# STC SA01238SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Kenmore Air Harbor Inc, United States
- Description: Installation of EDO 689-2130 floats, and a gross weight increase of up to 2200 pounds.
- Applied: July 5, 2002
- Status date: July 17, 2003
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A22NM](https://openairdocs.org/tcds/A22NM)
- Certificate PDF: https://openairdocs.org/files/sha256/84/85/8485beb37320e00ccc822604decb2b8cac443a85eb19337c3f4899f2290124bc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/450F16A80BD9F3D5862576FE00442A4A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01238SE

## ADs that name it (0)

None.

## Approved models (1)

- Sky International Inc. A-1B ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))

## 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: SA01238SE This certificate issued to: Kenmore Air EDO Floats, L.L.C.

6321 NE 175th Street Kenmore, WA 98028 Part 23 of the Federal Sviation Regulations.

Original Product - Jype Certificate Number: A22NM Make: Sky International, Inc. (Aviat) Model: A-1B Description of Type Design Change: Installation of EDO 689-2130 floats, and a gross weight increase of up to 2200 pounds, in accordance with Kenmore Air Harbor Master Drawing List EFM-113, Revision A, dated March 10, 2003, or later FAA approved revisions.

Limitations and Conditions: The weight and balance report must be amended to include the gross weight increase of up to 2200 pounds as shown in the Airplane Flight Manual Supplement(AFMS).

Approval of this change applies to the above model only, and should not be extended to other specific models of these airplanes 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 AFMS EFM-115, dated July 17, 2003, or later FAA approved revision, must 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: July 5, 2002 Date Reissued:

Date of Issuance: July 17, 2003 Date Amended:

FEDERAL AVIATION By Direction of the Administrator беса _ I (Signature) NO MINISTRATION Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- July 17, 2003: Issued, Current. [certificate](https://openairdocs.org/files/sha256/84/85/8485beb37320e00ccc822604decb2b8cac443a85eb19337c3f4899f2290124bc)

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