EASA Regulations for Cessna 180

6 airworthiness directives and regulations affecting Cessna 180.

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New ADs and bulletins for Cessna 180, summarized like the ones below, every Monday.

EASA SIB CE-12-14

Jan 26, 2012

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.

Safety Information Bulletin
  • Cessna 150
  • Cessna 152
  • Cessna 170
  • Cessna 172
  • Cessna 175
  • Cessna 177
  • Cessna 180
  • Cessna 182
  • Cessna 185
  • Cessna 188
  • Cessna 190
  • Cessna 195
  • Cessna 206
  • Cessna 207
  • Cessna 210
  • Cessna T303
  • Cessna 336
  • Cessna 337

EASA SIB SAFO10016

Sep 7, 2010

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.

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

EASA SIB CE-04-03

Feb 1, 2010

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.

Safety Information Bulletin
  • Cessna 172
  • Cessna 180
  • Cessna 185
  • Reims Aviation Cessna 172
  • Reims Aviation Cessna 180
  • Reims Aviation Cessna 185

EASA SIB 2008-54

Jun 26, 2008

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.

Safety Information Bulletin
  • Cessna 150
  • Cessna 172
  • Cessna 177
  • Cessna 180
  • Cessna 182
  • Cessna 185
  • Cessna 188
  • Cessna 206
  • Cessna 207
  • Cessna 210
  • Reims Aviation

EASA SIB 2007-40

Nov 12, 2007

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.

Safety Information Bulletin
  • Cessna 180
  • Cessna 182
  • Cessna 185

EASA SIB 2007-36

Oct 5, 2007

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.

Safety Information Bulletin
  • Cessna 150
  • Cessna 172
  • Cessna P172
  • Cessna 175
  • Cessna 180
  • Cessna 182
  • Cessna 185
  • Cessna 205
  • Cessna 206
  • Cessna 210
  • Cessna 336
  • Cessna 337