060-0026-00

Roll and pitch reference for flight-control equipment

In operation, the gyro establishes a stable vertical reference. Aircraft motion relative to that reference is converted into roll and pitch information for the connected flight-control computer or compatible display system. The receiving equipment uses these signals to calculate guidance, flight-director or autopilot commands according to the particular installation. This makes the KVG 350 a sensing element in the control loop, not an actuator and not a cockpit control panel.

Published BendixKing flight-control documentation identifies the KVG 350 as a remote source of roll and pitch attitude reference. Documented installations include systems in which its signals are routed to a KCP-series flight computer and onward to flight-director or autopilot functions. The exact associated computer and display configuration varies by aircraft and system approval, so no universal interchangeability with another vertical gyro should be assumed from appearance alone.

Electrical supply and identification-plate data

The original plate on this photographed 060-0026-00 unit specifies an input of 115 V AC at 400 Hz. It also states 88 VA during start and 30 VA during normal running. These values are direct identification evidence for the exact configuration shown and should be used when planning bench power or checking the aircraft installation. Connection pin assignments still require the applicable KVG 350 installation or maintenance manual.

The same plate identifies TSO C4c, C9c and C52a compliance and lists the DO-160 environmental category as D2A/MNO/XXXXXXZBABB. It gives a unit weight of 6.8 lb, approximately 3.08 kg. The photographed serial number is 2841. Serial and modification status describe the illustrated example; the serial number and modification configuration of the unit allocated to an order are reconfirmed before shipment.

Remote installation and configuration control

The KVG 350 uses a remote mounting arrangement appropriate to a precision gyro. Installation location, orientation, structural support, cooling, vibration isolation and wiring must follow approved aircraft data. A fast-erect circuit is documented in compatible flight-control installations to increase the gyro erection rate when selected, but availability and switch wiring depend on the particular aircraft system. It must not be assumed for every installation without checking the wiring documentation.

Part Number 060-0026-00 is the ordering identity for this product. Search variants such as KVG350, KVG-350 and 060002600 are useful for identification, but they do not replace the exact manufacturer Part Number. Any proposed replacement must be checked for form, fit, function, electrical supply, connector arrangement, attitude-signal characteristics and approval status. Similar-looking remote gyros may use different outputs or mounting geometry.

Overhauled condition and ordering information

This 060-0026-00 KVG 350 is offered in Overhauled condition from partner stock with a six-month warranty. The principal image and gallery photograph retain the authentic Bendix/King and AlliedSignal markings, exact Part Number, electrical ratings, qualification data and visible construction. The image has not been redrawn by AI because technical accuracy and readable original markings take priority over cosmetic effects.

For a quotation, specify Part Number 060-0026-00, model KVG 350, required quantity, destination and documentation requirements. The exact included mount, mating connectors, release documentation and test records are confirmed at quotation stage. Other identified flight-control, communication and navigation units can be reviewed in the Garmin / BendixKing / Honeywell / Collins category. Products listed together may belong to related avionics installations but are not interchangeable unless approved technical data expressly authorizes the substitution.