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 the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.
Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine).
Mitchell automatic flight system AK506 consisting of Piper Autocontrol IIIB autopilot with optional radio coupler.
Mitchell auto. Flight system AK481, consisting of Piper altimatic IIIC autopilot with command automatic electronic pitch trim system, optional radio, and glide slope couplers.
Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.
Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System
Installation of Garmin GDL 88 ADS-B UAT Transceiver System