Isn't there just something really curious about the Stabalizer trim being manually controlled by a pair of cables running the length of the plane and in to the cockpit?
I was under the impression that the physical connection between pilot and plane had mostly been eliminated, redundancy now provided through back up electronic systems.
Presumably the crank is that size so the pilots get enough leverage to be able to turn it.
Isn't there just something really curious about the Stabalizer trim being manually controlled by a pair of cables running the length of the plane and in to the cockpit?