Abstract: The Ignition Performance Measuring Circut is intended for use with dual ignition systems, such as the dual-magneto ignition systems used on light aircraft. The circuit has a first and second channel. The first channel is dedicated to measuring the relative peak amplitude of amplitude difference signals, i.e. the algebraic difference between concurrent left and right conditioned ignition signals. Signal conditioning is performed by an input attenuator and a difference amplifier. The circuit operates without benefit of a positive synchronization. To any particular cylinder's ignition firing signals. The pilot of an aircraft using the invention circuit will be alerted to the presence of a degraded firing signal but will not be advised as to which cylinder or spark plug is contributing to the failure indication. The circuit has a peak detection network for selecting the largest amplitude difference signal from each series of firing signals.