EASA Regulations for Cessna 402C

4 airworthiness directives and regulations affecting Cessna 402C.

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New ADs and bulletins for Cessna 402C, 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-10-48

Sep 9, 2010

Cessna 402C — Incorrect Assembly of MLG Torque Link Centre Pivot Attachment

The FAA Special Airworthiness Information Bulletin SAIB: CE-10-48 addresses the incorrect assembly of the main landing gear (MLG) torque link center pivot attachment on Cessna Model 402C airplanes. It informs operators and maintenance personnel about new caution statements to be added to the Cessna 402C Maintenance Manual regarding the proper handling and installation of washer part number 5045018-2. This bulletin is informational and does not mandate regulatory action.

Safety Information Bulletin
  • Cessna 402C

EASA SIB CE-10-44

Aug 10, 2010

Cessna 402C Hydraulic Power Indicating - Temporary Revisions (TRs) to Pilot—s Operating Handbook (POH)

The Special Airworthiness Information Bulletin SAIB: CE-10-44 is a non-mandatory FAA information bulletin addressing hydraulic power indication issues on Cessna Model 402C airplanes. It highlights the meaning of the "HYD PRESS" light and the potential consequences if the hydraulic pressure indication is not properly addressed during flight operations.

Safety Information Bulletin
  • Cessna 402C

EASA SIB CE-10-01

Oct 7, 2009

Cessna "Twins" / Lack of Detent Positions in the Fuel Tank Selector Valve System.

The Special Airworthiness Information Bulletin SAIB: CE-10-01 is an FAA informational bulletin addressing a fuel tank selector valve system issue in Cessna twin engine reciprocating airplanes, specifically including the Cessna Model 402C. It highlights concerns about the lack of detent positions in the fuel tank selector valve system that can lead to failure in moving the valve to the commanded position, potentially causing total engine power loss.

Safety Information Bulletin
  • Cessna 402C