Feedthrough Plate (basic Cessna P/N 6211084-8) can be modified with feedthrough holes for electrical connectors, cables, tubes etc. 

Installation of a Bendix TCAS II system comprised of the following model numbers: TPA-81A, TCAS processor; two MST-67A, Mode S transponders; KFS-578A, TCAS control; two IVA-81A, TA/VSI indicators; two ANT-81A, TCAS antennas; and four Dorne and Margolin DMNI 50-2-2, Mode S Antennas.

Remove the existing aft baggage compartment overhead panels and replace with stainless steel panels using quick disconnect fasteners.

Installation of dual Bendix MLS-21B microwave landing systems (MLS) to include: 2 each VNS-41B with MLS angle receivers, 2 each CE-212B display controls and 3 each Dayton Granger 81001 or Bendix AT-214A/215A antennas, 2 forward on top centerline and 1 aft with power splitter connected to both receivers.

Installation of dual E-field antennas, Global 10085-2 in lieu of low 'P' static H-field antennas used with dual Global Flight Management Systems (FMS) GNS-1000. (650 S/N 650-0001 AND ON)

Installation of Honeywell Integrated Hazard Avoidance System (IHAS) 8000 Class A Traffic Alert System and Class B Terrain Awareness Warning System

Installation of Sensor Systems, Inc. Iridium Antenna per Pentastar Aviation, LLC Engineering Report No. 03ER-001 latest FAA revision.

Installation of a Bendix TCAS II system comprised of the following P/N's: TPA-81A, TCAS processor; KFS-578A, TCAS control; two MST-67A, Mode S transponders; two IVA-81A, TA/VSI: two ANT-81A, TCAS antenna; and four Dorne and Margolin DMNI 50-2-2, Mode S antennae.

RAAS activation on the Honeywell MK-VII EGPWSi.a.w. Installation Instructions, Doc. No. OPM-005Revision 1 has been issued to reflect the transfer of STC. EASA.A.S.03640

MK VII EGPWS Installation.Removed existing Equipment:i.a.w.Installation Instructions, Doc. No. OPM-004New installed EGPWS Equipment:- Honeywell MK-VII EGPWSi.a.w. Installation Instructions, Doc. No. OPM-004Revision 1: By revising the interface between the Vertical Gyro and theEGPWC and adapt the Gr... EASA.A.S.03639