A gas turbine engine comprising: a plurality of igniters; a combustion chamber (210, 310); and a system comprising an igniter event conductor that comprises a pressure conductive path adapted to conduct a change in pressure within the combustion chamber of an igniter event at a first of the igniters, wherein the igniter event conductor comprises a) a first portion adjacent an ignition location of the first of the igniters of the gas turbine engine and in the combustion chamber (210, 310) of the engine and b) a second portion apart from the first of the igniters and apart from the combustion chamber, wherein the igniter event conductor is adapted to conduct the change in pressure within the combustion chamber of an igniter event at the first of the igniters from the first portion to the second portion; a pressure sensor configured to sense the change in pressure within the combustion chamber of the igniter event, wherein the igniter event conductor is coupled to the pressure sensor and the igniter event conductor conducts the change in pressure within the combustion chamber of the igniter event to the pressure sensor, wherein the sensor is coupled to the second portion of the igniter event conductor; and a controller communicatively coupled to the sensor and configured to determine that the igniter event occurred at the ignition location of the first of the igniters rather than at another location in the combustion chamber based on an input from the sensor and a threshold value. a plurality of igniters; a combustion chamber (210, 310); and a system comprising an igniter event conductor that comprises a pressure conductive path adapted to conduct a change in pressure within the combustion chamber of an igniter event at a first of the igniters, wherein the igniter event conductor comprises a) a first portion adjacent an ignition location of the first of the igniters of the gas turbine engine and in the combustion chamber (210, 310) of the engine and b) a second portion apart from the first of the igniters and apart from the combustion chamber, wherein the igniter event conductor is adapted to conduct the change in pressure within the combustion chamber of an igniter event at the first of the igniters from the first portion to the second portion; a pressure sensor configured to sense the change in pressure within the combustion chamber of the igniter event, wherein the igniter event conductor is coupled to the pressure sensor and the igniter event conductor conducts the change in pressure within the combustion chamber of the igniter event to the pressure sensor, wherein the sensor is coupled to the second portion of the igniter event conductor; and a controller communicatively coupled to the sensor and configured to determine that the igniter event occurred at the ignition location of the first of the igniters rather than at another location in the combustion chamber based on an input from the sensor and a threshold value. an igniter event conductor that comprises a pressure conductive path adapted to conduct a change in pressure within the combustion chamber of an igniter event at a first of the igniters, wherein the igniter event conductor comprises a) a first portion adjacent an ignition location of the first of the igniters of the gas turbine engine and in the combustion chamber (210, 310) of the engine and b) a second portion apart from the first of the igniters and apart from the combustion chamber, wherein the igniter event conductor is adapted to conduct the change in pressure within the combustion chamber of an igniter event at the first of the igniters from the first portion to the second portion; a) a first portion adjacent an ignition location of the first of the igniters of the gas turbine engine and in the combustion chamber (210, 310) of the engine and b) a second portion apart from the first of the igniters and apart from the combustion chamber, wherein the igniter event conductor is adapted to conduct the change in pressure within the combustion chamber of an igniter event at the first of the igniters from the first portion to the second portion; a pressure sensor configured to sense the change in pressure within the combustion chamber of the igniter event, wherein the igniter event conductor is coupled to the pressure sensor and the igniter event conductor conducts the change in pressure within the combustion chamber of the igniter event to the pressure sensor, wherein the sensor is coupled to the second portion of the igniter event conductor; and a controller communicatively coupled to the sensor and configured to determine that the igniter event occurred at the ignition location of the first of the igniters rather than at another location in the combustion chamber based on an input from the sensor and a threshold value.