EASA Regulations for Piper PA-34-200

2 airworthiness directives and regulatory documents affecting Piper PA-34-200.

EASA AD US-2022-09-13

Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment

The Federal Register document titled "Time Limits / Maintenance Checks — Airworthiness Limitations Section — Amendment" is a final rule airworthiness directive issued by the FAA for Piper Aircraft, Inc. Model PA-34-200 airplanes. It establishes a life limit for alternate bolts, part numbers 693-215 and NAS6207-50D, that attach the drag link to the nose gear trunnion. This directive addresses a previously unlisted life limit to ensure continued airworthiness and safety of the affected aircraft.

Apr 28, 2022

Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-34 (Seneca)Piper PA-34-200

EASA SIB CE-09-15

Piper PA-34 Nose Gear Centering Attach Bolt

The Special Airworthiness Information Bulletin SAIB CE-09-15 is an FAA informational bulletin addressing a nose gear centering attach bolt issue on Piper Aircraft Models PA-34-200, PA-34-200T, and PA-34-220T. It highlights a potential failure of the nose landing gear to extend due to the hex-head bolt on the nose gear centering spring rod-end jamming against the nose gear door actuation aft tube assembly. This bulletin provides awareness but does not mandate corrective action under 14 CFR part 39.

Mar 3, 2009

Safety Information BulletinMaintenanceSafety MgmtPiper PA-34-200Piper PA-34-200TPiper PA-34-220T