EASA Regulations for Cessna 172

9 airworthiness directives and regulations affecting Cessna 172.

EASA AD 2017-0034R1

Engine — Gearbox — Modification / Inspection

EASA Airworthiness Directive 2017-0034R1 is a regulatory document addressing safety concerns related to Technify Motors GmbH TAE 125-02 engines installed on various aircraft including Diamond DA 40, DA 42, DA 42M, CEAPR DR 400, Cessna 172, and Piper PA-28. The directive mandates modification and inspection of the engine gearbox and clutch system to prevent oil leaks and potential engine power loss. It specifically targets affected gearboxes identified by part and serial numbers and requires replacement of the clutch with a dual mass flywheel.

Jan 18, 2018

Airworthiness DirectiveMaintenanceSafety MgmtContinental Aerospace Technologies, Gmbh TAE125Diamond DA 40Diamond DA 42Diamond DA 42MCEAPR DR 400Cessna 172Piper PA-28

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 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 CE-04-03

Cessna and Reims Aviation — Control Yoke Assembly

Special Airworthiness Information Bulletin No. CE-04-03 is a safety notification from the FAA regarding certain Cessna Aircraft Company and Reims Aviation 172, 180, and 185 series airplanes. It addresses the potential failure of the control yoke assembly due to corrosion caused by moisture ingress, which could result in loss of pitch and possible loss of aileron control. The bulletin lists specific affected models including various Cessna 172 variants and Reims Aviation Cessna models.

Feb 1, 2010

Safety Information BulletinMaintenanceSafety MgmtCessna 172Cessna 180Cessna 185Reims Aviation Cessna 172Reims Aviation Cessna 180Reims Aviation Cessna 185

EASA SIB CE-09-10

Cessna Seats Secondary Stop Installation

The Special Airworthiness Information Bulletin SAIB: CE-09-10 is an FAA informational bulletin addressing the availability of secondary seat stops for pilot and copilot seats on various Cessna aircraft models including 170, 172, 182, 206, 210, 337, and others. It highlights ongoing concerns with seat latch pin engagement that can lead to seat slippage and potential loss of airplane control. The bulletin informs operators about service bulletins issued by Cessna for installing secondary seat stops and inspecting certain reel assemblies.

Feb 26, 2009

Safety Information BulletinMaintenanceSafety MgmtCessna 170Cessna 172Cessna 182Cessna 206Cessna 210Cessna 337

EASA SIB 2009-20080401002

Unapproved Engine Mounts may have been installed on Cessna aircraft

The FAA Safety Notification No. 2009-20080401002 advises that unapproved engine mounts manufactured by XP Modifications, Inc. may have been installed on Cessna Model 172 airplanes and possibly other Cessna models. This notification alerts aircraft owners, operators, maintenance organizations, and parts distributors about the potential presence of these unapproved parts. The engine mounts were sold without FAA Parts Manufacturer Approval and were found in the process of installation on a Cessna 172 at Riverside, California.

Feb 26, 2009

Safety Information BulletinMaintenanceSafety MgmtCessna 172

EASA SIB 2008-84R1

Funkwerk Avionics (formerly Filser Electronic) TRT600 and TRT800 Series Transponders — Intermittent Loss of Detection, Insufficient Mode S Reply.

EASA Safety Information Bulletin 2008-84R1 addresses intermittent loss of detection and insufficient Mode S replies from Funkwerk Avionics TRT600 and TRT800 Series Transponders, including units formerly manufactured by Filser Electronic. These transponders are installed on various aircraft such as Cessna 150, 172, 182, 210, Diamond DA 20, Mooney M20J, Piper PA-28, and multiple sailplane models. The bulletin highlights issues affecting radar tracking and Mode S interrogation responses in European airspace.

Nov 12, 2008

Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 172Cessna 182Cessna 210Diamond DA 20Mooney M20JPiper PA-28

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 2007-36

FAA SAIB CE-01-41R2 - Cessna 150, 172, P172, 175, 180, 182, 185, 205, 206, 210, 336 and 337 Aeroplanes - Possible Cracks in Plastic or Non-Metallic Control Wheels

FAA Special Airworthiness Information Bulletin CE-01-41R2 addresses the potential for cracks in plastic or non-metallic control wheels installed on Cessna 150, 172, P172, 175, 180, 182, 185, 205, 206, 210, 336, and 337 series airplanes manufactured between 1960 and 1964. The bulletin informs owners, operators, and maintenance personnel about this issue and provides guidance on inspection and replacement procedures. This information is also referenced in EASA Safety Information Notice 2007-36.

Oct 5, 2007

Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 172Cessna P172Cessna 175Cessna 180Cessna 182Cessna 185Cessna 205Cessna 206Cessna 210Cessna 336Cessna 337