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-28/38 Stabilator Hinge Attaching Bolts - Inspection 6/78
Applicability: All models referenced in requirement documents. Document: 1. Piper SL No. 614; or
2. FAA AD 72-14-7.
Compliance: Within 100 hours time in service after 31 August 1972.
Overview
The Civil Aviation Regulations 1998, specifically within Part 39 - 105, addresses the safety of Piper PA-28 Series Aeroplanes through Airworthiness Directives, such as AD/PA-28/38. This directive was enacted to address the issue of stabilator hinge attaching bolts, which were identified as a potential safety risk. The policy objective of this regulation, issued by the Civil Aviation Safety Authority, is to ensure that the specified inspection of the stabilator hinge attaching bolts is carried out within 100 hours of time in service after 31 August 1972, thereby enhancing the safety and reliability of the aircraft. This legislative instrument ensures that all models of Piper PA-28 Series Aeroplanes comply with the stringent safety standards mandated by the Civil Aviation Regulations.
Scope and Application
The Civil Aviation Safety Authority (CASA) has issued a directive under the Civil Aviation Regulations 1998, specifically targeting the Piper PA-28 series aeroplanes. This directive mandates an inspection of the stabilator hinge attaching bolts on all models as referenced in the requirement documents, which include Piper Service Letter No. 614 or FAA AD 72-14-7. The directive applies to all Piper PA-28 aeroplanes that have been in service for 100 hours after 31 August 1972, ensuring that these aircraft meet the necessary safety standards to maintain airworthiness. This regulation is applicable across Australia and is enforced by CASA, the national civil aviation regulator. The directive does not specify any exclusions, exemptions, or thresholds, meaning that all applicable aircraft must comply with the prescribed inspection requirements without exception. Subordinate instruments may provide additional details or modifications to the application of this directive, ensuring continuous alignment with safety standards and operational requirements.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, include a Schedule of Airworthiness Directives (AD) aimed at ensuring the safety of aircraft operations. Under this part, AD/PA-28/38 pertains to the stabilator hinge attaching bolts on Piper PA-28 series aeroplanes (section 39-105). This AD requires an inspection of the stabilator hinge attaching bolts on all applicable models within 100 hours of time in service after 31 August 1972 (section 39-105). The applicable models are identified by either Piper Service Letter No. 614 or FAA AD 72-14-7 (section 39-105).
Entities and individuals governed by this legislation must adhere to the specified timeframes and procedures for inspecting the stabilator hinge attaching bolts as outlined in the AD. This involves ensuring that the bolts are checked for any signs of wear, damage, or fatigue that could compromise the aircraft's stability and control. Proper documentation of these inspections must be maintained to demonstrate compliance with the regulatory requirements.
Failure to comply with the inspection requirements stipulated in AD/PA-28/38 can lead to significant consequences. The Civil Aviation Safety Authority (CASA) may take enforcement action against non-compliant entities or individuals. The potential penalties for breaches of these regulations can include fines and other administrative actions. The specific penalties are not detailed in the provided excerpt, but they are likely to be severe given the critical nature of the required inspections for flight safety. Ensuring adherence to these provisions is paramount to maintaining the airworthiness and safety of Piper PA-28 series aeroplanes.