EASA Regulations for Piper PA-34-200

2 airworthiness directives and regulations affecting Piper PA-34-200.

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New ADs and bulletins for Piper PA-34-200, summarized like the ones below, every Monday.

EASA AD US-2022-09-13

Apr 28, 2022

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.

Airworthiness Directive
  • Piper Aircraft PA-34 (Seneca)
  • Piper PA-34-200

EASA SIB CE-09-15

Mar 3, 2009

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.

Safety Information Bulletin
  • Piper PA-34-200
  • Piper PA-34-200T
  • Piper PA-34-220T