1976 Decathalon 8KCAB
A flutter developed when pulling 2.3 or greater g”s. It emanated from the trim tab forward to the stabilizers. A great deal of work has been done to solve this problem and it has been reduced but not eliminated.
The following has been done:
Checked elevator cable tension and elevator trim tension
Checked elevator trim pulleys
Replaced elevator trim tab
Checked elevator trim balance
Checked stabilizer incidence
Checked stab brace wire tension
Recovered elevators and stabilizers
Checked free play in hinges
Examined fuselage longerons and stab mount cluster looking for cracks
Checked motor mounts
At this point the flutter continues to manifest itself, but only in the elevators, under both power on and power off maneuvers of 2.3 g’s. Any suggestions?
A flutter developed when pulling 2.3 or greater g”s. It emanated from the trim tab forward to the stabilizers. A great deal of work has been done to solve this problem and it has been reduced but not eliminated.
The following has been done:
Checked elevator cable tension and elevator trim tension
Checked elevator trim pulleys
Replaced elevator trim tab
Checked elevator trim balance
Checked stabilizer incidence
Checked stab brace wire tension
Recovered elevators and stabilizers
Checked free play in hinges
Examined fuselage longerons and stab mount cluster looking for cracks
Checked motor mounts
At this point the flutter continues to manifest itself, but only in the elevators, under both power on and power off maneuvers of 2.3 g’s. Any suggestions?