FIELD: physics.
SUBSTANCE: invention relates to test equipment for testing aircraft additional centre tank (ACT) system. The test equipment comprises at least one of the following test modules: a first test module and a second test module. The first test module can be connected to the ACT system in place of part of control apparatus which performs an auxiliary fuel management computer (AFMC) function. The first test module has apparatus for generating one or more test signals imitating one or more ACT valve control instructions. The second test module can be connected to the ACT system in place of the control apparatus which performs an auxiliary level sensing control unit (ALSCU) function, while the other part of the control apparatus which performs the AFMC function remains in place in the ACT system. The second test module has apparatus for generating one or more test signals imitating one or more fuel level readings in the ACT.
EFFECT: high efficiency of testing characteristics of an aircraft ACT system.
15 cl, 3 dwg
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