# STC SA00864SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Selkirk Aviation, United States - Description: Installation of fiberglass nosebowl. - Applied: July 2, 1999 - Status date: May 20, 2010 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6) - Certificate PDF: https://openairdocs.org/files/sha256/f1/cd/f1cd335df6cd547977318ecdc6e35b5ebf553f1429d662a21e0969767e4771cf - Approved model list and other attachments: [SA00864SE.pdf](https://openairdocs.org/files/sha256/90/b9/90b9abc89a142eed7d9db04b0ddf458b575c49b1c02627ea859e570cb00d6f7a) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5AB2EA6805973D2D8625773D004AC8FF.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA00864SE ## ADs that name it (0) None. ## Approved models (37) - Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company 210B ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - Cessna Aircraft Company 210C ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - Cessna Aircraft Company 210D ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) ## 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 APPROVED MODEL LIST (AML) NO. SA00864SE SELKIRK AVIATION, INC.** FIBERGLASS NOSEBOWLS ISSUE DATE: January 3, 2001 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL ORIGINAL TYPE** **CERTIFICATE NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED DRAWING** NUMBER REVISION and DATE AML AMENDMENT DATE 1 CESSNA 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR 3 and TCDS 5A6 Master Drawing List: SA-40-00 Revision E, dated 5/10/02 8/29/02 2 CESSNA 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P 3A13 CAR 3 and TCDS 3A13 Master Drawing List: SA-40-00 Revision E, dated 5/10/02 8/29/02 3 CESSNA 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 CAR 3 and TCDS 3A24 Master Drawing List: SA-40-00 Revision E, dated 5/10/02 8/29/02 4 CESSNA 210B, 210C, 210D 3A21 CAR 3 and TCDS 3A21 Master Drawing List: SA-40-00 Revision E, dated 5/10/02 8/29/02 Amended: August 29, 2002 FAA Approved: Acting Manager, Seattle Aircraft C e r t i f i c a t i o n O f f i c e ### SA00864SE.pdf United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA00864SE This certificate, issued to Selkirk Aviation 3377 West Industrial Loop Coeur d’Alene, ID 83815 certifies that the change in the type design for th e following product with the limitations and conditions therefor as specified hereon meets th e airworthiness requirements of Part * of the * Regulations. Original Product⎯Type Certificate Number: *See attached FAA-approved Model List (AML) Make: No. SA00864SE for a list of approved airplane Model: models and applicable airworthiness regulations. Description of the Type Design Change: Manufacure and installation of fiberglass nosebowl in accordance with Selkirk Aviation Approved Model List SA00864SE dated August 29, 2002 or later FAA-approved revision. Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed on the AML only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and FAA-approved Model List (AML) No. SA00864SE must be maintained as part of the permanent records for the modified aircraft. 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. 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. Date of application: July 2, 1999 Date reissued: May 20, 2010 Date of issuance: January 3, 2001 Date amended: September 6, 2002 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred in accordance with FAR 21.47. FAA FORM 8110-2(10-68) By direction of the Administrator _________ _________ (Signature) ____ Acting Manager, Seattle Aircraft Certification Office___ (Title) ## Every issue (1) - May 20, 2010: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f1/cd/f1cd335df6cd547977318ecdc6e35b5ebf553f1429d662a21e0969767e4771cf), [SA00864SE.pdf](https://openairdocs.org/files/sha256/90/b9/90b9abc89a142eed7d9db04b0ddf458b575c49b1c02627ea859e570cb00d6f7a) --- 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.