AD/CESSNA 400/56 - Upper Inner Cabin Door Handle and Locking Mechanism - Inspection

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Legislation au F2006B08342 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 400 Series Aeroplanes

 

AD/CESSNA 400/56 Upper Inner Cabin Door Handle and

Locking Mechanism - Inspection

Applicability: All model 402B with S/Nos. 402B-1301 to 402B-1349.

All model 404 with S/Nos. 404-0201 to 404-0237.

All model 414A with S/Nos. 414A-0001 to 414A-0059. All model 421C with S/Nos. 421C-0401 to 421C-0504.

 

Document: Cessna SL No. ME 78-21.

 

Compliance: Within 100 hours time in service after 30 September 1978.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


9/78

Overview

The Civil Aviation Regulations 1998 were enacted by the Australian Parliament to ensure the safety of civil aviation operations within Australia. This legislation, administered by the Civil Aviation Safety Authority (CASA), seeks to fill the legislative gap in maintaining stringent safety standards and procedures in civil aviation. One such legislative instrument, F2006B08342, amends the Civil Aviation Regulations 1998 to address specific safety concerns regarding certain Cessna 400 series aeroplanes. This directive, known as AD/CESSNA 400/56, mandates inspections of the upper inner cabin door handle and locking mechanism for particular model serial numbers to mitigate potential safety risks. The policy objective is to enhance aviation safety by ensuring these aircraft meet specific airworthiness standards, thereby protecting passengers and crew. The Cessna 400 series aeroplanes targeted by AD/CESSNA 400/56 include models 402B, 404, 414A, and 421C with specified serial numbers. The directive requires inspections to be conducted within 100 hours of time in service after 30 September 1978, as detailed in Cessna Service Letter No. ME 78-21. This targeted approach aims to identify and rectify any deficiencies in the upper inner cabin door handle and locking mechanism, thereby ensuring continued compliance with airworthiness directives and enhancing overall flight safety.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, focusing on the Cessna 400 Series Aeroplanes. This legislation mandates that certain Cessna 400 series aircraft, specifically those with serial numbers within defined ranges, must undergo an inspection of their upper inner cabin door handle and locking mechanism. The models and serial numbers in question include Cessna 402B with serial numbers ranging from 402B-1301 to 402B-1349, Cessna 404 with serial numbers from 404-0201 to 404-0237, Cessna 414A with serial numbers from 414A-0001 to 414A-0059, and Cessna 421C with serial numbers from 421C-0401 to 421C-0504. Compliance with this directive requires the inspection to be conducted within 100 hours of time in service after 30 September 1978. This directive applies to operators of these specific aircraft, ensuring that the specified maintenance is carried out to meet safety standards set by CASA. The legislation extends its reach to any entity or individual operating these aircraft within Australian airspace, thus ensuring adherence to national aviation safety standards.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, Part 39 - 105, concerning Cessna 400 Series Aeroplanes, are found in the Airworthiness Directives (AD). Specifically, AD/CESSNA 400/56 addresses the inspection requirements for the upper inner cabin door handle and locking mechanism. This directive applies to all model 402B with serial numbers (S/Nos.) 402B-1301 to 402B-1349, all model 404 with S/Nos. 404-0201 to 404-0237, all model 414A with S/Nos. 414A-0001 to 414A-0059, and all model 421C with S/Nos. 421C-0401 to 421C-0504. Compliance with this directive is mandatory and must be carried out within 100 hours of time in service after 30 September 1978, as referenced in Cessna Service Letter (SL) No. ME 78-21. The Act imposes specific obligations on the operators of the specified Cessna 400 Series aeroplanes. Operators must ensure that the upper inner cabin door handle and locking mechanism are inspected in accordance with the specified document (Cessna SL No. ME 78-21) within the timeframe provided. This inspection is crucial for maintaining the airworthiness of the aircraft, ensuring that the door handle and locking mechanism are in proper working order and do not pose a safety risk. Failure to comply with these requirements can lead to serious safety concerns and non-compliance with regulatory standards. Breach of these directives can result in significant consequences. The Civil Aviation Safety Authority (CASA) may take enforcement action against operators who fail to comply with the mandated inspections. Such actions can include fines, grounding of the aircraft, and other administrative penalties. While the specific penalties are not detailed in the provided text, it is clear that non-compliance can lead to serious repercussions for the operators. The severity of the penalties may vary depending on the circumstances of the breach, but it is evident that the legislation is designed to ensure strict adherence to safety standards.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.