AD/DH 104/26 - Rudder Control Pedal Reversal Lever - Inspection

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Legislation au F2006B08868 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


DH 104 (Dove) Series Aeroplanes

 

AD/DH 104/26 Rudder Control Pedal Reversal Lever - Inspection 2/71

Applicability: All models.

 

Document: Hawker Siddeley TNS CT(104) No. 219.

 

Compliance: Within 100 hours time in service after 31 March 1971 and thereafter at intervals not exceeding 2400 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, are integral to the regulation of civil aviation within Australia. One particular legislative instrument under this act, F2006B08868, addresses the safety of the Hawker Siddeley DH 104 Dove series aeroplanes through Airworthiness Directives. This legislation was introduced to ensure the continued airworthiness and safety of the Dove series aeroplanes, which are used for various civilian purposes. The policy objective is to maintain and enhance aviation safety by mandating regular inspections of critical components such as the rudder control pedal reversal lever, which is essential for the proper operation and control of the aircraft. By requiring these inspections at specified intervals, the regulations aim to prevent potential mechanical failures that could compromise flight safety.

Scope and Application

The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B08868, pertain specifically to the Hawker Siddeley DH 104 (Dove) series aeroplanes under Part 39 - 105, which outlines the Civil Aviation Safety Authority Schedule of Airworthiness Directives. This regulation applies to all models of the Dove series aeroplanes and mandates a critical inspection of the rudder control pedal reversal lever as documented in Hawker Siddeley TNS CT(104) No. 219. The directive requires compliance within 100 hours of time in service after 31 March 1971, with subsequent inspections to be conducted at intervals not exceeding 2400 hours of time in service. The Act operates on a Commonwealth level, enforcing stringent safety standards across Australia to ensure the airworthiness of these aircraft, while the scope of its application is limited to the specified models and maintenance schedules detailed within the directive.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, pertains to airworthiness directives for specific aircraft, such as the DH 104 (Dove) Series Aeroplanes. One such directive, AD/DH 104/26, focuses on the rudder control pedal reversal lever and mandates inspections for all models (AD/DH 104/26). According to the document Hawker Siddeley TNS CT(104) No. 219, the requirement is to inspect the rudder control pedal reversal lever within 100 hours of time in service after 31 March 1971. After this initial inspection, the directive mandates further inspections at intervals not exceeding 2400 hours of time in service (AD/DH 104/26). Operators of DH 104 (Dove) Series Aeroplanes must ensure that the specified inspections are conducted as per the stipulated intervals. These inspections are critical to maintaining the aircraft's airworthiness and ensuring the safety of all personnel onboard. Failure to comply with the inspection requirements can lead to serious safety issues and potential legal ramifications. The regulations are designed to ensure that the rudder control pedal reversal lever remains in a functional state, which is vital for the safe operation of the aircraft. Non-compliance with the inspection requirements set forth in AD/DH 104/26 may result in serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce penalties for violations of these regulations. The specific nature and severity of these penalties can vary, but they may include fines, operational restrictions, or even the grounding of the aircraft until the required inspections are satisfactorily completed. The overarching goal of these measures is to ensure that all aircraft operated under the Civil Aviation Regulations 1998 maintain the highest standards of safety and reliability. In the event of a breach of these regulations, the consequences can be both civil and criminal, depending on the severity and intent behind the non-compliance. For instance, serious breaches that result in accidents or endanger public safety may lead to criminal charges, which could result in significant fines and imprisonment for responsible individuals or entities. Additionally, civil penalties may include substantial financial penalties, which can impact the operational costs of the airline or aircraft owner. Therefore, it is imperative for all parties governed by these regulations to adhere strictly to the mandated inspection intervals and procedures to avoid these severe consequences.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Inspection
Compliance Periods

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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.