STC SA01790SE

United States of America Department of Transportation _ Federal Aviation Administration Supplemental Type Certificate Number SA01790SE

This certificate, issued to AeroMech Incorporated 1616 Hewitt Avenue, Suite 312 Everett, WA 98201 Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A24CE (Revision 95) Make: Hawker Beechcraft Model: 200, 200C B200, B200C, 300, 300LW, B300, B300C

Description of the Type Design Change: Group approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-KAIR-0709, Rev. “NEW,” dated September 10, 2007, or later FAA approved revisions.

Limitations and Conditions: For Class 1 Airframes, Instructions for Initial and Continued Airworthiness, Document AMI-IICA-KAIR-0713, Rev. “New,” dated September 10, 2007, or later approved revision, is a required part of this STC.

The Airplane Flight Manual Supplement for the Class 1 airframes, AeroMech Document AMI-AFMS-KAIR-0718, Rev. “Original”, FAA Approved September 20, 2007, (or latest FAA-approved revision), is required on-board for operation of the aircraft.

Descriptive data pertaining to this design change are considered inadequate for duplication on other products.

This approval is limited to the Hawker Beechcraft Models 200, 200C, B200, B200C, 300, 300LW, B300, B300C aircraft only.

A copy of this certificate and FAA approved flight manual supplement must be maintained as part of the permanent records of the aircraft. If the holder agrees to permit another person to use this certificate, the holder shall give the other person written evidence of the permission.

Date of application: August 15, 2007 Date reissued:

Date of issuance: September 20, 2007 Date amended:

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)