STC SA01830SE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01830SE This certificate issued to: Precise Flight, Inc.

63354 Powell Butte Road Bend, OR 97701 Part 23 of the Federal Aviation Regulations.

Original Product -Jype Certificate Number: 2A3 Make: Mooney Airplane Company Inc.

Model: M20M, M20S, M20R, and M20TN, Description of Type Design Change: Installation of a Fixed Oxygen System Manufactured in accordance with Precise Flight drawing lists 106N0000, Revision A, dated April 7, 2008, 100N0000, Revision AE, dated January 31, 2008, 035N0000, Revision -(IR), dated February 17, 2008, 027N0000, Revision E, dated September 5, 2007, 026N0000, Revision F, dated January 9 2008, 020N0000, Revision G, dated August 27, 2007, 016N0000, Revision C, dated September 5, 2007, 012N0000, Revision -(IR), dated May 20, 2005, 011N0000, Revision A, dated April 8, 2007, 010N0000, Revision J, datec January 25, 2008, and 009N0000, Revision C, dated June 6, 2007, or later FAA-approved revisions. Installed in accordance with Precise Flight Engineering Drawing List 106N0000, Revision A, dated April 7, 2008, or later FAA-approved revisions.

Maintained in accordance with the Instructions for Continued Airworthiness Precise Flight Document 106NMAN0002, Revision - (IR), dated February 22, 2008, or later FAA accepted 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 AFMS, Precise Flight Inc. Document 106NMAN0001, Revision - (IR), dated April 9, 2008, or later FAA-approved revisions, must be maintained as part of the permanent records for the modified aircraft. The oxygen system installed in accordance with this STC is qualified for operations up to and including 25,000 feet, but this installation does not change the maximum operating altitude of the airplane on which it is installed.

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.

See Continuation Sheet for additional Limitations and Conditions

Date of Application: December 12, 2007 Date Reissued:

Date of Issuance: April 15, 2008 Date Amended: February 12, 2009 FEDERAL AVIATION By Direction of the Administrator Signature HOMINIST RATION Acting Manager, Seattle Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01830SE Ssued to: Precise Flight, Inc.

Date of Issuance: April 15, 2008 Date Amended: February 12, 2009 Limitations and Conditions: (cont d/ Note: This continuation sheet is applicable to the STC as issued on April 15, 2008.

Certification Basis:

The certification basis for this modification is in accordance with Type Certificate Data Sheet, 2A3.

Additionally, for areas changed by this STC modification, the applicant has volunteered compliance with the following:

230532389289012505072310503 323513135158-2315 31986 23181.

23.1381, 23.1431, 23.1438, 23.1441, 23.1443, 23.1445, 23.1447, 23.1449, 23.1451, 23.1453,

23.1501, 23.1519, 23.1525, 23.1527, 23.1529, 23.1541, 23.1543, 23.1557, 23.1581, 23. 1583,

23.1585, at the amendment levels in effect on December 12, 2007, the date of application.

•END-.

FAA FORM 8110-2-1 (10-69)