What it approves
Installation of EDO model 249-2870 floats.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Number SA221NW
This certificate, issued to Kenmore Air Harbor, LLC.
6321 NE 175th Street Kenmore, WA 98028
Part 3 of the Civil Air Regulations,effective November 1, 1949.
Original ProductType Certificate Number: 5A6 Make: Cessna Model: 180J
Description of the Type Design Change: Installation of EDO model 249-2870 floats in accordance with EDO Corporation Installation Drawing No. 16775, except when rudder steering cables must be connected to the tailwheel steering bellcranks.
Limitations and Conditions: Data pertaining to this modification are considered inadequate for duplication on other aircraft. This approval is limited to the installation on Cessna 180J, Serial Numbers 18052356 and 18052317 only. A copy of this Certificate and Addendum No. SA221NW shall be maintained as part of the permanent records for the modified aircraft.
Date of application: October 6, 1975 Date reissued: April 5, 2019
Date of issuance: October 16, 1975 Date amended: May 18, 1978; July 22, 1994
FAA FORM 8110-2 (5/14) PAGE 1 OF 3 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 SA221NW
Kenmore Air Harbor, LLC.
Issued: October 16, 1975 Reissued: April 5, 2019 Amended: May 18, 1978; July 22, 1994
SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA221NW
The conditions and limitations of the original specifications apply except as follows:
This Addendum, which is part of the Supplemental Type Certificate No. SA221NW, 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 perm anent records.
SUPPLEMENTAL TYPE CERTIFICATE HOLDER: Kenmore Air Harbor, LLC.
CESSNA 180J (SEAPLANE-NORMAL CATEGORY) AS MODIFIED BY STC SA221NW
Serial Numbers Eligible: Serial Numbers 18052356 and 18052317
Airspeed Limits: Never exceed – 184 mph (160 knots) Maneuvering – 122 mph (106 knots) Max. structural cruising – 160 mph (139 knots) Flaps extended – 100 mph (87 knots)
Powerplant Instrument Markings: Same as specified
Maximum Weight: 2820 pounds
Center of Gravity Limits With Edo 249-2870 Floats: (+40.2) to (+43.9) at 2820 pounds (+35.0) to (+43.9) at 2125 pounds or less
Placards: A placard must be installed on the instrument panel in full view of the pilot as follows:
- END -
FAA FORM 8110-2 (5/14) PAGE 3 OF 3 PAGES
GROSS WEIGHT IS LIMITED TO 2820 POUNDS WHEN EDO 249-2870 FLOATS ARE INSTALLED.
PILOT IS RESPONSIBLE FOR PROPER LOADING.
(SEE WEIGHT & BALANCE DATA)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| The Cessna Aircraft Company | 180J | 5A6 |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 5, 2019 | Reissued, current | Certificate |
| July 22, 1994 | Amended, earlier issue | Certificate |