COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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 CASR 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.
Aerospatiale (Socata) TBM 700 Series Aeroplanes
AD/TBM 700/36 Pilot Door Frame 11/2004 DM
Applicability: Model TBM 700 aircraft equipped with a pilot door, serial number 126, 129, 157, 165, 174, 185, 188, 231, 234, 240, 250, 252, 270, 280, or 282 through 286.
Requirement: Action in accordance with Socata Service Bulletin No. 70-117-53, dated March 2004.
Note: DGAC AD F-2004-149 refers.
Compliance: At the next scheduled yearly inspection after 22 September 2004 or before 30 June 2005, whichever occurs first.
This Airworthiness Directive becomes effective on 22 September 2004.
Background: A pilot door frame non-conformity occurred on certain aircraft during production. This anomaly has resulted in the requirement for the installation of a reinforcement plate.
David Villiers
Delegate of the Civil Aviation Safety Authority 16 September 2004
The above AD is notified in the Commonwealth of Australia Gazette on 22 September 2004.
Page 1 of 1
Overview
The Civil Aviation Safety Regulations 1998 were enacted to establish a framework for the maintenance of airworthiness of aircraft operating in Australia. This regulation plays a critical role in ensuring that all aircraft meet the necessary safety standards to protect passengers, crew, and the general public. One of the specific instruments issued under these regulations is the Airworthiness Directive (AD) concerning the Aerospatiale (Socata) TBM 700 Series Aeroplanes, issued by a delegate of the Civil Aviation Safety Authority (CASA) on 16 September 2004. This AD was introduced to address a non-conformity issue identified in the pilot door frame of certain TBM 700 aircraft, which required a reinforcement plate to be installed. The policy objective behind this directive is to ensure the continued safety of these aircraft by mandating specific corrective actions, thus mitigating any potential safety risks associated with the identified anomaly.
Scope and Application
The Civil Aviation Safety Regulations 1998, specifically PART 39 - 105, pertains to the safety directives issued by the Civil Aviation Safety Authority (CASA) in Australia. These regulations apply to the maintenance and operation of aircraft, with a particular focus on ensuring that the aircraft meet specific airworthiness standards. This particular Airworthiness Directive (AD) applies to Aerospatiale (Socata) TBM 700 Series Aeroplanes that are equipped with a pilot door and meet certain serial number criteria. The directive mandates specific actions to address a previously identified unsafe condition concerning the pilot door frame, requiring the installation of a reinforcement plate in accordance with Socata Service Bulletin No. 70-117-53. This action must be completed at the next scheduled yearly inspection after the issuance of the AD, which is 22 September 2004, or before 30 June 2005, whichever occurs first. The AD is applicable within the Commonwealth of Australia and is enforced by CASA, with the directive becoming effective from the date of its notification, which is 22 September 2004.
Key Provisions
The main operative sections of the Airworthiness Directive (AD/TBM 700/36) (section 1) pertain to the applicability and requirements for the Aerospatiale (Socata) TBM 700 Series Aeroplanes. Specifically, this directive applies to aircraft with serial numbers 126, 129, 157, 165, 174, 185, 188, 231, 234, 240, 250, 252, 270, 280, and 282 through 286. The requirement (section 2) mandates that the action specified in Socata Service Bulletin No. 70-117-53, dated March 2004, be implemented to address a non-conformity in the pilot door frame. The directive becomes effective on 22 September 2004 and must be complied with at the next scheduled yearly inspection after this date, but no later than 30 June 2005.
The obligations imposed by this directive on the parties governed by it are primarily centred around the timely implementation of the specified corrective actions. Aircraft operators or owners must ensure that the necessary reinforcement plate is installed on the pilot door frame as detailed in the Socata Service Bulletin No. 70-117-53. Failure to comply with these directives may result in the aircraft being deemed unairworthy, which could prevent it from being operated until the required modifications are made. Additionally, operators must adhere to the compliance timeline, ensuring that the corrective action is completed by the stipulated date to maintain airworthiness.
Should there be a breach of the requirements outlined in this Airworthiness Directive, there are potential civil and criminal consequences. While the specific penalties are not detailed in the directive itself, under the broader framework of the Civil Aviation Safety Regulations 1998, breaches of airworthiness directives can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include fines, penalties, or even legal proceedings against the operators or owners of the aircraft. The severity of these penalties can vary, but they are intended to enforce compliance and ensure the continued safety of aviation operations.