# STC SA00908NY - Type: Supplemental type certificate - Status: Current, Amended - Holder: Maple Leaf Aviation Ltd, Canada - Description: Installation of Fiberglass stabilator tips. - Applied: July 30, 1998 - Status date: December 13, 2018 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE) - Certificate PDF: https://openairdocs.org/files/sha256/47/54/4754f4e895a825ab870840f8a9e3d668f74c6a5cb6a009904ebabe2887b25c97 - Approved model list and other attachments: [SA00908NY_AML.pdf](https://openairdocs.org/files/sha256/2d/c6/2dc6a6a50d02ba1bdd400b18e48bb6669e9ea6a2efa84c4dd98f62b4333c8729) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/69955FFB3940E8DF86258366005DD859.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00908NY ## ADs that name it (0) None. ## Approved models (4) - The Cessna Aircraft Company 177 ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) - The Cessna Aircraft Company 177A ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) - The Cessna Aircraft Company 177B ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) - The Cessna Aircraft Company 177RG ([TCDS A20CE](https://openairdocs.org/tcds/A20CE)) ## 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 Supplemental Type Certificate IMPORT Number: SA00908NY Maple Leaf Aviation Ltd. This certificate issued to: Group 520, Box 16, RR5 Brandon, Manitoba Part 23 of the Federal Aviation Regulations. Original Product - Type Certificate Number: Make: *See attached FAA Approved Model List (AML) **See attached FAA Approved Model List (AML) Model: *See attached FAA Approved Model List (AML) No. SA00908NY for a list of approved models and applicable airworthiness regulations. 1. Installation of Fiberglass Stabilator Tips in accordance with Maple Leaf Aviation Ltd. Master Drawing List Report No. 177-0960200, dated December 10, 1997, TCCA approved on July 24, 1998, or later TCCA approved revision as listed on the 2. Installation of Upper and Lower Fiberglass Tail Cone sections in accordance with Maple Leaf Aviation Ltd. Modification Data Approved Model List (AML) Number SA00908NY. Summary Report No. MLA1013-MDS, Rev. NI, dated February 3, 2011, TCCA approved on April 12, 2011, or later TCCA approved revision as listed on the Approved Model List (AML) Number SA00908NY. Description of Type Design Change: Continued on Page 3 of 3) Limitations and Conditions: 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. 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. Limitations and Conditions: Continued on Page 3 of 3) Date of Application: July 30, 1998 Date Reissued: Date of Issuance: November 6, 1998 Date Amended: December 13, 2018 By Direction of the Administrator Anthony E. Gallo Manager, New York ACO Branch transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of this Supplemental Type This certificate may be Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. Page 1 of 3 FAA Form 8110-2 (5/14) United States of America Department of Transportation Federal Aviation Administration TINISTRA Supplemental Type Certificate Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA00908NY To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): This certificate may be transterred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The ST's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. FAA Form 8110-2 (5/14) Page 2 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00908NY Date Amended: December 13, 2018 Description of Type Design Change: (continued): 3. Maintenance of the Upper and Lower Fiberglass Tail Cone sections must be in accordance with TCCA accepted Maple Leaf Aviation Ltd. Instructions for Continued Airworthiness MLA 1013-ICA, Rev. NI, dated February 03, 2011, or later TCCA accepted revision as listed on the Approved Model List (AML) Number SA00908NY. Limitations and Conditions: (continued): Certification Basis: Based on 14 CFR §$ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the modified Textron 177, 177A, 177B series models and Textron 177RG is as follows: (a) For parts not changed or not affected by the change: The existing type certification basis for the aircraft models as shown on the respective FAA Type Certificate Data Sheets: A13CE and A20CE. (b) For parts changed or affected by the change: As specified in the Approved Model List (AML) Number SA00908NY. ------END----- FAA Form 8110-2 (5/14) Page 3 of 3 ### SA00908NY_AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. ПТЕМ Company) Aircraft Cessna (former Aviation Textron Company) Aircraft Cessna (tormer Aviation Textron MAKE 177RG 177B 177A 177 Series Model/ A20CE AI3CЕ TCDS Page 1 of 1 approved revision. §23.1529 at Amdt.23-26 plus: 12, 2011, or later TCCA Amdt.23-1 through 23-6, TCCA approved on April 14 CFR part 23, dated February 3, 2011, MLA1013-MDS, Rev. NI, Summary Report No. Tail Cone Sections: and Lower Fiberglass Modification Data Installation of Upper Maple Leaf Aviation Ltd. TCCA approved revision. on July 24, 1998, or later Per TCDS A20CE 10, 1997, TCCA approved Tip: 0960200, dated December Fiberglass Stabilator MDL Report No. 177- Maple Leaf Aviation Ltd. Installation of §23.1529 at Amdt.23-26 approved revision. plus: 12, 2011, or later TCCA Amdt.23-1 through 23-6. TCCA approved on April 14 CFR part 23, dated February 3, 2011, MLA1013-MDS, Rev. NI, Summary Report No. Tail Cone Sections: Modification Data and Lower Fiberglass Maple Leaf Aviation Ltd. Installation of Upper TCCA approved revision. Per TCDS A13CE on July 24, 1998, or later 10, 1997, TCCA approved Tip: 0960200, dated December MDL Report No. 177- Fiberglass Stabilator Installation of Maple Leat Aviation Ltd. Alteration tor MDL/Inst. DWG Certification Basis Installation of Fiberglass Plastic Stabilator Tips and Tail Cone Sections Maple Leaf Aviation Limited FAA APPROVED MODEL LIST (AML) NUMBER SA00908NY FAA Approved: _ TCCA accepted revision. NI, dated February 03, 2011, or later Airworthiness MLA1013-ICA, Rev. Ltd. Instructions for Continued TCCA accepted Maple Leaf Aviation Maintenance in accordance with N/A TCCA accepted revision. NI, dated February 03, 2011, or later Airworthiness MLA1013-ICA, Rev. Ltd. Instructions for Continued TCCA accepted Maple Leaf Aviation Maintenance in accordance with NA ICA Compliance & Airworthiness Division Manager, New York ACO Branch Anthony E. Gallo Notes Model Specific December 13, 2018 N.A. December 13,2018 N.A. Amended Date November 6, 1998 Issue Date Original ## Every issue (1) - December 13, 2018: Amended, Current. [certificate](https://openairdocs.org/files/sha256/47/54/4754f4e895a825ab870840f8a9e3d668f74c6a5cb6a009904ebabe2887b25c97), [SA00908NY_AML.pdf](https://openairdocs.org/files/sha256/2d/c6/2dc6a6a50d02ba1bdd400b18e48bb6669e9ea6a2efa84c4dd98f62b4333c8729) --- 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.