# STC SA02460CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: D'Shannon Products Ltd., United States
- Description: Install Genesis Aero, LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanks
- Applied: June 5, 2007
- Status date: November 19, 2012
- Product: Aircraft, Small Airplane
- 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/sha256/2a/bd/2abd82c0022d6e2f3a29725b3fc4a0210ec23393fd28142cc70bd731fa99c4bd
- Approved model list and other attachments: [SA2460CH_AML.pdf](https://openairdocs.org/files/sha256/48/43/48433fa126d76197c0023e87984b1933e7d644253ffe2cbe12c59b3260edb611)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FA86D6364F062B4586257AD1006441DC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02460CH

## 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. SA02460CH for list of

Model: * approved airplane models and applicable airworthiness regulations .

Install Genesis Aero, LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanks DBL1400, Rev. D dated April 1, 2007, in accordance with Installation Manual KB-1401, Rev. I, dtd. April 1, 2007 and optional JVE, Inc. Vortex Generators JVE-500 in accordance with STC SA09074SC, and Drawing List JVE-500, Rev. 2, dtd. August 21, 1995, 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. SA02460CH, 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 Genesis Aero, LLC. Instructions for Continued Airworthiness Document No. ICA-20TT, Rev. 0., dated 07/05/07 or later FAA-accepted revision.

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 reissued : August 2, 2007, June 6, 2011, November 19, 2012 Date amended :

By direction of the Administrator Original Signed By:

Timothy Smyth

( Signature) Timothy Smyth Manager, Propulsion and Program Management Branch Chicago Aircraft Certification Office

( Title)

Date of application : June 5, 2007

Date of issuance : August 1, 2007

### SA2460CH_AML.pdf

FAA APPROVED MODEL LIST (AML) NUMBER SA02460CH Genesis Aero, LLC Issue Date: August 1, 2007

**AIRPLANE AIRPLANE MAXIMUM REQUIRED FLIGHT ELIGIBLE INSTALLATION TYPE CERTIFICATE AML**

MAKE MODELS GROSS WEIGHT MANUAL SUPPLEMENT SERIAL MANUAL CERTIFICATE BASIS AMENDMENT LBS DOCUMENT REV.* DATE* NUMBERS DOCUMENT REV.* DATE* NUMBER DATE

NUMBER NUMBER Raytheon 35 2550 FMS-20TT-35 IR 7/14/2007 ALL KB-1401 Rev. I 04/01/07 A-777 CAR 03 (Beech) A35, B35 2850 FMS-20TT-AB35 IR 7/14/2007 ALL Dated C35 2900 FMS-20TT-C35 IR 7/14/2007 ALL 11/13/45 D35 2925 FMS-20TT-D35 IR 7/14/2007 ALL E35 2925 FMS-20TT-E35 IR 7/14/2007 ALL F35 2950 G35 2975 FMS-20TT-FG35 IR 7/14/2007 ALL Hawker H35, J35 3100 FMS-20TT-HJ35 IR 7/14/2007 ALL 3A15 CAR 3 Beechcraft K35, M35 3150 FMS-20TT-KM35 IR 7/14/2007 ALL Dated N35, P35 3325 FMS-20TT-NP35 IR 7/14/2007 ALL 5/15/1956 35-33, 35-A33 3202 KB-1401 Rev. I 04/01/07 3A15 CAR 3 35-B33, 35-C33 FMS-20TT-AF33 A 6/30/2008 ALL Dated 7/16/2008 E33, F33 5/15/1956 G33 3465 FMS-20TT-G33 IR 7/14/2007 ALL KB-1401 Rev. I 04/01/07 3A15 CAR 3 S35 3550 FMS-20TT-S35 IR 7/14/2007 ALL Dated 3600 FMS-20TT-S35-1 IR 7/14/2007 ALL KB-1401 Rev. I 04/01/07 5/15/1956 JVE-0494 Rev. I 12/21/95 35-C33A, 3550 FMS-20TT-E33C IR 7/14/2007 ALL KB-1401 Rev. I 04/01/07 E33A, E33C 35-C33A, 3600 FMS-20TT-E33C-1 IR 7/14/2007 ALL KB-1401 Rev. I 04/01/07 E33A, E33C JVE-0494 Rev. I 12/21/95 V35, V35A 3550 FMS-20TT-V35AB IR 7/14/2007 D-7977 thru KB-1401 Rev. I 04/01/07 V35B D-9947 V35B FMS-20TT-V35B-1 IR 7/14/2007 D-9948 & Subsq.

* or later FAA approved revision Page 1 of 2

FAA APPROVED MODEL LIST (AML) NUMBER SA02460CH Genesis Aero, LLC Issue Date: August 1, 2007

**AIRPLANE AIRPLANE MAXIMUM REQUIRED FLIGHT ELIGIBLE INSTALLATION TYPE CERTIFICATE AML**

MAKE MODELS GROSS WEIGHT MANUAL SUPPLEMENT SERIAL MANUAL CERTIFICATE BASIS AMENDMENT LBS DOCUMENT REV.* DATE* NUMBERS DOCUMENT REV.* DATE* NUMBER DATE

NUMBER NUMBER Hawker F33A 3550 FMS-20TT-F33AC IR 7/14/2007 CE-290 thru KB-1401 Rev. I 04/01/07 3A15 CAR 03 Beechcraft CE-673 Dated F33C CJ-26 thru 5/15/1956 CJ-128 F33A FMS-20TT-F33AC-1 IR 7/14/2007 CE-674 & Subsq.

F33C CJ-129 & Subsq.

V35, V35A 3600 FMS-20TT-V35AB-1 IR 7/14/2007 ALL V35B F33A, F33C FMS-20TT-F33AC-2 IR 7/14/2007 ALL 36, A36 3780 FMS-20TT-36E IR 7/14/2007 E-1 thru E-2110 Except E-1946, & E-2104 A36, G36 3833 FMS-20TT-36L IR 7/14/2007 E-1946, E-2104, E-2111, & Subsq.

A36TC 3833 FMS-20TT-36TC IR 7/14/2007 EA-1 thru CAR 03 EA-272 Dated Except 5/15/1956 and EA-242 amendment 3-8 * or later FAA approved revision Original Signed By:

Timothy Smyth Timothy Smyth Manager, Propulsion and Program Management Branch Chicago Aircraft Certification Office Date Amended: 7/16/2008 Date Re-issued: 6/6/2011, 11/19/2012 Page 2 of 2

## Every issue (2)

- November 19, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2a/bd/2abd82c0022d6e2f3a29725b3fc4a0210ec23393fd28142cc70bd731fa99c4bd), [SA2460CH_AML.pdf](https://openairdocs.org/files/sha256/48/43/48433fa126d76197c0023e87984b1933e7d644253ffe2cbe12c59b3260edb611)
- June 6, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/af/60/af60c679f54917a62700f5ba319dcd828a833cf89e2dcad6659a0542cb9954c7), [sa02460ch.pdf](https://openairdocs.org/files/sha256/aa/d0/aad062b49ee8b161dba9239b06ed16684c8b066da927cfbfe534b6a8fc31281c)

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