STC SA2737WE

This Certificate issued to Staggerwing Museum Foundation, Inc.

560 Old Shelbyville Highway Tullahoma, TN 37388 Part 03 of the Civil Air Regulations, effective November 13, 1945 and Part 3 effective November 1, 1949, as amended by 3-14 (paragraph 3.242) (Normal Category).

A-765 BEECH D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), JRB-6 Description of Type Design Change: Installation of Spar Strap Extension to outboard wing panel in accordance with FAA sealed Hamilton Aircraft Co., Inc. Drawing List 80-100. To be eligible, these aircraft must incorporate the provisions of STC SA1533WE – center section wing spar reinforcement.

See Page 2

Date of application : July 17, 1973

Date of issuance : August 10, 1973

Date reissued: April 28, 1977; September 3, 2004

Date amended: November 12, 1973

( Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

Number SA2737WE

April 28, 1977, September 3, 2004

The approval of this change in type design applies basically to Beech models D18S, E18S, E18S- 9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J (SNB-5), and JRB-6 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 by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

This reinforcement provides relief from the inspection requirements imposed by AD 73-18-4 (outboard wing panel).

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

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