Thanks so far. Interesting point about the C150/152 wing drop, though. If the aircraft is correctly rigged there should very little tendency for a wing to drop unless the rudder is being pedalled at point of stall. I understand that the airworthiness certification flight test allows only a max of 15 degrees of wing drop under ANY stall condition. I guess that means if your C152 is dropping a wing badly (without pilot input) it would be a good idea to log it in the appropriate maintenance form as a defect - and get it fixed quickly. Would appreciate any info from your experiences on wing drop characteristics of the C150/152?