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Old 26th Aug 2012, 10:48
  #40 (permalink)  
Farfrompuken
 
Join Date: Nov 2000
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LJ

The difference in engine output between the -A and -M would necessitate the difference in rudder you note above.

ISTR the USAF losses were entirely due to the way they handled the aircraft, rather than any specific design/build issue.

T67M way superior to the Grob but that's all history anyhow.
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