EASA Regulations for Cessna 414A

2 airworthiness directives and regulations affecting Cessna 414A.

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New ADs and bulletins for Cessna 414A, summarized like the ones below, every Monday.

EASA SIB CE-14-19

Jun 4, 2014

Cessna 310, 401, 402, 411, 414 and 421 series Aeroplanes — MLG Torque Link

The FAA Special Airworthiness Information Bulletin SAIB: CE-14-19 addresses an airworthiness concern related to the main landing gear (MLG) torque link assembly on Cessna 300 and 400 series airplanes, including models 310P, 310Q, 310R, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, and 421C. The bulletin highlights the need to inspect and ensure the correct thickness and positioning of washers in the MLG torque link assembly. This information bulletin is advisory and does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin
  • Cessna 310P
  • Cessna 310Q
  • Cessna 310R
  • Cessna 401
  • Cessna 401A
  • Cessna 401B
  • Cessna 402
  • Cessna 402A
  • Cessna 402B
  • Cessna 402C
  • Cessna 411
  • Cessna 411A
  • Cessna 414
  • Cessna 414A
  • Cessna 421
  • Cessna 421A
  • Cessna 421B
  • Cessna 421C

EASA SIB CE-11-29R1

Oct 25, 2011

Cessna 414A and 421C, if modified by S-TEC Corporation STC - Flight Control System

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-29R1 addresses flight control system concerns for Cessna 414A and 421C aircraft modified by S-TEC Corporation Supplemental Type Certificates SA08996AC-D, SA7787SW-D, and SA7790SW-D with optional trim installed. The bulletin provides guidance on inspecting rudder trim tab blocks and phenolic blocks along the flight control system to prevent wear and ensure proper rudder travel. This information bulletin is advisory and does not mandate regulatory action.

Safety Information Bulletin
  • Cessna 414A
  • Cessna 421C