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ACRO E-mail Archive Thread: [Acro] Re: Luscombe spin

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ACRO E-mail Archive Thread: [Acro] Re: Luscombe spin



                


Thread: [Acro] Re: Luscombe spin

Message: [Acro] Re: Luscombe spin

Follow-Up To: ACRO Email list (for List Members only)

From: Frank <frankgorham at comcast.net>

Date: Sat, 21 Dec 2002 03:30:32 UTC


Message:

Ashley:
           Actually the T-41/172's of that vintage which I flew would give 1-1/2 to 2 turns max and then into the spiral where it was a race to prevent exceeding Vne or an engine overspeed in recovery.

            Cheers,  Frank
  ----- Original Message ----- 
  From: AMSnaproll at aol.com 
  To: acro at gf24.de 
  Sent: Friday, December 20, 2002 3:50 PM
  Subject: [Acro] Luscombe spin


  Sure, you simply limit the elevator travel so that the airplane will not propogate deeply enough into the stall to sustain autorotation. Some of the late '70's 172s were like that, even with a snaproll-like entry, the aircraft would unstall after 1/4 turn and degenerate into a speed increasing spiral, even though full elevator and pro-spin rudder was applied. Mind you, this applies only to a utility category CG location.

  Ashley Messenger
  Eagle 180MD 
Attachement 1: part2.html


                


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