# STC SA02722CH - Type: Supplemental type certificate - Status: Current, Issued - 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 - Applied: April 13, 2009 - Status date: July 1, 2009 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS A-777](https://openairdocs.org/tcds/A-777) - Certificate PDF: https://openairdocs.org/files/sha256/e9/10/e910824b0e5c6cdb3b150f85abc2687cbce1525bdb17e3497c46234e153aaff5 - Approved model list and other attachments: [SA02722CH AML.pdf](https://openairdocs.org/files/sha256/00/bb/00bb4925a351ae631e9ed3f0c26ee19c42b10ccdce876d5e271afba200c96c06) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1277F01542D2EC23862576310064B2C3.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02722CH ## ADs that name it (0) None. ## Approved models (34) - Hawker Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - 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 B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation E33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation G36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation V35B ([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. Part * of the * Regulations. Original Product--Type Certificate Number: * * See attached FAA Approved Model Make: * List (AML) No. SA02722CH for list of Model: * approved airplane models and applicable airworthiness regulations . 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. 1. Compatibility of this design change with previous modifications must be determined by the installer. 2. A copy of this Certificate and FAA Approved Model List (AML) No. SA02722CH, 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 the product, the holder shall give the other person written evidence of that permission. D’Shannon Products, Ltd. 1309 County Road 134 Buffalo, MN 55313 Date of application : April 13, 2009 Date of issuance : July 1, 2009 ( Signature) Thaddeus D. Krolicki Jr. Manager, Propulsion Branch Chicago Aircraft Certification Office ( Title) FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES Number ### SA02722CH AML.pdf FAA APPROVED MODEL LIST (AML) NUMBER SA02722CH D'Shannon Products, LTD Issue Date: July 1, 2009 **AIRPLANE AIRPLANE REQUIRED FLIGHT ELIGIBLE INSTALLATION TYPE CERTIFICATE AML** MAKE MODELS MANUAL SUPPLEMENT SERIAL MANUAL CERTIFICATE BASIS AMENDMENT DOCUMENT REV.* DATE* NUMBERS DOCUMENT REV*. DATE* NUMBER DATE NUMBER NUMBER 35 2550 FMS-DP-35 TT IR 5/26/2009 A35, B35 2850 FMS-DP-AB35 TT IR 5/26/2009 C35 2900 FMS-DP-C35 TT IR 5/26/2009 D35 FMS-DP-D35 TT IR 5/26/2009 E35 FMS-DP-E35 TT IR 5/26/2009 F35 2950 G35 2975 H35, J35 3100 FMS-DP-HJ35 TT IR 5/26/2009 K35, M35 3150 FMS-DP-KM35 TT IR 5/26/2009 N35, P35 3325 FMS-DP-NP35 TT IR 5/26/2009 35-33, 35-A33 35-B33, 35-C33 3202 FMS-DP-AF33 TT IR 5/26/2009 E33, F33 G33 3465 FMS-DP-G33 TT IR 5/26/2009 S35 FMS-DP-S35 TT IR 5/26/2009 35-C33A, E33A, E33C V35, V35A V35B F33A, F33C FMS-DP-F33C TT IR 5/26/2009 E-1 thru E-2110 Except E-1946 & E-2104 E-1946, E-2104, E-2111 & Subsq. EA-1 thru EA-272 Except EA-242 FMS-DP-V35AB TT IR 5/26/2009 MAXIMUM GROSS WEIGHT LBS FMS-DP-FG35 TT IR 5/26/2009 FMS-DP-E33C TT IR 5/26/2009 FMS-DP-36TC TT IR 5/26/2009 5/26/2009 FMS-DP-36L TT IR 5/26/2009 FMS-DP-36E TT IR CAR 03 Dated 11/13/1945A-777 KB-1401-01 Rev. A 05/14/09 ALL 3A15 CAR 03 Dated 5/15/1956 CAR 03 Dated 5/15/1956 and amendment 3-8 Hawker Beechcraft 2925 3600 3833 A36TC A36, G36 36, A36 3780 * or later FAA approved revision Sheet 1 of 1 _____________________________ Thaddeus D. Krolicki Jr. Manager, Propulsion Branch Chicago Aircraft Certification Office ## Every issue (1) - July 1, 2009: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e9/10/e910824b0e5c6cdb3b150f85abc2687cbce1525bdb17e3497c46234e153aaff5), [SA02722CH AML.pdf](https://openairdocs.org/files/sha256/00/bb/00bb4925a351ae631e9ed3f0c26ee19c42b10ccdce876d5e271afba200c96c06) --- 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.