AUXILIARY COMPONENT MOUNTING SYSTEM FOR GAS TURBINE ENGINES

An assembly (200) for mounting an auxiliary component (120) to an engine case (210) of a gas turbine engine (100) includes a support bracket (222), the support bracket (222) having a first end (230) configured for attachment to a first flange (232) of the engine case (210), a second end (236) configured for attachment to a second flange (238) of the engine case (210), and an intermediate portion (246) located intermediate the first end (230) and the second end (236); a bearing member (248) disposed within the intermediate portion (246); a locator (224) disposed within the bearing member (248); a first plurality of bolts (234) configured to attach the first end (230) of the support bracket (222) to the first flange (232); a second plurality of bolts (240) configured to attach the second end (238) of the support bracket (222) to the second flange (238); and a mechanical fuse (264).