COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-28 Series Aeroplanes
AD/PA-28/36 Stabilator Hinge Attaching Bolts - Inspection 5/72
Applicability: Models PA-28-140 with S/Nos. 28-7225001 to 28-7225240. PA-28-280 with S/Nos. 28-7205001 to 28-7205225. PA-28-235 with S/Nos. 28-7210001 to 28-7210018. PA-
28R- 200 with S/Nos. 28R-7235001 to 28R-7235125.
Document: Piper SB No. 350.
Compliance: Prior to further flight after 24 May 1972.
Overview
The Civil Aviation Regulations 1998, as amended through F2006B05595, are designed to enhance aviation safety by introducing specific Airworthiness Directives, such as AD/PA-28/36, which focuses on the stabilator hinge attaching bolts for certain Piper PA-28 series aeroplanes. This legislative instrument was introduced to address safety concerns related to the stabilator hinge attaching bolts in these specific models, ensuring that any potential issues are identified and rectified to prevent accidents or failures during flight. The enacting body for these regulations is the Parliament of the Commonwealth of Australia, with a clear policy objective to maintain and improve the safety standards within the civil aviation sector. The regulations mandate that inspections be conducted prior to further flight after a specified date to ensure compliance and mitigate any risks associated with the identified problem.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39, specifically address the airworthiness directives for certain Piper PA-28 series aeroplanes, which are crucial in ensuring safety within the aviation sector. The directive AD/PA-28/36 pertains to the stabilator hinge attaching bolts and mandates an inspection for compliance prior to further flight after 24 May 1972. The legislation applies to specific models of the Piper PA-28 series, namely the PA-28-140 with serial numbers ranging from 28-7225001 to 28-7225240, the PA-28-280 with serial numbers from 28-7205001 to 28-7205225, the PA-28-235 with serial numbers from 28-7210001 to 28-7210018, and the PA-28R-200 with serial numbers from 28R-7235001 to 28R-7235125. This directive is enforced under the jurisdiction of the Civil Aviation Safety Authority, reflecting the Commonwealth's commitment to stringent safety standards in civil aviation. The scope of this legislation is confined to these specific models and serial number ranges, with compliance required before any further flight post the specified date.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, detail the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives for certain Piper PA-28 series aeroplanes. One such directive, AD/PA-28/36, mandates an inspection of the stabilator hinge attaching bolts on specific models and serial numbers (section 5/72). The directive applies to PA-28-140 models with serial numbers ranging from 28-7225001 to 28-7225240, PA-28-280 models with serial numbers from 28-7205001 to 28-7205225, PA-28-235 models with serial numbers from 28-7210001 to 28-7210018, and PA-28R-200 models with serial numbers from 28R-7235001 to 28R-7235125. Compliance with this directive must be achieved prior to further flight after 24 May 1972, as referenced in Piper Service Bulletin No. 350.
The obligations imposed by this directive require aircraft operators and maintenance personnel to conduct a thorough inspection of the stabilator hinge attaching bolts as per the specifications outlined in Piper Service Bulletin No. 350. This inspection must be completed before any subsequent flight operations of the affected aircraft models to ensure compliance with the regulatory requirements. Failure to adhere to these requirements could result in non-compliance with civil aviation regulations, potentially leading to safety hazards or operational restrictions.
In the event of non-compliance with the AD/PA-28/36 directive, there may be significant civil and criminal consequences. While specific penalties are not detailed within the text of this directive, it is within the broader regulatory framework of the Civil Aviation Regulations 1998 that such penalties would be determined. Typically, breaches of aviation safety directives can result in fines, operational grounding of the aircraft, and potential legal actions against the operators or maintenance personnel responsible for ensuring compliance. The exact penalties would depend on the severity of the non-compliance and any resultant safety risks or operational disruptions.