# STC SA3318NM - Type: Supplemental type certificate - Status: Current, Amended - Holder: Venting Engineering, United States - Description: Installation of a Venting fuel cap and restricting adapter assembly. - Applied: October 23, 1985 - Status date: June 23, 1988 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS A9CE](https://openairdocs.org/tcds/A9CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21) - Certificate PDF: https://openairdocs.org/files/sha256/02/e7/02e76a50e6de5a468f6d43812332a4f7bb160674ca61da7a8a619a7398cee0f7 - Approved model list and other attachments: [SA3318NM AML.pdf](https://openairdocs.org/files/sha256/cd/b2/cdb2df18512cb5ed478c8c6abce5dee49763e05ad5bb1a4cb074aa69c289e5d4) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B53184B0AFF91B7285256CC2000A96C7.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA3318NM ## ADs that name it (0) None. ## Approved models (17) - The Cessna Aircraft Company 177 ([TCDS A13CE](https://openairdocs.org/tcds/A13CE)) - The Cessna Aircraft Company 177RG ([TCDS A20CE](https://openairdocs.org/tcds/A20CE)) - The Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - The Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - The Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company 188 ([TCDS A9CE](https://openairdocs.org/tcds/A9CE)) - The Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - The Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE)) - The Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE)) - The Cessna Aircraft Company 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) - The Cessna Aircraft Company 208A ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) - The Cessna Aircraft Company 210 ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company P206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - The Cessna Aircraft Company P210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - The Cessna Aircraft Company U206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) ## 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 5A331811 This certificate issued to: Venting Engineering, Ltd. Surt * of the * Fregulations Original Product - Type Certificate Lumber * *See attached Approved Model List (AML) Maki * No. SA3318NM for list of approved airplane models and applicable Model: * airworthiness regulations. Description of Type Design Change: Installation of a Venting Engineering, Ltd. fuel cap and restricting adapter assembly (Part No. 575-010) in accordance with Venting Engineering, Ltd. Installation Instructions No. 575-1000, dated October 23, 1985, or later FAA approved revisions. TOTE 1. This modification is a replacement for Cessna fuel cap (Part No. C156001-0106). 2. This cap assembly complies with AD 79-10-14 as per amendment 39-5901, dated 5/30/88. 3. This installation applies only to those aircraft models listed in the AML that were originally eligible for the Wisco red plastic fuel cap (Cessna P/N C-156001). Limitations and Conditions: Approval of this change in type design applies to the above model aircraft 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 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 Approved Model List (AML) shall be maintained as part of the permanent records for the modified aircraft. Tutespapplication: October 23, 1985 Date Reissued: Interfissance: January 31, 1986 Date Amended: June 23, 1988 FEDERAL AVIATION By Direction of the Administrator TOMINIST RANDO Assistant Manager, Seattle Aircraft Certification Office (Title) ### SA3318NM AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. **VENTING ENGINEERING, LTD.** **APPROVED MODEL LIST (AHL) NO. SA3318NM FOR** **VENTING ENGINEERING FUEL CAP AND** RESTRICTING ADAPTER ASSEMBLY Issue Date: January 31, 1986 **FAA SEALED** **ORIGINAL CERTIFICATION DRAWING/** TYPE BASIS DRAWING LIST AFM MEL AIRCRAFT AIRCRAFT CERTIFICATE FOR REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION NUMBER AND DATE NUMBER/DATE DATE Cessna 177 A13CE Part 3 of Civil Air 575-010 12/10/86 Regulations and T.C. 2 Cessna 177RG A20 CE 575-010 12/10/86 3 Cessna 180 5A6 575-010 12/10/86 4 Cessna 182 3A13 575-010 12/10/86 5 Cessna R1 82 3A13 575-010 12/10/86 6 Cessna 182A 3A13 575-010 12/10/86 7 Cessna 185 3A24 575-010 12/10/86 8 Cessna 188 AOCE 575-010 12/10/86 9 Cessna 205 3A21 575-010 12/10/86 10 Cessna 206 A4 CE 575-010 12/10/86 11 Cessna U206 A4 CE 575-010 12/10/86 12 Cessna P206 A4 CE 11 575-010 12/10/86 Page 1 of 2 **VENTING ENGINEERING, LTD.** **APPROVED MODEL LIST (AHL) NO. SA3318NM FOR** **VENTING ENGINEERING FUEL CAP AND** RESTRICTING ADAPTER ASSEMBLY Issue Date: January 31, 1986 **FAA SEALED** **ORIGINAL CERTIFICATION DRAWING/** TYPE BASIS DRAWING LIST AFM MEL AIRCRAFT AIRCRAFT CERTIFICATE FOR REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION NUMBER AND DATE NUMBER/DATE DATE 13 Cessna 207 A16CE Part 3 of Civil Air 575-010 12/10/86 Regulations and T.C. 14 Cessna 207A A16CE 575-010 12/10/86 15 Cessna 208 A37CЕ 575-010 12/10/86 16 Cessna 208A A37 CE 575-010 12/10/86 17 Cessna 210 3A21 575-010 12/10/86 18 Cessna P21ON 3421 575-010 12/10/86 FAA Approved: 0.7. Cragi Assistant Manager, Seattle Aircraft Certification Office Date: June 23, 1988 Page 2 of 2 ## Every issue (1) - June 23, 1988: Amended, Current. [certificate](https://openairdocs.org/files/sha256/02/e7/02e76a50e6de5a468f6d43812332a4f7bb160674ca61da7a8a619a7398cee0f7), [SA3318NM AML.pdf](https://openairdocs.org/files/sha256/cd/b2/cdb2df18512cb5ed478c8c6abce5dee49763e05ad5bb1a4cb074aa69c289e5d4) --- 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.