Piper PA-32R Lance — Service Bulletins

This Service Bulletin No. 1355A from Piper Aircraft addresses the inspection and potential replacement of the tee bar assembly in various Piper aircraft models, including the PA-32R-300 Lance. It supersedes the previous bulletin (SB 1355) and clarifies inspection instructions while correcting a reference error. The bulletin mandates compliance for affected aircraft, particularly those with 3,500 or more hours of time in service. It outlines a two-part compliance process: an initial inspection for cracks and a replacement procedure if cracks are found. The document emphasizes the importance of addressing any structural cracks before flight to maintain safety and compliance with FAA regulations.

• Initial inspection required within 100 hours TIS for aircraft with 3,500 or more hours TIS.
• Recurring inspections every 100 hours TIS until compliance with replacement is achieved.
• Cracks in the tee bar assembly must be addressed before the next flight.
• Replacement of the tee bar weldment assembly is mandatory if cracks are found.
• Ensure no more than 0.010 inches of free play exists between control components.