065-0064-08

Role within the flight-control architecture

A representative signal path is pilot-selected mode and aircraft sensor input → KCP 220 flight computer → compatible primary and trim servos → aircraft control linkage. Annunciators and cockpit displays report the selected or captured modes to the crew. Exact connected units vary by aircraft and installation approval, so a component named in the same system family is not automatically compatible with this suffix.

The connector face on the exact unit carries three multi-pin interfaces marked J2203, J2202 and J2201. These interfaces link the computer to the aircraft harness and other system equipment. Their visible design is documented by the images, but pin functions are not inferred from connector position. Wiring, shielding, grounds and test points must follow the approved installation drawing.

Exact identification and qualification marks

The original plate identifies the unit as a KCP 220 Flight Computer with Part Number 065-0064-08 and serial number 2726. It carries TSO C9c and C52a references together with RTCA/DO-160B. The plate also records modification status. These readings come from the exact photographed unit and are preserved without copying data from another KCP 220 suffix.

No dependable suffix-specific supply current, mass or overall dimensions were confirmed in the reviewed primary material and exact plate. Those values are therefore not invented. Installation clearances must also include the rack, connector backshells and cable bend radius. The applicable KCP 220 installation and maintenance manuals remain the controlling references. They also define the mandatory post-installation tests and allowable configuration changes.

Installation, testing and configuration control

The main image shows the full rectangular housing, three front connectors, rails, labels and fasteners on a neutral studio background. The gallery image focuses on the exact plate and modification marks. Original caution labels are retained, while no reseller branding is carried into the product presentation. The photographed connector geometry has not been redesigned.

Replacement requires confirmation of Part Number, modification status, system version, aircraft wiring and any associated configuration straps. Bench evaluation and aircraft return-to-service checks require approved equipment and procedures. Autopilot faults can be caused by sensors, mode controllers, air-data inputs, servos, wiring or power as well as the computer, so fault isolation should precede component substitution. The photographed connector labels support identification, but they are not a wiring instruction and must not replace the approved interconnect diagram.

Serviceable stock and ordering requirements

This 065-0064-08 KCP 220 is offered in Serviceable condition from partner stock with a six-month warranty. The price applies the agreed minimum margin to the exact same-condition public comparison because it exceeded the offer-list figure. The unit allocated to an order is reconfirmed for serial number, release documentation and test status.

For a quotation, specify Part Number 065-0064-08, model KCP 220, aircraft application, quantity and paperwork requirement. Rack, mating connectors, mode controller, air-data computer, sensors and servos are included only when expressly stated. Related avionics can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Related items are not necessarily interchangeable.