AD/PA-32/37 - Forward Baggage Door - Inspection

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, address various aspects of aviation safety and operational standards, including the establishment of specific airworthiness directives for different aircraft models. One such directive is AD/PA-32/37, which concerns the Piper PA-32 (Cherokee Six) series aeroplanes. This directive was introduced to ensure the ongoing airworthiness and safety of these specific aircraft models by mandating regular inspections of the forward baggage door. The policy objective is to maintain the integrity and safety of the aircraft by identifying and addressing potential issues with the forward baggage door through periodic inspections, as outlined in the directive. This requirement is applicable to all relevant models and serial numbers, with inspections needing to be performed within certain time intervals post-modification or after a specific period of service. Compliance with this directive is crucial to ensure that any issues are identified and rectified promptly, thereby maintaining the overall safety standards of civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning Airworthiness Directives, govern the safety standards for the Piper PA-32 (Cherokee Six) series aeroplanes. This legislation applies to all PA32-260 models with serial numbers ranging from 32-01 to 32-7500039, as well as PA-32-300 models with serial numbers from 32-40001 to 32-7540147. The regulation mandates inspections on the forward baggage door in accordance with Piper Service Bulletin No. 463. The inspections are required within 100 hours of time in service after 13 May 1975, and subsequently, at intervals not exceeding 10 hours of time in service until the aircraft is modified with the installation of Piper Kit 760-972V. For aircraft adhering to ANO 100.5.1, this directive must be documented on the maintenance release as maintenance required. In instances where the pilot in command performs the inspection, certification is not mandatory; however, in all other cases, certification is required and may be provided on the maintenance release or by a Licensed Aircraft Maintenance Engineer. The scope and application of this directive are comprehensive, ensuring the continued safety and airworthiness of the specified aircraft models across the Commonwealth of Australia.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39, specifically Section 105, sets out the airworthiness directives for various aircraft, including the Piper PA-32 (Cherokee Six) series aeroplanes. The directive AD/PA-32/37 pertains to the forward baggage door inspection for certain models of the Piper PA-32 aeroplanes. Specifically, this directive applies to all models PA32-260 with serial numbers 32-01 to 32-7500039 and PA-32-300 with serial numbers 32-40001 to 32-7540147 (105.01). Compliance with this directive is mandatory and must occur within 100 hours of the aeroplane's time in service after 13 May 1975. Following this initial inspection, the inspection must be repeated at intervals not exceeding 10 hours of time in service until the aeroplane is modified by the installation of Piper Kit 760-972V. The obligations imposed by this directive require that the specified models of the Piper PA-32 aeroplanes undergo a thorough inspection of the forward baggage door. This inspection is a critical safety measure to ensure that the aeroplane remains airworthy and complies with the safety standards set by the Civil Aviation Safety Authority (CASA). For aircraft that are maintained in accordance with ANO 100.5.1, this directive must be recorded on the maintenance release as "maintenance required" (105.02). Additionally, the inspection can be performed by the pilot in command, in which case certification is not required. However, if the inspection is performed by anyone other than the pilot in command, certification must be made on the maintenance release by a Licensed Aircraft Maintenance Engineer (105.03). Failure to comply with the airworthiness directive AD/PA-32/37 may result in significant civil or criminal consequences. The exact penalties for non-compliance with the Civil Aviation Regulations are not specified within the directive itself, but generally, violations of these regulations can lead to substantial fines, potential grounding of the aircraft, and other enforcement actions by CASA. The severity of the penalties would depend on the specifics of the non-compliance and could result in both civil and criminal liability for the operator of the aircraft. Ensuring adherence to these directives is crucial for maintaining the safety and airworthiness of the aircraft and avoiding any legal repercussions.