# STC SA00560SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Precise Flight Inc, United States - Description: Installation of Precise Flight Pulselite Controls System. - Applied: November 7, 1997 - Status date: February 21, 2006 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/19/88/1988fa3b187a468fd0fdf0b7d7492342777f8a666df9288aaa36d178ea0021fc - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F9801AB2BEFFA05D862579A60072FA64.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00560SE ## ADs that name it (0) None. ## Approved models (1) - Bell Helicopter Textron Canada Limited 407 ([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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA00560SE This certificate, issued to Precise Flight, Inc. 63354 Powell Butte Road Bend, OR 97701 Part 27 of the Federal Aviation Regulations. Original ProductType Certificate Number: H2SW Make: Bell Model: 407 Description of the Type Design Change: Installation of the Precise Flight Pulselite Controls System. The system is to be manufactured in accordance with Precise Flight Engineering Drawing Lists 002P0000, Revision J; 015P0000, Revision K; 025P0000, Revision H, or later FAA approved revisions. It is to be installed in accordance with appropriate Precise Flight Drawing List 141P0000, Revision B, or later FAA approved revision, and to the installation manuals listed on the drawing list; and to be maintained in accordance with the Instructions for Continued Airworthiness contained in PFI Document 000PMAN0002, Revision B, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. 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 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. A copy of this Certificate and FAA Approved Flight Manual Supplement document 141PMAN0001, Revision A, dated February 8, 2006, or later FAA Approved revision, must be maintained as part of the permanent records for the 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: November 7, 1997 Date reissued: Date of issuance: August 19, 1998 Date amended: November 7, 2003; February 21, 2006 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - February 21, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/19/88/1988fa3b187a468fd0fdf0b7d7492342777f8a666df9288aaa36d178ea0021fc) --- 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.