ltd. FAA Approved Flight Manual Supplement (FMS), Document No. FMS-DP-36E, Rev. IR dated May 26, 2009 or later FAA approved revision is required for Model 36 and Model A36, S/N E-1 through E-2110 except E-1946 and E-2104. 6. D’Shannon Products, Ltd. FAA Approved Flight Manual Supplement (FMS), Document No. FMS-DP-36L, Rev., IR dated May 26, 2009 or later FAA approved revision, is required for Model A36 and G36, S/N E-1946, E-2104, E-2111 and after. 7. D’Shannon Products, Ltd. FAA Approved Flight Manual Supplement (FMS), Document No. FMS-DP-36TC, Rev., IR dated May 26, 2009 or later FAA approved revision, is required for Model A36TC, S/N EA1 through EA-241, and EA-243 through EA-272. 8. Models 36 and A36, S/N E-1 through E-2110 except E-1946 and E-2104, modified pursuant to this STC must be equipped with the following installations: A. Continental I0-550-B engine per STC SA2200SW B. Cooling Air Baffles per STC SA2200SW or STC SA368CH C. Lower Cowling Access Panels per STC SA414CH D. Gap Seals per STC SA1176SO or SA1416CE 9. Models A36 S/N E-1946, E-2104, and E-2111 & Subsequent; and Models G36 & A36 TC, modified pursuant to this STC must be equipped with the following installations: A. Cooling Air Baffles per STC SA368CH B. Gap Seals per STC SA1176SO or STC SA1416CE …END… ## Every issue (2) - September 23, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/12/f2/12f2a784778bbcbccd0e979e2ca175abb23561a770231b782fc64544ae576c97) - July 1, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/ca/74/ca74a6537a91a1526a90497e3fbe81ff263ce6028ab00d93a324167422fe6af0) --- 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.