# STC SA02040AK - Type: Supplemental type certificate - Status: Current, Issued - Holder: F Atlee Dodge Aircraft Service, United States - Description: Installation of vented fuel cap assembly (P/N 3267) - Applied: June 18, 1995 - Status date: September 7, 1995 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS A-797](https://openairdocs.org/tcds/A-797), [TCDS A-780](https://openairdocs.org/tcds/A-780), [TCDS A-691](https://openairdocs.org/tcds/A-691), [TCDS 1A2](https://openairdocs.org/tcds/1A2), [TCDS 1A4](https://openairdocs.org/tcds/1A4), [TCDS 1A6](https://openairdocs.org/tcds/1A6) - Certificate PDF: https://openairdocs.org/files/sha256/96/43/9643dbcb624cb19aa204fdca01b29d730ae07bf0b7884a6b135563f734baaf64 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6D80D401BB9912AA86258305004CEE29.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02040AK ## ADs that name it (0) None. ## Approved models (35) - FS 2002 Corp. PA-14 ([TCDS A-797](https://openairdocs.org/tcds/A-797)) - FS 2003 Corp. PA-12 ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - FS 2003 Corp. PA-12S ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - Piper Aircraft Inc. PA-11 ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. PA-11S ([TCDS A-691](https://openairdocs.org/tcds/A-691)) - Piper Aircraft Inc. PA-18 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-125 (Army L-21A) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-20 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20-115 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20-135 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S-115 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S-135 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-22 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-108 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-135 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-135 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) ## 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 Number: SA02040AK This certificate issued to: F. Atlee Dodge Aircraft Services, Inc. Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirement's of part* of the * regulations. Original Product - Type bertificule Number: * *See attached FAA Approved Model List (AML) No. 3267 for list of approved Аваке: * airplane models and applicable Model: airworthiness regulations. Description of Type Design Change: Installation of vented fuel cap assembly (P/N 3267) in accordance with F. Atlee Dodge Aircraft Services, Inc. Installation Instructions as listed on AML No. 3267, or later FAA approved revisions. Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer. A copy of this Certificate and FAA Approved Model List (AML) No. 3267 dated 9-7-95, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft. Date of Application: June 18, 1995 Date Reissued: Date of Issuance: September 07, 1995 Date Amended: FEDERAL AVIATION By Direction of the Administrator Mulla (Signature) Robert L. Miller TOMNISTRATIOT Anchorage Aircraft Certification Office Manager (Title) FAA Form 8110-1(10-68) AML AMEND. DATE N/A N/A N/A N/A N/A N/A ****************************** NUMBER/DATE 8-31-95 8-31-95 8-31-95 8-31-95 8-31-95 8-31-95 (AML) NO. 3267 SERVICES, INC. INSTALLATION OF VENTED FUEL CAP ASS'Y 3267 3267 3267 3267 3267 3267 9-7-95 FAA APPROVED MODEL LIST F. ATLEE DODGE AIRCRAFT FOR (P/N 3267) ORIGINAL ISSUE DATE: CERT. BASIS CAR 4a CAR 3 CAR 3 CAR 3 CAR 3 CAR 3 END **** * * TC # ORIG. A-691 A-780 A-797 1A2 1A4 1A6 A/C MODEL PA-11/-11S PA-12/-12S PA-14 PA-18 SERIES PA-20 SERIES PA-22 SERIES ******************************* A/C MAKE PIPER PIPER PIPER PIPER PIPER PIPER ITEM # ## Every issue (1) - September 7, 1995: Issued, Current. [certificate](https://openairdocs.org/files/sha256/96/43/9643dbcb624cb19aa204fdca01b29d730ae07bf0b7884a6b135563f734baaf64) --- 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.