# STC SR00907DE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Erickson Incorporated, United States - Description: Installation of modified engine starters - Applied: February 26, 2018 - Status date: January 30, 2019 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 29 - Data sheets: [TCDS H10SW](https://openairdocs.org/tcds/H10SW) - Certificate PDF: https://openairdocs.org/files/sha256/e1/0b/e10bf2629e78fe2fdf60871e1a63f645546e2d86cf3076466baa29ffb3daf1d7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/907C5E8749BFD4908625856D004D06C4.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR00907DE ## ADs that name it (0) None. ## Approved models (1) - Bell Textron Inc. 214ST ([TCDS H10SW](https://openairdocs.org/tcds/H10SW)) ## 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. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00907DE This certificate and the supporting data which is the bases for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of Application: February 26, 2018 Date Reissued: Date of Issuance: January 30, 2019 Date Amended: Signature Title Kreg R. Voorhies ODA Administrator, Cert Works ODA(AIR)-833887-NM FAA Form 8110-2 (5/14) Page 1 of 3 This certificate, issued to: Erickson Incorporated 4002 Cirrus Dr. Medford, OR 97504 Part 29 of the Federal Aviation Regulations. Original Product - Type Certificate Number: H10SW Make: Bell Helicopter Textron, Inc. Model: 214ST Description of the Type Design Change: Installation of modified engine starters in accordance with Document No. CW0602-1016, Master Drawing List, Bell 214ST Starter Upgrade, Revision IR dated 12/19/2018, FAA approved 1/29/2019 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. CW0725-1047, Revision IR dated 1/14/2019, FAA accepted 1/29/2019, or later FAA accepted revision is required to be made available at installation. An FAA Approved Rotorcraft Flight Manual Supplement is not required for this modification. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. (Certification Basis on page 3 of 3) FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number: SR00907DE To (Name and address of transferee) From (Name and address of grantor) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00907DE Date of Issuance: January 30, 2019 FAA Form 8110-2 (5/14) Page 3 of 3 Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Bell Helicopter Textron, Inc 214ST installation modified engine starters is as follows: a. The type certification basis for Bell Helicopter Textron, Inc 214ST rotorcraft is shown on TCDS H10SW for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, February 26, 2018, is based upon 14 CFR Part 29, effective February 1, 1965 plus Amendments 29-1 through 29-16. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: Regulations established in accordance with the TCDS Certification Basis applicable to this design change: 14 CFR Sections: 29.301 Amdt. - ; 29.303 Amdt. - ; 29.305(a) Amdt. - ; 29.307(a) Amdt. 29-4; 29.337(a) Amdt. - ; 29.601(a) Amdt. - ; 29.603 Amdt. - ; 29.605 Amdt. - ; 29.607 Amdt. 29-5; 29.609(a) Amdt. - ; 29.611 Amdt. - ; 29.613 Amdt. - ; 29.619(b)(1) Amdt. - ; 29.625(a) Amdt. - ; 29.901 Amdt. 29-3; 29.903(c) Amdt. 29-3; 29.1163(a,b) Amdt. 29-3; 29.1301(a-c) Amdt. - ; 29.1301(d) Amdt. - ; 29.1309(a) Amdt. 29-14; 29.1309(b,c) Amdt. 29-14; 29.1351(a) Amdt. 29-14; 29.1353(a) Amdt. 29-15; 29.1359(b) Amdt. - ; 29.1529 Amdt. 29-4 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ## Every issue (1) - January 30, 2019: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e1/0b/e10bf2629e78fe2fdf60871e1a63f645546e2d86cf3076466baa29ffb3daf1d7) --- 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.