AD 2026-04-11 Lycoming Connecting Rod Bushings (Posted April 2, 2026)
AD 2026-04-11 Lycoming Connecting Rod Bushings
AD 2026-04-11 Lycoming Connecting Rod Bushings
Inspection required for Pilot and Co-Pilot yoke bushhings.
This AD has been superseded by AD 2026-04-11
The FAA has issued AD 2024-21-02 for Lycoming engines with certain connecting rod bushings installed.
The FAA has issued AD 2024-14-03 addressing a report of an uncommanded auto pitch trim runaway when the autopilot was first engaged.
The FAA has issued AD2024-08-09 effective 16 July 2024 for GA8 aircraft that addresses an unsafe electrical bonding issue.
The FAA is adopting a new airworthiness directive (AD) AD2024-07-07. It addresses an unsafe condition identified as excessive wear in the forward cargo door slide.
This AD applies to all Lycoming TIO-540-AJ1A reciprocating engines and it is effective June 28, 2017.
This AD requires you to repetitively inspect the wing spar assembly for cracks and replace any wing spar assembly found cracked
AD 2003-24-13 Cessna Aircraft Company: Amendment 39-13382; Docket No. 2003-CE-28-AD.
This AD currently requires initial and follow-up torque check inspections of pump relief valve attaching screws.