And why are the Piper Seminole stall warners disconnected on the ground so that you can't test em?
Think lowering the later stages of flap on the Seneca alters the relative airflow making the one stall warner useless. Look carefully at the stall warner vane, they are positioned at slightly different angles.
Probably suggests why the Seneca seems to stall at full flap on landing, crashing down weakening the nose drag link on the nose leg that seems to fail a lot.
Last edited by BigEndBob; 21st April 2007 at 21:11.