Installation of the Honeywell KFD 840 Primary Flight Display System.REQUIRED DATA: AML No. 159-08325-0002, Revision -, dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate.

Installation of S-TEC System 40X/50X single and two axis automatic flight guidance systems, Model ST-786-40X/50X.

Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-865-20/30.

Installation of Mitchell automatic flight system Model AK401 consisting of Century IIB autopilot with optional radio coupler.

Installation: Wing leading edge fuel tanks Data required: Floair Document 141-3.21.1 dated June 23, 1972, and approved Airplane Flight Manual Supplement, Floair Document 141-3.91 dated July 24, 1972.

Installation of Mitchell automatic flight system Model YK428 consisting of yaw damper system

Installation of Mitchell automatic flight system model AK408 consisting of Century II auto-pilot with optional radio coupler.

Installation of Mitchell flight director remote annunciator Model AK375.

Installation of Clark three- light gear position indicator system.

Installation of Mitchell automatic flight system model AK330, consisting of Century I autopilot with optional omni tracker.