Installation of exhaust silencers in accordance with Beryl D’Shannon installation instructions for Part Number 1010-1 and 1010-2, Rev. A, dated 2-2-76, or for Part Number 1010-3 and 1010-4, Rev. B, dated 2-10-76.The exhaust silencer is manufactured in accordance with Beryl D’Shannon Drawing No. 1010, Rev. B, dated 2-2-76.

Installation of exhaust silencers in accordance with Top Banana Installation Instructions dated March 12, 1975, Revision of October 22, 1975.Silencer is manufactured in accordance with Top Banana Drawing No. 2-12-A35 “G” change.

: Installation of auxiliary wing tip fuel tanks in accordance with Drawing Number RB1-001B and Installation Instructions number RB-1, Revision of April 1, 1960.This wing tip tank installation is acceptable with either the baggage auxiliary tanks, or the wing auxiliary tanks. However, it is not acceptable with both auxiliary installations incorporated simultaneously.

Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E., Inc. STC SA09074SC.

Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E., Inc. STC SA09074SC.

Installation of a stainless steel exhaust system. Required as part of this STC is Atlantic Aero Document 19593010, Instructions for Continued Airworthiness, Rev B, dtd 3/27/02, or later FAA approved revision.

Replacement of original main landing gear doors with monolithic machined gear doors.

Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632