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It's a -200, and Iran Air is the only airline still operating them for commercial flights. They're at least 30 years old, pretty insane considering that the average age of some FLEETS is 10 years old.
I've heard smaller airports fly them as well after big airliners sell them. But for a larger group to keep them on is cool especially considering the age as you mentioned. They're supposedly good planes so why not keep on with em I suppose.
Iran Air still flies the 747-200 because they couldn't buy new planes from Boeing or Airbus until very recently due to sanctions.
Planes can continue to go on for quite the time in the air, it's engines and flight time hours that is the issue 9/10. Some people say that the pressure changes it experiences over its life is a big factor, but it's not really proven..
Different systems and different component lifecycles use different metrics to gauge age and wear. Engine life are highly impacted by flight hours. With that said, the airframe service life, the fuselage in particular, is absolutely driven by the pressurization cycles it experiences throughout its lifecycle rather than just numerical hours. In fact, short haul airplanes are designed to have a higher number of service cycles in its lifetime despite a lower flight hours Limit of Validity because a short haul airplane is expected to make more flight cycles each day than a long haul airplane. The design service objective lifetime is then one of the factors that drives structural sizing.
Aluminum as a material slowly fatigues naturally over time, but cyclical loading will drive that fatigue rate much higher. If you've seen an aluminum commercial airplane that's towards the end of its life, you'll see numerous doublers and triplers underneath the skin to strengthen the areas that have fatigue cracks that have developed and been arrested.
Boeing put out a document that talks about how it will comply with the fairly recent FAA rule that established regulations on airframe limit of validity, and laid out what the airframe DSO vs LoV for each model is.
The pressure changes do have an effect on the lifetime of the air due to the cyclic stresses applied to the airframe, but generally it's a quantity that is proportional to the number of hours flown and the intended use of the aircraft.
I just want to clarify that it's primarily proportional to the number of take off-get to altitude-landing cycles rather than just pure hours flown, though you're also right in the sense that different structural components will have different loading scenarios that will drive variations in life limit considering the application of factors of safety.