PT-200Ts Series 3

PT-200Ts-III for gyroscopic instruments

The main load for the PT-200Ts Series 3 is aviation gyroscopic equipment. The converter supplies the three-phase power needed to spin up and operate attitude indicators, gyro-compass equipment and related navigation units. Instruments of this class depend on stable 400 Hz power; if the supply is lost or unstable, the instrument readings may become unreliable. On aircraft with this converter installed, loss of PT-200Ts operation can lead to warning indications in the cockpit and failure flags on the affected flight-navigation instruments.

Construction of the PT-200Ts Series 3 umformer

The PT-200Ts Series 3 is built as a motor-generator unit on a common shaft. One part of the machine is a DC motor powered from the aircraft DC bus. The other part is a synchronous three-phase generator that produces the required AC output. This electromechanical layout is typical for aircraft of earlier design generations, where rotary converters were used before static converters became common. The housing includes mounting provisions for installation on the aircraft structure and may include a filter box to reduce radio interference produced by the rotating electrical machine.

Aircraft installation of PT-200Ts Series 3

The PT-200Ts Series 3 is normally installed outside the cockpit, because rotary converters produce noise, vibration and electrical interference. Depending on aircraft type, it may be mounted in a radio equipment bay, electrical compartment, technical bay, under the cockpit floor, or on a dedicated shock-mounted frame. On helicopters, installation is usually arranged in service areas where the unit is accessible for inspection but isolated from the crew workplace. Correct mounting is important: the converter rotates at high speed and must be secured in a way that prevents vibration damage and wiring fatigue.

PT-200Ts-III operation with APP-1A switching logic

In many aircraft systems, the PT-200Ts Series 3 works together with automatic switching equipment such as APP-1A. The converter may be started automatically when the aircraft’s main AC generators fail or when backup power logic requires a separate 36 V, 400 Hz source. This makes the unit part of the emergency or standby electrical architecture for selected instruments. In maintenance, it is important to check not only the converter itself, but also the switching device, control relay logic, protection circuits and cockpit failure indication.

Series 3 features of the PT-200Ts converter

The Series 3 version shares the main electrical characteristics of other PT-200Ts variants, but may differ in construction details, filtering elements, wiring layout and component base. Later or different series can use revised filter boxes, updated rectifier or diode elements, different terminal arrangements and improved reliability of mechanical assemblies. These changes mean that series designation matters when replacing the unit. A converter with the same output voltage and power rating is not automatically interchangeable unless the aircraft documentation allows the specific version.

Maintenance and supply of PT-200Ts Series 3

The PT-200Ts Series 3 should be inspected as both an electrical and mechanical aircraft unit. A proper check normally includes input current, output voltage, output frequency, load performance, heating, vibration, noise, bearing condition and connector state. Because the unit runs at high speed, storage condition and bearing condition matter just as much as the electrical parameters. For procurement, the full designation PT-200Ts Series 3 or PT-200Ts-III should be specified together with required condition, documentation, test status and aircraft applicability.