# STC SR01561SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Kawak Aviation Technologies Inc, United States
- Description: Installation of the Model 36300 Auxiliary Hydraulic System.
- Applied: February 25, 2005
- Status date: June 28, 2006
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS TR7BO](https://openairdocs.org/tcds/TR7BO)
- Certificate PDF: https://openairdocs.org/files/sha256/21/8c/218cda68db913e41ad4ad039205eca7a976128a84c6b4a6b6813bb974ab507e4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/266528A930F0DC1486257A160056ED28.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01561SE

## ADs that name it (0)

None.

## Approved models (1)

- Kaman Aerospace Corporation K-1200 ([TCDS TR7BO](https://openairdocs.org/tcds/TR7BO))

## 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 SR01561SE This certificate , issued to Kawak Aviation Technologies, Inc.

20690 Carmen Loop, Suite 102 Bend, Oregon 97702 Part 27 of the Federal Aviation Regulations.

Original Product ⎯Type Certificate Number : TR7BO Make : Kaman Model : K-1200

Description of the Type Design Change : Manufacture of the Kawak Aviation Technologies Model 36300 Auxiliary Hydraulic System in accordance with Master Drawing List 36300-MDL, Revision A dated May 31, 2005, or later FAA approved revision. Installation of the Model 36300 Auxiliary Hydraulic System in accordance with Kawak Aviation Technologies manual KATI-IM-632, Revision IR, dated May 14, 2005, or later FAA approved revision. This modification must be maintained in accordance with Kawak Aviation Technologies Instructions for Continued Airworthiness (ICA) document number KATI-MM-632, Revision IR, dated February 25, 2005, or later FAA accepted revision.

Limitations and Conditions : Approval of this change in type design applies to the above model rotorcraft only. This approval should not be extended to rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. Rotorcraft modified in accordance with this STC must be operated with an FAA approved copy of the Rotorcraft Flight Manual Supplement (RFMS), Kawak Aviation Technologies RFMS document number KATI-FM-632, Revision IR, approved on June 6, 2005, or later FAA approved revision. A copy of this certificate, the ICA and the RFMS shall be maintained as part of the permanent records for the modified rotorcraft.

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 : February 25, 2005 Date reissued : June 28, 2006 Date of issuance : June 7, 2005 Date amended :

___Original signed by Mike Pasion (Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (2)

- June 28, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/21/8c/218cda68db913e41ad4ad039205eca7a976128a84c6b4a6b6813bb974ab507e4)
- June 7, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/dc/7b/dc7b9d2867cb52c9b995796e8b288c23b51c26aba166ee7f6c5b5707e4822c53)

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