What it approves
Installation of high strength replacement wheel bolt hardware
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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate 14 CFR 21.120) FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 3 Number: SA2410AK This certificate issued to:
Description of Type Design Change: Installation of high strength replacement wheel bolt hardware in accordance with Airforms, Inc., Installation Instructions, Report No: 32-601-36-01, Rev. N/C, dated April 7, 2013.
1. The replacement hardware is eligible for installation only on the main wheels of Cessna models 208 and 208B aircraft with any of the Cessna approved tire sizes and 10 inch diameter Cleveland wheel and brake assembly, P/N 20-244.
2. This Supplemental Type Certificate (STC) is compatible with Aeroacoustics, Inc. gross weight increase STCs utilizing Cleveland wheel and brake assembly P/N 20-244.
(Limitations and Conditions continued on page 3 of 3)
Airforms, LLC.
3650 W. Aviation Ave Wasilla, AK 99654 Original Product Type Certificate Number: A37CE Make: Textron Aviation Inc.
Model: 208; 208B Date of application: April 9, 2013 Date of issuance: May 3, 2013 Date reissued: May 25, 2017; August 19, 2022 Date amended:
August A. Asay Title: Manager, Anchorage ACO Branch Part 23 of Federal Aviation Regulations.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate 14 CFR 21.120) FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 3 Number: SA2410AK
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA2410AK To (Name and address of transferee):
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate 14 CFR 21.120) FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 3 (Continuation Sheet) Date of application: April 9, 2013 Date of issuance: May 3, 2013 Date reissued: May 25, 2017; August 19, 2022 Number: SA02410AK Limitations and Conditions: (Continued from Page 1 of 3)
3. The replacement hardware is eligible for installation on aircraft equipped with or without the Aero Twin, Inc., brake disc spacer STC SA2126AK-D.
4. The installer must determine whether this design change is compatible with previously approved modifications.
5. For Instructions for Continued Airworthiness refer to Cessna 208 Maintenance Manual, section 32-40-00, revision 25.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 19, 2022 | Reissued, current | Certificate |
| May 25, 2017 | Reissued, earlier issue | Certificate |
| May 3, 2013 | Issued, earlier issue | Certificate |