EASA Regulations for Cessna 402C

4 airworthiness directives and regulations affecting Cessna 402C.

EASA SIB CE-14-19

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.

Jun 4, 2014

Safety Information BulletinMaintenanceSafety MgmtCessna 310PCessna 310QCessna 310RCessna 401Cessna 401ACessna 401BCessna 402Cessna 402ACessna 402BCessna 402CCessna 411Cessna 411ACessna 414Cessna 414ACessna 421Cessna 421ACessna 421BCessna 421C

EASA SIB CE-10-48

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.

Sep 9, 2010

Safety Information BulletinMaintenanceSafety MgmtCessna 402C

EASA SIB CE-10-44

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.

Aug 10, 2010

Safety Information BulletinFlight OpsSafety MgmtCessna 402C

EASA SIB CE-10-01

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.

Oct 7, 2009

Safety Information BulletinMaintenanceSafety MgmtCessna 402C