AD/T53/20 - Accessory Drive Carrier

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 



AlliedSignal (Lycoming) Turbine Engines - T53 Series

 

AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

 

AD/T53/20 Accessory Drive Carrier 8/2000

Applicability: AlliedSignal (formerly Textron Lycoming) T5313B, T5317A, T53-L-703 series and T53 military series engines.

 

Requirement: Inspect the accessory drive carrier assembly in accordance with one of the following, as applicable, AlliedSignal Aerospace Service Bulletins.

 

Engine Model No.

 

1. T53-L-13B, T53-L-13BS/SA and T53-

L-13BS/SB series engines:


Service Bulletin No.

 

SB T53-L-13B-A0092 Revision 1 dated July 1,1997.

 

2.    T5313B and T5317A series engines: SB T5313B/17A-A0092 Revision 1 dated

July 1, 1997.

 

3.    T53-L-703 series engines: SB T53-L-703-A0092 Revision 1 dated

July 1, 1997.

 

Note 1: FAA AD 97-21-07 R1 Amendment 39-10610 refers.

 

Compliance:  Unless previously accomplished, within 100 hours time in service from the effective date of this Directive or prior to 7 March 2001, whichever occurs first.

 

Note 2: AD/T53/19 must be incorporated prior to or at the same time as this Directive is accomplished.

 

This Airworthiness Directive becomes effective on 10 August 2000.

 

Background:  This Directive is raised to require a one time visual inspection of the accessory drive carrier assembly for affected serial numbers. Failure to remove a defective assembly could result in an N2 overspeed with possible uncontained engine failure.


 

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 27 June 2000


The above AD is notified in the Commonwealth of Australia Gazette on 12 July 2000.

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Government, establish the regulatory framework governing civil aviation in Australia. This legislation, overseen by the Civil Aviation Safety Authority (CASA), was introduced to address the need for a comprehensive and consistent set of regulations to ensure the safety and efficiency of civil aviation operations within the country. A notable aspect of the regulations is the incorporation of Airworthiness Directives (ADs), which are issued under subregulation 39.1 (1) of the Civil Aviation Regulations 1998, to address specific safety concerns identified with particular aircraft or aeronautical products. The policy objective behind these ADs is to mandate necessary actions to rectify unsafe conditions, thereby enhancing the overall safety of civil aviation. For instance, AD/T53/20, issued on 8 August 2000, mandates a visual inspection of the accessory drive carrier assembly for certain AlliedSignal (Lycoming) Turbine Engines to prevent potential engine failure. This directive became effective on 10 August 2000 and was published in the Commonwealth of Australia Gazette on 12 July 2000.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 106, mandate that the Civil Aviation Safety Authority (CASA) must issue Airworthiness Directives to ensure the safety of aeronautical products within the Commonwealth of Australia. The directive in question, AD/T53/20, pertains to the inspection of the accessory drive carrier assembly for certain AlliedSignal (formerly Textron Lycoming) T53 series engines, including the T5313B, T5317A, T53-L-703 series, and T53 military series engines. This directive applies to all aircraft equipped with the specified engine models and necessitates a visual inspection in accordance with the relevant AlliedSignal Aerospace Service Bulletins. The inspection must be completed within 100 hours of the directive's effective date or before 7 March 2001, whichever comes first, with an additional requirement that another directive, AD/T53/19, be incorporated concurrently. This directive was issued to address potential safety hazards, particularly the risk of uncontained engine failure due to N2 overspeed, and was published in the Commonwealth of Australia Gazette on 12 July 2000.

Key Provisions

The Civil Aviation Regulations 1998, particularly in Part 39 - 106, outline a significant Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority (CASA). Specifically, AD/T53/20 pertains to the inspection of the accessory drive carrier assembly for certain AlliedSignal (Lycoming) T53 series turbine engines (section 1). The AD applies to the T53-L-13B, T53-L-13BS/SA, T53-L-13BS/SB, T53-L-703 series, and T53 military series engines (section 2). The directive requires a visual inspection of the accessory drive carrier assembly to ensure it is free from defects that could lead to engine failure (section 3). The inspection must be conducted in accordance with specific AlliedSignal Aerospace Service Bulletins, which are referenced in the directive (section 3). The AD imposes clear obligations on the parties involved, such as aircraft operators and maintenance personnel. They are required to conduct the inspection as outlined in the directive and adhere to the specified service bulletins (section 3). The directive mandates that the inspection must be completed within 100 hours of the AD's effective date or before 7 March 2001, whichever comes first (section 4). Furthermore, it is noted that another directive, AD/T53/19, must be incorporated at the same time or prior to this inspection (section 4). Failure to comply with this AD can lead to serious safety implications, including the risk of N2 overspeed and uncontained engine failure, which could endanger flight safety (section 1). There are no explicit penalties stated within the directive itself, but non-compliance with CASA directives generally can lead to enforcement actions under the Civil Aviation Act 1988. Such actions may include fines and other civil or criminal penalties for severe breaches. The severity of the consequences often depends on the extent of non-compliance and the potential risk posed to aviation safety.

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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.