# STC SA619GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Kaman Corporation Aircraft Wheel and Brake LLC, United States
- Description: Installation of Parker Hannifin Main Wheel and Brake Kit Part Numbers 199-90
- Applied: March 29, 1982
- Status date: September 19, 2022
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20)
- Certificate PDF: https://openairdocs.org/files/sha256/58/a6/58a6af96aa8446e0d09b53f9dfb56b5879bf5aa67297c6f84c6faf5c1a09c2df
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173863597220240725195733.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA619GL

## ADs that name it (0)

None.

## Approved models (9)

- Hawker Beechcraft Corporation 65-90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90-1 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90-4 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation H90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))

## 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.

SA619GL Kaman Corporation Aircraft Wheel and Brake, LLC 1160 Center Road Avon, OH 44011 Part 3 Civil Air Regulations 3A20 Textron Aviation Inc.

65-90, 65-A90, 65-A90- I (JU-21A), 65-A90-4 (RU-21E, RU-21H), B90, C90, C90A, C90GT, C90GTi, E90, H90 (T-44A) Installation of Parker Hannifin Main Wheel and Brake Kit Part Numbers 199-90 in accordance with Parker Hannifin Conversi0n Kit lnstallation Manual IM199-90, Revision J, dateu January 7. 2009, or later FAA approved revisions.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

March 29, 1982 September 19, 2022 June 23, 1982 August 24, 1982; August 22, 1983; October 11, 1988; November 22, 1991; January 5, 1995; June 4, 2009 Steven L. Lardinois Manager, Systems Section Chicago ACO Branch 3

SA619GL 3

SA619GL Date Reissued: September 19, 2022

(Continued from Page 1: Limitations and Conditions)

3. 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.

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

## Every issue (2)

- September 19, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/58/a6/58a6af96aa8446e0d09b53f9dfb56b5879bf5aa67297c6f84c6faf5c1a09c2df)
- January 5, 1995: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8c/85/8c851ee01eb2f1a321105b60831c3734693dbfe08bc32a33cb28cb287abedb95)

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