# STC SH1152NW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Air Products & Parts LLC, United States - Description: Installation of the Automatic Flagman Model 135 Control Stick Grip - Applied: November 18, 1980 - Status date: July 30, 2021 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW), [TCDS H1IN](https://openairdocs.org/tcds/H1IN), [TCDS H3WE](https://openairdocs.org/tcds/H3WE), [TCDS H-1](https://openairdocs.org/tcds/H-1), [TCDS 2H3](https://openairdocs.org/tcds/2H3), [TCDS 2H1](https://openairdocs.org/tcds/2H1), [TCDS 4H11](https://openairdocs.org/tcds/4H11), [TCDS 4H12](https://openairdocs.org/tcds/4H12) - Certificate PDF: https://openairdocs.org/files/sha256/7c/df/7cdf276d58c52c69d5f7f6fa9bae656385066b10f01699f5e925c4b5d9ec3898 - Approved model list and other attachments: [AML SH1152NW.pdf](https://openairdocs.org/files/sha256/a8/52/a852f634463107bb9e42537a26ce9783e1c0faeebdf7c9c1bdae7861507e567b) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6789F307FA0E123D8625886E005124BA.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SH1152NW ## ADs that name it (0) None. ## Approved models (34) - Bell Helicopter Textron Canada Limited 206 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206B-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - 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)) - Eurocopter France SA.315B Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN)) - MD Helicopter Inc. 369 ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369A ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369D ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369H ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369HE ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369HM ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - MD Helicopter Inc. 369HS ([TCDS H3WE](https://openairdocs.org/tcds/H3WE)) - Scotts-Bell 47 Inc 47D ([TCDS H-1](https://openairdocs.org/tcds/H-1)) - Scotts-Bell 47 Inc 47D1 ([TCDS H-1](https://openairdocs.org/tcds/H-1)) - Scotts-Bell 47 Inc 47G ([TCDS H-1](https://openairdocs.org/tcds/H-1)) - Scotts-Bell 47 Inc 47G-2 ([TCDS H-1](https://openairdocs.org/tcds/H-1)) - Scotts-Bell 47 Inc 47G-2A ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-2A-1 ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-3 ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-3B ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-3B-1 ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-3B-2 ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-4 ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-4A ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47G-5 ([TCDS 2H3](https://openairdocs.org/tcds/2H3)) - Scotts-Bell 47 Inc 47J ([TCDS 2H1](https://openairdocs.org/tcds/2H1)) - Scotts-Bell 47 Inc 47J-2 ([TCDS 2H1](https://openairdocs.org/tcds/2H1)) - Scotts-Bell 47 Inc 47J-2A ([TCDS 2H1](https://openairdocs.org/tcds/2H1)) - Scotts-Bell 47 Inc 47K ([TCDS 2H1](https://openairdocs.org/tcds/2H1)) - Siam Hiller Holdings Inc. UH-12E ([TCDS 4H11](https://openairdocs.org/tcds/4H11)) - Sikorsky Aircraft Corporation 269C ([TCDS 4H12](https://openairdocs.org/tcds/4H12)) ## 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. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SH1152NW Air Products & Parts, LLC P.O Box 687 Olney, TX, 76374 Part * the * Regulations *See attached FAA Approved Model List (AML) No. SH1152NW for a list of the approved rotorcraft models and applicable airworthiness regulations. Installation of the Flight Grip Model 135 Control Stick Grip in accordance with Flight Grip Master Drawing List MDL135, dated March 21, 2002, or later FAA approved revision. Approval of this change in type design applies to the rotorcraft models listed on the AML only. This approval should not be extended to other 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 rotorcraft. A copy of this Certificate and AML must 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. November 18, 1980 April 2, 1986; September 10, 2001; July 30, 2021 January 5, 1981 June 14, 2001; March 29, 2002 For Acting Manager, Seattle ACO Branch 2 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SH1152NW 2 ### AML SH1152NW.pdf FLIGHT GRIP, LLC FAA APPROVED MODEL LIST (AML) SH1152NW FOR INSTALLATION OF FLIGHT GRIP MODEL 135 CONTROL STICK GRIP ISSUE DATE: January 5, 1981 **ITEM AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE** **CERTIFICATION** **BASIS FOR** **FAA SEALED** **DRAWING LIST** **INSTALLATION** **INSTRUCTIONS AML** **AMENDED** **NUMBER ALTERATION NUMBER REV NUMBER REV DATE** 1. Aerospatiale SA.315B H11N CAR 10 (FAR 21.29) & CAR 6, December 20, 1956 MDL135 3/21/02 136 2 3/21/02 3/29/02 2. Bell 47D, 47D1, 47G, 47G-2 H-1 CAR 6, May 24, 1946 MDL135 3/21/02 136 2 3/21/02 3/29/02 3. Bell 47J, 47K, 47J-2, 47J-2A 2H1 CAR 6, January 15, 1951 MDL135 3/21/02 136 2 3/21/02 3/29/02 4. Bell 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 46G-3B-1, 47G-4, 47G-4A, 47G-5, 47G-3B-2 2H3 CAR 6, December 20, 1956 MDL135 3/21/02 136 2 3/21/02 3/29/02 5. Bell 206, 206A, 206A-1, 206B, 206B-1, 206L, 206L-1 H2SW CAR 6, December 20, 1956 MDL135 3/21/02 136 2 3/21/02 3/29/02 6. Hiller UH-12E 4H11 CAR 6, December 20, 1956 MDL135 3/21/02 136 2 3/21/02 3/29/02 7. Hughes 269C 4H12 CAR 6, January 15, 1951 MDL135 3/21/02 136 2 3/21/02 3/29/02 8. Hughes 369, 369A, 369H, 369HM, 369HS, 369HE, 369D H3WE CAR 6, December 20, 1956 MDL135 3/21/02 136 2 3/21/02 3/29/02 1 2 FAA APPROVED: __________________________________________ DATE: _______________ 3 Manager Special Certification Branch 4 Seattle Aircraft Certification Office 5 6 Amended: June 14, 2001; March 27, 2002 7 Reissued: April 2, 1986; September 10, 2001 8 ## Every issue (2) - July 30, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/7c/df/7cdf276d58c52c69d5f7f6fa9bae656385066b10f01699f5e925c4b5d9ec3898), [AML SH1152NW.pdf](https://openairdocs.org/files/sha256/a8/52/a852f634463107bb9e42537a26ce9783e1c0faeebdf7c9c1bdae7861507e567b) - March 29, 2002: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/a2/80/a2803fd425f2504ca2d1a645f12a963fe94c65af410353881dd557a091648e1e), [AML SH1152NW.pdf](https://openairdocs.org/files/sha256/a8/52/a852f634463107bb9e42537a26ce9783e1c0faeebdf7c9c1bdae7861507e567b) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.