AD/CESSNA 188/2 - Control Column Bearing Blocks and Bobweight

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Legislation au F2006B05155 Not in force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 188 (Agwagon) Series Aeroplanes

 

AD/CESSNA 188/2 Control Column Bearing Blocks

and Bobweight


11/67

 

Applicability: All models with S/Nos. 0001 to 0051, 0053 to 0129, 0131 to 0135, 0137 to 0143,

0145, 0146, 0147, 0151, 0152, 0153, 0155, 0157, 0158, 0161, 0162, 0169, 0170,

0171, 0172 and 0174.

 

Requirement: Action in accordance with Cessna Service Kit No. 188-5. (Cessna SL 67-1 Item 1 also refers).

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998 were enacted in 1998 to ensure the safety of civil aviation operations within Australia, as well as to harmonise Australian civil aviation regulations with international standards. Part 39, in particular, deals with airworthiness directives, which are mandatory instructions issued by the Civil Aviation Safety Authority (CASA) to address safety issues in aircraft. One such directive, AD/CESSNA 188/2, pertains to the control column bearing blocks and bobweight for specific Cessna 188 (Agwagon) series aeroplanes. This directive was introduced to address identified safety issues within the specified models, ensuring compliance with the safety standards set by CASA. The AD/CESSNA 188/2 requires that all applicable Cessna 188 models must implement the action specified in Cessna Service Kit No. 188-5 to rectify the identified issues with the control column bearing blocks and bobweight. The directive mandates compliance forthwith, emphasising the importance of immediate action to maintain the airworthiness of these aircraft. This regulation is enforced by the Civil Aviation Safety Authority, which operates under the authority of the Australian Government to ensure that all civil aviation activities within Australia adhere to the highest safety standards.

Scope and Application

The Civil Aviation Safety Authority (CASA) administers the Civil Aviation Regulations 1998, specifically within Part 39 - 105, which outlines the Schedule of Airworthiness Directives for various aircraft, including the Cessna 188 (Agwagon) Series Aeroplanes. This particular directive, AD/CESSNA 188/2, applies to all models of the Cessna 188 series with specific serial numbers, ranging from 0001 to 0051, 0053 to 0129, 0131 to 0135, 0137 to 0143, 0145, 0146, 0147, 0151, 0152, 0153, 0155, 0157, 0158, 0161, 0162, 0169, 0170, 0171, 0172, and 0174. The directive mandates action in accordance with Cessna Service Kit No. 188-5, with additional reference to Cessna SL 67-1 Item 1. Compliance with this directive is required forthwith, ensuring that all specified aircraft models adhere to the outlined safety measures to maintain their airworthiness. The directive encompasses all entities and persons responsible for the maintenance and operation of these particular aircraft models within the Commonwealth of Australia.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39 - 105, contain the Schedule of Airworthiness Directives which addresses various aircraft types, including the Cessna 188 (Agwagon) Series Aeroplanes. Section AD/CESSNA 188/2 pertains to the control column bearing blocks and bobweight. This section mandates action in accordance with Cessna Service Kit No. 188-5 and also references Cessna SL 67-1 Item 1 for additional guidance. This directive applies to all models within specified serial number ranges, as detailed in the document. Under the Civil Aviation Regulations, the obligations for the parties governed by this directive are clear. Owners or operators of Cessna 188 (Agwagon) Series Aeroplanes with the specified serial numbers must comply with the directive immediately. This involves implementing the corrective action as outlined in Cessna Service Kit No. 188-5, ensuring that the control column bearing blocks and bobweight are addressed in accordance with the manufacturer’s instructions. The requirement for compliance is immediate, underscoring the importance of maintaining the airworthiness of these aircraft. Failure to comply with the provisions outlined in the Airworthiness Directives can lead to significant consequences. The regulations do not explicitly state offences or penalties within this specific directive, but general provisions within the Civil Aviation Act 1988 and associated regulations may apply. Non-compliance could result in enforcement actions, including fines or other civil penalties. Additionally, in severe cases, it could lead to criminal charges if the non-compliance is deemed to endanger safety. The specific penalties would depend on the nature and severity of the non-compliance, as well as the relevant legislative framework in place.

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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.