# STC SR01369SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Kawak Aviation Technologies Inc, United States
- Description: Installation of Kawak Aviation Technologies, Inc. (KATI) Model 35150 Auxiliary Hydraulic System
- Applied: October 5, 2000
- Status date: November 27, 2013
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/45/31/4531a87dee1483fc8e1f3bd000143d4c32356fe96173951d2073c69a2672ef14
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F9F58EAB777120E586257C3200534B23.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR01369SE

## ADs that name it (0)

None.

## Approved models (4)

- Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## 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.

Number SR01369SE

This certificate, issued to KAWAK Aviation Technologies, Inc.

20690 Carmen Loop, Suite 102 Bend, OR 97702

Part 27 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H2SW Make: Bell Model: 206L, 206L-1, 206L-3, and 206L-4

Description of the Type Design Change: Installation of Kawak Aviation Technologies, Inc. (KATI) Model 35150 Auxiliary Hydraulic System in accordance with KATI Drawing List No. 35150-401-MDL, Revision C, dated April 18, 2013, or later Federal Aviation Administration (FAA) approved revision and KAWAK Installation Manual Number KATI-IM-627, Revision C, dated January 22, 2013, or later FAA-approved revision. This modification must be maintained in accordance with KATI Instructions for Continued Airworthiness (ICA) Document KATI-MM-627, Revision A, dated January 18, 2013, or later FAA-accepted revision.

Limitations and Conditions: Approval of this change in type design applies only to the rotorcraft listed above. This approval should not be extended to other rotorcraft of this model on which other previously approved modification are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. Modified rotorcraft must be operated in accordance with a copy of FAA-approved Rotorcraft Flight Manual Supplement (RFMS) AASI-FM-627, Revision IR, dated January 26, 2004, or later FAA-approved revision. A copy of this certificate, the RFMS, and the ICA, 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: October 5, 2000 Date reissued: June 28, 2006 Date of issuance: January 26, 2004 Date amended: November 27, 2013

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

## Every issue (3)

- November 27, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/45/31/4531a87dee1483fc8e1f3bd000143d4c32356fe96173951d2073c69a2672ef14)
- June 28, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d2/ab/d2ab3abf27a4402d3cb66e4011904eb80a7d59ea929a98a83aeef1c29ebf12c8)
- January 26, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/69/91/6991e7c5dd897d5ba28c768ffacdbd6cbd845dd618ec722889c987533fd26da4)

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