# STC SA162GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Kaman Corporation Aircraft Wheel and Brake LLC, United States
- Description: Installation of Cleveland main wheels and brakes.
- Applied: February 11, 1977
- Status date: September 19, 2022
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A4SW](https://openairdocs.org/tcds/A4SW), [TCDS A3SW](https://openairdocs.org/tcds/A3SW)
- Certificate PDF: https://openairdocs.org/files/sha256/c3/df/c3dfcb1c1e0e034c56d48407ae92cc4cdbda9af8fff3d7d67834baaa17fef5e5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119735201420250606170938.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA162GL

## ADs that name it (0)

None.

## Approved models (2)

- Thrush Aircraft LLC. S2R ([TCDS A3SW](https://openairdocs.org/tcds/A3SW))
- Thrush Aircraft LLC. S2R ([TCDS A4SW](https://openairdocs.org/tcds/A4SW))

## 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 SA162GL Kaman Corporation Aircraft Wheel and Brake, LLC 1160 Center Road Avon, OH 44011 Part 3 & 8 Civil Air Regulations A3SW and A4SW Thrush Aircraft, LLC S-2R lnstallation of Cleveland Main Wheels and Brakes in accordance with Parker Hannifin Conversion Kit P/N 199-68A, Revision A, dated March 8, 1988, and Cleveland Installation Drawing 50-40, Revision B, dated January 9, 1984, or later FAA Approved revisions.

1. This STC applies to those airplanes already using automotive type brake fluid and 27-inch wheels, and with a maximum of 600 H.P.

2. The approval of this change in type design applies basically to the Model S-2R only...

February 11, 1977 October 28, 1980; September 19, 2022 April 15, 1977 August 2, 1984; May 6, 1988 Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SA162GL 3

SA162GL Date Reissued: September 19, 2022

(Continued from Page 1: Limitations and Conditions) This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.

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

## Every issue (1)

- September 19, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c3/df/c3dfcb1c1e0e034c56d48407ae92cc4cdbda9af8fff3d7d67834baaa17fef5e5)

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