# STC SA02249SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: CarpenterDev, LLC, United States - Description: Installation of a silicone rubber wingtip device intended as a provision for mounting battery powered devices such as strobes or air temperature sensor - Applied: March 9, 2012 - Status date: September 18, 2013 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO) - Certificate PDF: https://openairdocs.org/files/sha256/df/45/df458fb50feb5f32f86bb04e5fa5ea05e718556b8c5ebcb5efb8d633625b25f8 - Approved model list and other attachments: [AML_SA02249SE.pdf](https://openairdocs.org/files/sha256/ef/07/ef07e885654b17d459dccde473e48eb04616f89b3bb8086f2d32775f0c95b91e) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0CAF628F31D7918086257BF1005254DF.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA02249SE ## ADs that name it (0) None. ## Approved models (72, first 50) - Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172C ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172H (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172R ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - Cessna Aircraft Company 172S ([TCDS 3A12](https://openairdocs.org/tcds/3A12)) - 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 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182S ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company T182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company T182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company TR182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-235 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) All 72: https://openairdocs.org/stc/SA02249SE/models.md ## 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. Number SA02249SE This certificate, issued to CarpenterDev, LLC 21012 NE 36th St Sammamish, WA 98074 Part * of the * Regulations. Original ProductType Certificate Number: * See attached Federal Aviation Administration (FAA) Make: Approved Model List (AML) SA02249SE for approved Model: aircraft models and applicable airworthiness regulations Description of the Type Design Change: Installation of a silicone rubber wingtip device intended as a provision for mounting battery powered devices such as strobes or air temperature sensor in accordance with CarpenterDev Installation Instructions 10000, Revision 002, dated May 12, 2012, and Installation Guide CDEV-002, dated October 22, 2012, or later Federal Aviation Administration (FAA) approved revisions . Fabrication controlled by CarpenterDev Drawing Part Number 10001, Revision 04, Sheets 1 and 2, dated May 12, 2012, or later FAA-approved revision. Maintained in accordance with CarpenterDev Instructions for Continued Airworthiness (ICA) CDEV-003 or later FAA-accepted revision. Limitations and Conditions: Approval of this change in type design applies to the aircraft listed on AML SA02249SE only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, the AML, Installation Instructions, Installation Guide, and ICA must be maintained as part of the permanent records for the modified aircraft. Date of application: March 9, 2012 Date reissued: June 10, 2013 Date of issuance: December 5, 2012 Date amended: September 18, 2013 (Signature) Manager, Seattle Aircraft Certification Office (Title) Number SA02249SE CarpenterDev, LLC Issued: December 5, 2012 Reissued: June 10, 2013 Amended: September 18, 2013 The equipment listed in the Accepted Equipment List (AEL), document CDEV-013, Rev. 001, dated August 21, 2013, or later FAA-accepted AEL, has been found acceptable for installation in this application. Equipment providing flight guidance information including attitude, altitude, heading, navigation, angle of attack, or speed information cannot be installed without separate FAA approval. It is the responsibility of the pilot-in-command to ensure that equipment installed per this STC does not interfere with the proper operation of any required aircraft systems. The certification basis for this modification is based upon Part 3 of Civil Air Regulations as listed in AML SA02249SE. 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 - ### AML_SA02249SE.pdf **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA02249SE FOR** INSTALLATION OF A SILICONE RUBBER WINGTIP DEVICE ISSUE DATE: December 5, 2012 Page 1 of 2 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED AIRCRAFT** **INSTALLATION MANUAL** **FAA APPROVED** MASTER DRAWING LIST AML REV DATE Number Revision* Drawing Revision* 1. Cessna 172; 172A; 172B; 172C; 172D; 172E; 172F (USAF T-41A); 172G; 172H (USAF T-41A); 172I; 172K; 172L; 172M; 172N; 172P; 172Q; 172R; 172S 3A12 CAR 3 CarpenterDev Installation Instructions 10000 Revision 002, dated 5/12/12 Part Number 10001 Installation Guide CDEV-002 dated 10/22/12 2. Cessna 182; 182A; 182B; 182C; 182D; 182E; 182F; 182G; 182H; 182J; 182S; 182T; 182K; 182L; 182M; 182N; 182P; 182Q; 182R; R182; T182; TR182; T182T 3A13 CAR 3 CarpenterDev Installation Instructions 10000 Revision 002, dated 5/12/12 Part Number 10001 Installation Guide CDEV-002 dated 10/22/12 3. Piper Aircraft, Inc. PA-28-140, PA-28-151, PA-28-150, PA-28-161, PA-28-160, PA-28-181, PA-28-180, PA-28R-201, PA-28-235, PA-28R-201T, PA-28S-160 2A13 CAR 3 CarpenterDev Installation Instructions 10000 Revision 002, dated 5/12/12 Part Number 10001 004 Installation Guide CDEV-002 dated 10/22/12 **FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA02249SE FOR** INSTALLATION OF A SILICONE RUBBER WINGTIP DEVICE ISSUE DATE: December 5, 2012 Page 2 of 2 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TC NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **FAA APPROVED AIRCRAFT** **INSTALLATION MANUAL** **FAA APPROVED** MASTER DRAWING LIST AML REV DATE Number Revision* Drawing Revision* 3. Cont. Piper Aircraft, Inc. PA-28-236, PA-28S-180, PA-28RT-201, PA-28R-180, PA-28RT-201T, PA-28R-200, PA-28-201T 2A13 CAR 3 CarpenterDev Installation Instructions 10000 Revision 002, dated 5/12/12 Part Number 10001 004 Installation Guide CDEV-002 dated 10/22/12 4. Piper Aircraft, Inc. PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32-301FT, PA-32-301XTC, PA-32R-301 (SP), PA-32R-301 (HP), PA-32R-301T, PA-32-301, PA-32-301T A3SO CAR 3 CarpenterDev Installation Instructions 10000 Revision 002, dated 5/12/12 Part Number 10001 Installation Guide CDEV-002 dated 10/22/12 * Or later FAA Approved Revision FAA Approved: Acting Manager, Seattle Aircraft Certification Office AMENDED: REISSUED: June 10, 2013 ## Every issue (3) - September 18, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/df/45/df458fb50feb5f32f86bb04e5fa5ea05e718556b8c5ebcb5efb8d633625b25f8), [AML_SA02249SE.pdf](https://openairdocs.org/files/sha256/ef/07/ef07e885654b17d459dccde473e48eb04616f89b3bb8086f2d32775f0c95b91e) - June 10, 2013: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a7/9d/a79d6bbd7b113b3a88a3217b3222ff627ca6534c2a9f42361cb5c14623bd0c5b), [AML_SA02249SE.pdf](https://openairdocs.org/files/sha256/8e/a5/8ea5fc1b10ffb45f3e41ce7fb1e6ca46003c2bb2853d16a2ba8b3e1115d45e52) - December 5, 2012: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/70/63/7063fa88a67b76f820e047555d8821437e02c4ebea294168585ad6b65ff97f97), [AML SA02249SE.pdf](https://openairdocs.org/files/sha256/81/92/81926693ec8933c960397632df8ef9196fbe9c82ad7605ba80fcd18ff5c56dfd) --- 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.