Aircraft propulsion system pylon with multiple mounting stations

An apparatus for an aircraft, comprising:

• a pylon comprising a leading end, a trailing end, a base end, a first mounting beam, a second mounting beam, a first mounting station and a second mounting station;
• the pylon extending longitudinally between the leading end and the trailing end;
• the pylon projecting spanwise along a span line out from the base end towards the first mounting station and the second mounting station, the first mounting station disposed a first spanwise distance along the span line from the base end, and the second mounting station disposed a second spanwise distance along the span line from the base end, wherein the second spanwise distance is greater than the first spanwise distance;
• the first mounting beam linearly extending from the base end of the pylon to a distal end of the first mounting beam;
• the second mounting beam linearly extending from the base end of the pylon to the distal end of the second mounting beam;
• the pylon configurable to mount to
• a portion of a first propulsion system at the first mounting station, wherein the first propulsion system comprises a first propulsor rotor with a first diameter;
• or
• a portion of a second propulsion system at the second mounting station, wherein the second propulsion system comprises a second propulsor rotor with a second diameter that is greater than the first diameter;
• the first mounting station including a first station first mount configured to attach the portion of the first propulsion system to the first mounting beam and a first station second mount configured to attach the portion of the first propulsion system to the second mounting beam;
• and
• the second mounting station including a second station first mount configured to attach the portion of the second propulsion system to the first mounting beam and a second station second mount configured to attach the portion of the second propulsion system to the second mounting beam.