# STC SA2069NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Kenmore Air Harbor LLC, United States - Description: Installation of Continental IO-520 series engine modified per STC SE2068NM or Continental O-470-U engine modified per STC SE2107NM. - Applied: October 11, 1982 - Status date: April 5, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS 5A6](https://openairdocs.org/tcds/5A6) - Certificate PDF: https://openairdocs.org/files/sha256/18/1c/181c332876dde762c686dc964f9043d8b6bb2c2f63497333670e5a679996e65d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/153B21C266737F58862585CE0055E3DB.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA2069NM ## ADs that name it (0) None. ## Approved models (4) - The Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) ## 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 SA2069NM This certificate, issued to Kenmore Air Harbor, LLC. 6321 NE 175th Street Kenmore, WA 98028 Part 3 of the Civil Air Regulations. Original ProductType Certificate Number: 5A6 Make: Cessna Model: 180G, 180H, 180J, and 180K Description of the Type Design Change: Installation of Continental IO-520 Series engine modified per STC SE2068NM or Continental 0-470-U engine modified per STC SE2107NM in accordance with Kenmore Air Harbor, Inc. Installation Instructions No. K13149, dated April 12, 1983, or later FAA-approved revisions. Limitations and Conditions: Approval of this change in type design applies to the above aircraft model 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 Addendum No. SA2069NM and Kenmore Air Harbor, Inc. Installation Instructions K13149, or later FAA-approved revision shall 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. Date of application: October 11, 1982 Date reissued: April 5, 2019 Date of issuance: December 7, 1980 Date amended: August 26, 1994 FAA FORM 8110-2 (5/14) PAGE 1 OF 4 PAGES By direction of the Administrator (Signature) Acting Manager, Seattle ACO Branch (Title) Transfer the ownership of Supplemental Type Certificate Number to (Name of Transferee) (Address of Transferee) (Number and Street) (City, State, and ZIP Code) from (Name of Grantor) (Print or Type) (Address of Grantor) (Number and Street) (City, State, and ZIP Code) Signature of Grantor (In Ink): U.S. GPO: 1987-763-289 Number SA2069NM Kenmore Air Harbor, LLC. Issued: December 7, 1980 Reissued: April 5, 2019 Amended: August 26, 1994 **SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA2069NM** The conditions and limitations of Type Certificate Data Sheet No. 5A6 apply except where superseded by the following: This Addendum, which is part of the Supplemental Type Certificate No. SA2069NM, prescribes the conditions and limitations under which the STC was issued and meets the airworthiness requirements of Civil Air Regulations Part 3. A copy of this Addendum shall be maintained as part of the modified aircraft permanent records. SUPPLEMENTAL TYPE CERTIFICATE HOLDER: Kenmore Air Harbor, LLC. CESSNA 180G, 180H, 180J, and 180K (NORMAL CATEGORY) AS MODIFIED BY STC SA2069NM Engine: 1 Continental 0-470-U C O-520KAH-2 1 Continental 0-IO-520 C O-520KAH-1 Fuel: 100/100LL minimum grade aviation gasoline Engine Limits: Maximum Continuous, 2700 rpm and 270 hp Propeller and: (a) McCauley D3A34C403/80VA-0 Propeller Limits: Diameter: Not over 80”; not under 78.5” Pitch Settings at 30 in. sta.: Low 10.6º, High 25.6º (b) Cessna Spinner 0750286 (c) Governor, McCauley C290D3/T5, Woodward C210680, or Woodward C2100-001 Airspeed Limits: Vy (best rate of climb speed) 92 knots (IAS) Maximum Weight: Model Reference 180G and 180 H See Data Sheet 5A6 180J and 180K See Data Sheet 5A6 or STC SA649NW NOTE 1: Current weight and balance report, together with list of equipment included in certifi cated empty weight and loading instructions, when necessary, must be provided for each aircraft at the time of modification. **FAA FORM 8110-2 (5/14) PAGE 3 OF 4 PAGES** Number SA2069NM Kenmore Air Harbor, LLC. Issued: December 7, 1980 Reissued: April 5, 2019 Amended: August 26, 1994 SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA2069NM (Continued) NOTE 2: The following placard must be displayed as indicated. Adjacent to or in close proximity to the aircraft identification plate: NOTE 3: With the described engine and propeller installation, performance will be at least equal to or better than that given in the original FAA Approved Flight Manual for the Cessna 180 Series Airplanes. Replace existing placard in cockpit in view of pilots with the following: - END - **FAA FORM 8110-2 (5/14) PAGE 4 OF 4 PAGES** Engine Model 0-520KAH Engine Installed per Kenmore Air Harbor, Inc. STC SA2069NM Airplane equipped with Kenmore Air Harbor Conversion Model 0-520KAH engine. 270 HP at 2700 RPM Maximum ## Every issue (2) - April 5, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/18/1c/181c332876dde762c686dc964f9043d8b6bb2c2f63497333670e5a679996e65d) - August 26, 1994: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b5/12/b5129219d4f210206190825e32893576c6dae2b4068dc5252ea53dd7c3ca22bc) --- 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.