Not mentioned in this clip, and apparently not widely known, is that purely by chance, the specific aluminium alloy used is almost immune to fatigue. At the time the airframe was designed, airframe fatigue was not well understood, and in fact the accident that first led to the serious study of it was still some years in the future (in Australia between Adelaide and Melbourne if my memory is correct).
The reason that the DC-3 was designed for short, unimproved runways, is simply that there was nothing else at the time (long, paved runways are a product of military requirements in WW2, and by 1945 were plentiful almost everywhere, because it was a world war). But what made it possible for the aircraft to continue for ninety years is this immunity to fatigue. And this longevity meant was that there was no market for a replacement. I remember that as late as 1971 more than half the world's airline flights were in DC-3s. The factor that led to a rapid drop in DC3 use where it could be replaced (mainly by the F27) in the 1970s was that the US Army made extensive use of the DC-3 in the Vietnam war, and substantially depleted the world stocks of spares, especially engine spares - up to that time the world fleet of DC-3s had been kept flying by the large stock of spares that had been sold, often at scrap prices, shortly after the end of hostilities in WW2.
John
JDNSW
1986 110 County 3.9 diesel
1970 2a 109 2.25 petrol
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