# STC SA01701SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Machen Inc - Description: Allow an increase in the takeoff maximum gross weight of the above model aircraft to 6850 pounds. - Status date: November 8, 2006 - Data sheets: A17WE, A17WE - Certificate PDF: https://openairdocs.org/files/sha256/13/1b/131babb8788067c8860ed9bf0b9c95e00f8a427c9208b04d34a6bcc0c84fe936 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DDBF79F9C5C05F39862572250074DE7B.0001 - Page: https://openairdocs.org/stc/SA01701SE ## ADs that name it None. ## Approved models (2) - Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) (TCDS A17WE) - Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) (TCDS A17WE) ## 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 SA01701SE This certificate, issued to: Machen Inc. 10555 Airport Drive, Coeur d’Alene Airport Hayden Lake, ID 83835 Part 23 of the Federal Aviation Regulations. Original Product⎯Type Certificate Number: A17WE Make: Aerostar Model: 601P, 602P Description of the Type Design Change: Allow an increase in the takeoff maximum gross weight of the above model aircraft to 6850 pounds per Machen Top Drawing List 203-TDL dated October 16, 2006, and installation instructions given in Machen Report 203-12, Rev. N/C, dated August 15, 2006, or a later FAA approved revision to either of these documents. Limitations and Conditions: Incorporation of this modification requires the concurrent or prior incorporation of Supplemental Type Certificate SA1658NM. This approval should not be extended to other airplanes of this model on which other previously approved modifications have been 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 have no adverse effect on the airworthiness of these airplanes. A copy of this certificate and Airplane Flight Manual Supplement or Pilots Operating Handbook Supplement (as appropriate) both dated September 11, 2006, or a later FAA approved revision to either of these documents, must be maintained as part of the permanent records of this aircraft. The airplane must be maintained in accordance with Section 7 of Machen Report 203-12, Rev. N/C, dated August 15, 2006 or a later FAA approved revision to this document. 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: December 6, 2002 Date reissued: Date of issuance: September 11, 2006 Date amended: November 8, 2006 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - November 8, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/13/1b/131babb8788067c8860ed9bf0b9c95e00f8a427c9208b04d34a6bcc0c84fe936) - September 11, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/69/02/6902e7b5dc1876beb10e45b09a2e20ea55101b7fb85779914e2486c09accbfd2) --- 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.