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BCS-4-1AT

Fuel Balancing Unit

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Availability
Pre-order
Condition
New
Warranty
6 Months
Price on request

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Description

BCS-4-1AT fuel balancing unit

BCS-4-1AT is the established Latin catalogue form of the Russian БЦС-4-1АТ centering unit. Aircraft technical documentation identifies it as part of the ATsT5-1BT automatic fuel balancing and capacitance fuel-quantity system. The block is not a flight-control centre-of-gravity computer; its “centering” function concerns balanced fuel consumption between the left and right wing tanks.

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Function in the ATsT5-1BT system

The system automatically keeps fuel consumption balanced between corresponding left- and right-wing tanks while also measuring total and individual fuel quantities. BCS-4-1AT participates in the automatic balancing channel and works with the measuring/conversion and switching equipment. It also supports the logic associated with minimum-fuel warnings for the caisson tanks as defined by the installed system.

Documented Yak-40 installation

The Yak-40 technical description places BCS-4-1AT in the right equipment compartment as part of ATsT5-1BT. The documented set includes ten DT-30V tank sensors, two DTSK1A-2T temperature-compensation sensors, the BIP2-7T measuring/conversion block, UK2-1AT switching unit and PPTI3-2TA indicator. The exact aircraft effectivity must still be checked by serial number.

Power and system interfaces

The ATsT5-1BT system documentation specifies 28.5 V DC and 115 V, 400 Hz AC supplies. These are system power values and should not be treated as a complete standalone BCS-4-1AT pin specification. Selection requires the full Cyrillic marking БЦС-4-1АТ, drawing and series, connectors, aircraft wiring and the companion-block execution. The related BCS-6-1T belongs to a different fuel system.

Inspection and ordering

Inspect the front panel, controls or indicators, connectors, rack fittings, seals and data plate. Functional testing must reproduce tank-sensor signals and switching logic with the approved ATsT5-1BT procedure. State the aircraft, system, complete marking, quantity, condition and document requirements in the enquiry. Related fuel-system electronics are available under Electronic Control Units.

Technical details

Product Name
Fuel Balancing / Centering Unit
Primary Designation
BCS-4-1AT
Original Cyrillic Designation
БЦС-4-1АТ
Product Type
Automatic fuel-balancing electronic unit
Documented System
ATsT5-1BT automatic fuel balancing and capacitance fuel-quantity system
All specificationsCollapse specifications
Documented Aircraft
Yak-40; verify aircraft serial and equipment fit
Documented Function
Balancing fuel consumption between corresponding left and right wing tanks
System Indication
Fuel quantity by tank/side and total; minimum-fuel warning logic
Associated Sensors
Ten DT-30V tank sensors and two DTSK1A-2T temperature-compensation sensors
Associated Blocks
BIP2-7T measuring/conversion block, UK2-1AT switching unit and PPTI3-2TA indicator
System DC Supply
28.5 V DC
System AC Supply
115 V AC, 400 Hz
Installation Location
Right equipment compartment in the documented Yak-40 installation
Alternative Designations
BCS-4-1AT; BCS4-1AT; BTsS-4-1AT; БЦС-4-1АТ; БЦС4-1АТ
Interchangeability
Not interchangeable with BCS-6-1T; match the complete ATsT5-1BT configuration
Documentation
Product passport and Yak-40 / ATsT5-1BT technical documentation

Payment & delivery

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BCS-4-1AT