EASA Regulations for Cessna 207

6 airworthiness directives and regulations affecting Cessna 207.

EASA SIB CE-12-41

Cessna (incl. formerly Reims Aviation) 177, F177, 182, F182, 206, 207, 210, 337 and F337 Series Aeroplanes — Flight Control Column Loose Glide Screw

The Special Airworthiness Information Bulletin SAIB: CE-12-41 is an FAA advisory concerning a potential loose glide screw in the flight control columns of various Cessna aircraft models, including the 177, F177, 182, F182, 206, 207, 210, 337, and F337 series. This bulletin informs owners, operators, and maintenance personnel about the risk of the glide screw backing out and jamming the elevator control system. The affected screw part numbers are NAS220-14 and MS27039-0814.

Aug 14, 2012

Safety Information BulletinMaintenanceSafety MgmtCessna 177Cessna F177Cessna 182Cessna F182Cessna 206Cessna 207Cessna 210Cessna 337Cessna F337

EASA SIB CE-12-14

Cessna Aeroplanes - Alternative Methods of Compliance (AMOC) for FAA AD 2011-10-09

The document titled 'Cessna Aeroplanes - Alternative Methods of Compliance (AMOC) for FAA AD 2011-10-09' is a Special Airworthiness Information Bulletin (SAIB CE-12-14) issued by the FAA. It addresses three alternative methods of compliance for FAA Airworthiness Directive 2011-10-09, which affects multiple Cessna airplane models including the 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 series. The AMOCs provide more efficient and cost-effective procedures for seat track inspections and repairs while maintaining safety standards.

Jan 26, 2012

Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 152Cessna 170Cessna 172Cessna 175Cessna 177Cessna 180Cessna 182Cessna 185Cessna 188Cessna 190Cessna 195Cessna 206Cessna 207Cessna 210Cessna T303Cessna 336Cessna 337

EASA SIB CE-11-08

Cessna 206/207 aeroplanes - Sierra Industries STC SA3634SW and SA3853SW

The Special Airworthiness Information Bulletin SAIB: CE-11-08 is an FAA informational bulletin addressing fuel storage concerns on Cessna Models 206 and 207 aircraft equipped with Sierra Industries STC SA3634SW or SA3853SW auxiliary fuel tank bladders. It highlights a potential issue where operators may misjudge actual fuel quantity due to insufficient settling time of fuel in the auxiliary bladders after refueling. The bulletin does not mandate regulatory action but provides safety recommendations.

Jan 4, 2011

Safety Information BulletinSafety MgmtCessna 206Cessna 207

EASA SIB SAFO10016

Cessna (including Reims Aviation) - Missing or Improper Seat Stops

The Safety Alert for Operators (SAFO) 10016 titled "Cessna (including Reims Aviation) - Missing or Improper Seat Stops" addresses the requirement for type design seat stops on seat rails in various Cessna aircraft models. Affected aircraft include Cessna models 150, 152, 172, 206, 303, 336, 337, and legacy single-engine models such as 170, 175, 177, 180, 182, 185, 188, 190, 195, 205, 207, and 210. The document highlights the importance of proper seat stop installation to maintain airworthiness and safety during critical flight phases.

Sep 7, 2010

Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 152Cessna 172Cessna 206Cessna 303Cessna 336Cessna 337Cessna 170Cessna 175Cessna 177Cessna 180Cessna 182Cessna 185Cessna 188Cessna 190Cessna 195Cessna 205Cessna 207Cessna 210

EASA SIB 2008-54

FAA SAIB CE-04-72R1 - Cessna / Reims Aeroplanes - Voltage Regulator VR600A with insufficient over-voltage protection

FAA SAIB CE-04-72R1 is a Special Airworthiness Information Bulletin addressing the voltage regulator VR600A used in certain Cessna single-engine aircraft, including models 150, 172, 177, 180, 182, 185, 188, 206, 207, and 210 series, as well as those manufactured by Reims Aviation. The bulletin highlights insufficient over-voltage protection in the VR600A voltage regulator, which can lead to undetected over-voltage conditions. EASA SIB No. 2008-54 supports the FAA's recommendations and informs European operators of the same issue.

Jun 26, 2008

Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 172Cessna 177Cessna 180Cessna 182Cessna 185Cessna 188Cessna 206Cessna 207Cessna 210Reims Aviation

EASA SIB 2007-14

FAA SAIB CE-05-27 - Foam-Filled Elevator Trim (F-FET) Tabs installed on Cessna single-engine aircraft

EASA Safety Information Notice No. 2007-14 is an informational notice referencing FAA Special Airworthiness Information Bulletin CE-05-27 regarding foam-filled elevator trim (F-FET) tabs installed on certain Cessna single-engine aircraft models 206, 207, and 210. The document highlights potential issues with these F-FET tabs, including moisture absorption leading to internal corrosion, added weight, and possible flutter. It applies to specific aircraft serial numbers listed in the FAA bulletin.

May 7, 2007

Safety Information BulletinMaintenanceSafety MgmtCessna 206Cessna 207Cessna 210