# STC SA04348CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Kaman Corporation Aircraft Wheel and Brake LLC, United States
- Description: Installation of Parker Hannifin Corporation, Aircraft Wheel & Brake Division, Wheel and Brake Conversion Kit, part number 199- 283
- Applied: April 6, 2017
- Status date: September 17, 2022
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A59EU](https://openairdocs.org/tcds/A59EU)
- Certificate PDF: https://openairdocs.org/files/sha256/8b/a8/8ba8c5a29d86e57d9716c3c358699d194ac67c9d412063bec970d74e5ed832ee
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120828079220250627132924.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA04348CH

## ADs that name it (0)

None.

## Approved models (1)

- Piaggio Aviation S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU))

## 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.

for SA04348CH Kaman Corporation Aircraft Wheel and Brake, LLC 1160 Center Road Avon, OH 44011 Part 23 Federal Aviation Regulations A59EU Piaggio Aviation S.p.A.

P-180 Installation of Parker Hannifin Corporation, Aircraft Wheel & Brake Division, Wheel and Brake Conversion Kit, part number 199-283, in accordance with document number IM199-283, Kit Installation Publication: Main Wheel & Brake Conversion Kit Parker Hannifin Part No. 199-283, Revision A, dated October 16, 2018 or later FAA approved revision, and drawing number 50-166, Installation, Wheel & Brake, Revision A, dated November 30, 2017, or later FAA approved revision.

1. A copy of this certificate shall be maintained as part of the permanent records for the modified aircraft.

2. Maintain aircraft wheels and brakes in accordance with FA/\ accepted Instructions for Continued Airworthiness, Doc. No. AMMS199-283, Revision N/C, dated June 11, 2018 or later FAA accepted revision April 6, 2017 September 17, 2022 October 17, 2018 Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SA04348CH 3

SA04348CH Date Reissued: September 17, 2022

(Continued from Page 1: Limitations and Conditions)

3. Compatibility of the design change with previously proved modifications must be determined by the installer.

4. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

----------END---------- 3 3

## Every issue (2)

- September 17, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8b/a8/8ba8c5a29d86e57d9716c3c358699d194ac67c9d412063bec970d74e5ed832ee)
- October 17, 2018: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/08/c7/08c75d0d237def552666d935cd3a82af9f7729dea602ab024f8172f335c83400)

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