# STC SA01561CH - Type: Supplemental type certificate - Status: Current, Reissued - Holder: D'Shannon Products Ltd., United States - Description: Installation of Hartzell Model PHC-(C, L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Teledyne Continental Motors six-cylinder engines - Applied: April 30, 2001 - Status date: May 18, 2023 - Product: Aircraft, Small Airplane - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS 5A3](https://openairdocs.org/tcds/5A3), [TCDS A-777](https://openairdocs.org/tcds/A-777) - Certificate PDF: https://openairdocs.org/files/sha256/a2/71/a271b579a6bda05acc928181a702e4830d8f2353c30bcc165798ce106f07bac2 - Approved model list and other attachments: [SA01561CH_ AML.pdf](https://openairdocs.org/files/sha256/14/d5/14d53e3b4b894f8357dfb125efd52667eeb8acc6e1214403176c00ae55f4e0c2) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182136244520230601142128.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01561CH ## ADs that name it (0) None. ## Approved models (33) - 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 A45 (Military T-34A; B-45) ([TCDS 5A3](https://openairdocs.org/tcds/5A3)) - 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 D45 (Military T-34B) ([TCDS 5A3](https://openairdocs.org/tcds/5A3)) - 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 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 This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration TAIN STRATO Supplemental Type Certificate Number: SA01561CH This certificate issued to: D'Shannon Products, Ltd. 1309 County Road 134 Buffalo, MN 55313 * of _the * Regulations Type Certificate Number: Original Product *See Approved Model List Make: *See Approved Model List Description of Type Design Change: Model: *See Approved Model List Installation of Hartzell Model PHC-(C, L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Teledyne Continental Motors six-cylinder engines in accordance with D'Shannon Products Installation Instructions as listed on AML No. SA01561CH, or later FAA approved revision. 1. Compatibility of this design change with previously approved modifications must be determined by the installer. (See Continuation Sheet 3 of 3) Aviation Administration. suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Paul (Vu) Nygen Title: Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service Modification is limited to aircraft that have been converted by D'Shannon Products STCs SA1-569, SA2361SW, and Black Aviation, Inc. STC SA1864SW, T-34 Mentors, LLC STC SA1450SW, or Western Skyways, Inc. STC SA8676SW/SE8677SW. 3. FAA approved Airplane Flight Manual Supplement FMS-F8068-2, Rev. 2, dated April 20, 2023 or later FAA approved revision is required. Refer to FMS-F8068-2 for eligible hub applications. 4. Eligible engines: Teledyne Continental Motors IO-470-J, -K, -C, and -N, 10-520-B, -BA, -BB, TSIO-520-D, -DB and IO-550-B (limited to 285 hp). 5. Check aircraft Weight and Balance. 6. A copy of this certificate and FAA Approved Model List (AML) No. SA01561CH, dated September 3, 2003, or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft. 7. 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. - END - (14 CFR 21.47). This FAA Form 8110-2 (03/21) Page 3 of 3 ### SA01561CH_ AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. FAA APPROVED MODEL LIST (AML) NO. SA01561CH D' Shannon Products FOR Installation of Hartzell Model PHC-(C,L)YF-1RF/F8068 (-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Teledyne Continental six-cylinder engines Date Issued: October 25, 2001 Date Amended: September 3, 2003 Date Reissued: March 7, 2011, June 17, 2011 **INSTALLATION** **ORIGINAL INSTRUCTIONS** **TYPE CERTIFICATION AFM AML** AIRCRAFT AIRCRAFT CERTIFICATE BASIS FOR NO ISION SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION NUMBER NO. NO. / DATE DATE DATE 1 Raytheon A35, B35, C35, D35, A-777 CAR 3 DSP- Initial FMS-F8068-2 Aircraft E35, F35, G35 043001B Release Initial Company Dated Release (Beech) 4/30/2001 Dated or later 4/30/2001 FAA or later approved FAA revisior approved revision 2 Raytheon N35, 335, 535, M35, ЗА15 CAR 3 DSP- Initial FMS-F8068-2 Aircraft N35, S35, 043001B Release Initial Company 35-33, Dated Release (Beech] 4/30/2001 Dated 35-C33, or later 4/30/2001 Е33, ЕЗЗА, Е33С, FAA or later 833; 533 and A56 approved FAA revision approved revision Raytheon A45 (T-34A, B-45), 5АЗ CAR 3 DS₽- FMS-F8068-2 9/3/2003 Aircraft 045 (T-34B) 043001B Dated Rev. compani 7/1/2003 Dated Beech or later 7/1/2003 or FAA later FAA approved approved revision revision FAA Approved: Chicago Aircraft Certification Office imothy Smyepulsion Branch Page 1 of 1 ## Every issue (3) - May 18, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a2/71/a271b579a6bda05acc928181a702e4830d8f2353c30bcc165798ce106f07bac2), [SA01561CH_ AML.pdf](https://openairdocs.org/files/sha256/14/d5/14d53e3b4b894f8357dfb125efd52667eeb8acc6e1214403176c00ae55f4e0c2) - June 17, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/38/69/3869b465b806fdc76aea77877e7a15fae464aac6d92ff03e0d2577c62507b2b4), [SA01561.AML.pdf](https://openairdocs.org/files/sha256/f6/5a/f65a8c08ca4491e6c6123e41f0b33139e967bb8823f80aa6dff33a3220369562) - March 7, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/65/9f/659f4737c7a43a1b1df7fe29b1cd8bc31acf5ea9e77cc5cdc262cbb326c5d6d9), [SA01561CH AML.pdf](https://openairdocs.org/files/sha256/c2/8d/c28d4783f960e1b93cd8495a8a3380b13678a7befa4287f63e4f09814a933c4f) --- 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.