RegNotify

EASA Regulations for Cessna 180

6 airworthiness directives and regulations affecting Cessna 180.

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 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 2007-40

FAA SAIB CE-08-02 - Cessna 180, 182 and 185 Aeroplanes - Horizontal Stabiliser Trim Freeze-up In-Flight

FAA Special Airworthiness Information Bulletin CE-08-02 is an informational bulletin addressing an airworthiness concern affecting Cessna 180, 182, and 185 series aircraft. The bulletin highlights issues with horizontal stabilizer trim freeze-up in flight caused by excessive wear in the pitch trim actuator screw-jack threads, specifically involving parts with Cessna part numbers 0712500-13 and 0712500-11. This condition may impair pitch trim control and aircraft handling.

Nov 12, 2007
Safety Information BulletinMaintenanceSafety MgmtCessna 180Cessna 182Cessna 185

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