EASA Regulations for Cessna 337

7 airworthiness directives and regulations affecting Cessna 337.

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New ADs and bulletins for Cessna 337, summarized like the ones below, every Monday.

EASA SIB CE-12-41

Aug 14, 2012

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.

Safety Information Bulletin
  • Cessna 177
  • Cessna F177
  • Cessna 182
  • Cessna F182
  • Cessna 206
  • Cessna 207
  • Cessna 210
  • Cessna 337
  • Cessna F337

EASA SIB CE-12-24R1

Jun 4, 2012

Cessna 336/337 and (formerly Reims) F337 Aeroplanes — Frayed Flap Extend Cables

The Special Airworthiness Information Bulletin SAIB: CE-12-24R1 is an FAA advisory regarding frayed flap extend cables on Cessna Models F337, 336, and 337 airplanes, including those formerly produced by Reims. It informs owners, operators, and maintenance personnel about the potential for cable wear and recommends inspection practices to ensure continued airworthiness. This bulletin is informational and does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin
  • Cessna 336
  • Cessna 337
  • Reims F337

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-10-20R1

May 21, 2010

Cessna Aircraft Company 336, 337 and (Reims) F337 aeroplanes - Wingtip Extensions

The Cessna Aircraft Company 336, 337 and (Reims) F337 aeroplanes - Wingtip Extensions Special Airworthiness Information Bulletin (SAIB: CE-10-20 R1) is an FAA advisory bulletin addressing safety concerns related to wingtip extensions on Cessna Models 336, 337, and F337 (Reims) series airplanes. It highlights potential structural issues such as wrinkled skins, cracks, and loose wing tips following modifications with Supplemental Type Certificates (STCs) for extended wingtips and winglets. The bulletin provides guidance to enhance safety but does not mandate regulatory action.

Safety Information Bulletin
  • Cessna 336
  • Cessna 337
  • Reims F337

EASA SIB CE-09-10

Feb 26, 2009

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.

Safety Information Bulletin
  • Cessna 170
  • Cessna 172
  • Cessna 182
  • Cessna 206
  • Cessna 210
  • Cessna 337

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