# STC SA00701SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Precise Flight Inc - Description: Installation of Precise Flight Pulselite System. - Status date: November 7, 2003 - Data sheets: H10WE, H11NM - Certificate PDF: https://openairdocs.org/files/sha256/72/cc/72ccf555777e6b68f81adab022e4d6e7d08221cd5e9607a19adc2be72d9964a4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E2E671B4E9A982C2862579A6006A636F.0001 - Page: https://openairdocs.org/stc/SA00701SE ## ADs that name it None. ## Approved models (2) - Robinson Helicopter Company R22 (TCDS H10WE) - Robinson Helicopter Company R44 (TCDS H11NM) ## 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 SA00701SE This certificate, issued to Precise Flight, Inc. 63354 Powell Butte Road Bend, OR 97701 Part * of the * Regulations. Original ProductType Certificate Number: *See attached FAA Approved Model List (AML) Make: No. SA00701SE for list of approved airplane Model: models and applicable airworthiness regulations Description of the Type Design Change: Installation of Precise Flight Pulselite System in accordance with Precise Flight, Inc. Engineering drawings 590P0001, Revision -, dated January 26, 1999, and 590P0002, Revision -, dated January 26, 1999, 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 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. A copy of this Certificate, and FAA Approved Model List (AML) No. SA00701SE, and Precise Flight, Inc. FAA approved Rotorcraft Flight Manual Supplement for Robinson R22 or R44, dated May 18, 1999, or later FAA approved revision, 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: January 14, 1999 Date reissued: Date of issuance: May 18, 1999 Date amended: November 7, 2003 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### AML SA00701SE.pdf **FAA APPROVED MODEL LIST (AML) NO. SA00701SE** **PRECISE FLIGHT, INC.** For **PULSELITE INSTALLATION** Issue Date: May 18, 1999 Item Aircraft Make Aircraft Model Original Type Certificate Number Certification Basis for Alteration FAA Approved Instructions and Drawing __________________________ Number REV AML Amdt. Date 1 Robinson R22 H10WE FAR 27 and Type Certificate H10WE Engineering Drawing 590P0001 Engineering Drawing 590P0002 Revision -, dated January 26, 1999, or later FAA approved revision Revision -, dated January 26, 1999, or later FAA approved revision IR 2 Robinson R44 H11NM FAR 27 and Type Certificate No. H11NM Engineering Drawing 590P0001 Engineering Drawing 590P0002 Revision -, dated January 26, 1999, or later FAA approved revision Revision -, dated January 26, 1999, or later FAA approved revision IR FAA Approved: ________________________________ Acting Manager, Seattle Aircraft C e r t i f i c a t i o n O f f i c e Sheet 1 of 1 ## Every issue (1) - November 7, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/72/cc/72ccf555777e6b68f81adab022e4d6e7d08221cd5e9607a19adc2be72d9964a4), [AML SA00701SE.pdf](https://openairdocs.org/files/sha256/b9/98/b9983926ba9539cc444a07874dd017e6292f246e990bef50239ee830353b7676) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.