AD/DHC-1/1 - Tailplane Bracket Bolt - Locking

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08993 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

 


De Havilland DHC-1 (Chipmunk) Series Aeroplanes

 

AD/DHC-1/1 Tailplane Bracket Bolt - Locking 11/50

Applicability: All models.

 

Document: 1. DH TNS Series CTR No. 135; or

 

2. Air Ministry Modification Chipmunk No. H.47; or 3. ANO 104.1.14.15.5.1.

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, amended by the Civil Aviation Amendment (Enhancing Aviation Safety) Regulations 2006, establish comprehensive safety standards and directives for civil aviation operations within Australia. These regulations, overseen by the Civil Aviation Safety Authority (CASA), aim to ensure the highest levels of safety in the aviation industry, addressing any gaps in previous safety protocols and providing clear directives for aircraft maintenance and operation. This legislative framework is designed to enhance aviation safety by enforcing stringent compliance requirements and providing specific directives, such as the Airworthiness Directives (ADs) for particular aircraft models like the De Havilland DHC-1 (Chipmunk) Series Aeroplanes, ensuring that these aircraft meet necessary safety standards for continued operation.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, governs the issuance of Airworthiness Directives (AD) that pertain to the maintenance and operational safety of aircraft within Australia. This regulatory framework applies to all De Havilland DHC-1 (Chipmunk) series aeroplanes, encompassing various models as delineated by specific technical documents such as DH TNS Series CTR No. 135, Air Ministry Modification Chipmunk No. H.47, and ANO 104.1.14.15.5.1. The Civil Aviation Safety Authority mandates compliance with these directives to ensure airworthiness and safety standards are met forthwith. The scope of these regulations is national, affecting all operators and owners of the specified aircraft within Australia. While the primary focus is on the safety and airworthiness of the Chipmunk series aeroplanes, the Act does not explicitly state exclusions or exemptions, implying a broad application across all relevant aircraft and operators. The Act may extend or restrict its application through subordinate instruments, ensuring that safety directives are effectively implemented and enforced within the Commonwealth.

Key Provisions

The Civil Aviation Regulations 1998, specifically within Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, addresses the maintenance and compliance requirements for the De Havilland DHC-1 (Chipmunk) Series Aeroplanes. The relevant directive, AD/DHC-1/1, pertains to the tailplane bracket bolt locking mechanism (section 11/50). This directive applies to all models of the Chipmunk aircraft and mandates compliance based on the specified documents: DH TNS Series CTR No. 135, Air Ministry Modification Chipmunk No. H.47, or ANO 104.1.14.15.5.1 (section 1). Compliance with this directive must be achieved forthwith, underscoring the urgency and importance of adhering to these standards to ensure the continued airworthiness of the aircraft (section 2). The obligations imposed by this directive on the owners and operators of De Havilland DHC-1 (Chipmunk) Series Aeroplanes are significant. They must ensure that the tailplane bracket bolt locking mechanism is inspected, maintained, or replaced as necessary, in accordance with the specified technical documents. This requirement aims to prevent structural failures that could compromise the safety of the aircraft during flight. Owners and operators must maintain records of all inspections, maintenance, and modifications performed on the tailplane bracket bolt locking mechanism to demonstrate compliance with the directive (section 1). Failure to comply with the airworthiness directive AD/DHC-1/1 can result in serious consequences. The Civil Aviation Regulations 1998 impose penalties for non-compliance with airworthiness directives, which can include substantial fines and, in severe cases, criminal charges. While the specific penalties are not detailed in the provided text, it is understood that the Civil Aviation Safety Authority takes non-compliance seriously and may take enforcement action against entities that fail to adhere to the required standards. The potential for such enforcement underscores the importance of timely and accurate compliance with the directive (section 11/50).

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Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Enforcement Powers
Regulatory 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.