COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F27 Series Aeroplanes
AD/F27/93 Nose Gear Down Lock Latch - Inspection 2/78
Applicability: All models.
Requirement: Inspect the nose landing gear down lock latch for conformity with the profile shown at page 6 of Dowty Rotol SB 32-37 dated September 1962 or Dowty Rotol Drawing 200061330.
Incorrectly profiled latches must be replaced before further flight.
Compliance: Unless previously accomplished since 1 October 1977, within 300 hours time in service after 30 December 1977.
Overview
The Civil Aviation Regulations 1998, amended through Legislative Instrument F2006B09744, address specific safety concerns regarding the maintenance and operation of Fokker F27 Series Aeroplanes. This legislative instrument, enacted under the authority of the Commonwealth of Australia, focuses on ensuring the airworthiness of these aircraft by setting stringent maintenance directives. The policy objective behind these regulations is to enhance the safety standards of civil aviation by mandating regular inspections and necessary repairs to critical components, such as the nose gear down lock latch, to prevent potential operational failures and ensure the safety of passengers and crew.
The regulations introduced by F2006B09744 are designed to close gaps in safety protocols identified in the operation of Fokker F27 aircraft, particularly concerning the nose gear down lock latch. By requiring inspections and replacements of non-conforming parts, the legislation aims to maintain the structural integrity and operational safety of the aircraft, thereby aligning with the overarching goal of the Civil Aviation Safety Authority to uphold high safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives for Fokker F27 Series aeroplanes. This legislation mandates an inspection of the nose landing gear down lock latch to ensure it conforms with the profile specified in Dowty Rotol SB 32-37 dated September 1962 or Dowty Rotol Drawing 200061330. This requirement applies universally to all models of Fokker F27 Series aeroplanes operating within the Commonwealth of Australia. Failure to comply with the specified profile necessitates replacement of the latch before further flight, underscoring the critical nature of this directive for maintaining airworthiness. Compliance with this directive must be achieved unless the inspection was previously performed since 1 October 1977, and it must be conducted within 300 hours of time in service after 30 December 1977, ensuring timely adherence to safety standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, include a directive that governs the airworthiness of Fokker F27 series aeroplanes. This is outlined in AD/F27/93, which pertains to the nose gear down lock latch inspection (Section 2/78). The directive applies to all models of Fokker F27 series aeroplanes (Section 2/78). It requires that the nose landing gear down lock latch be inspected to ensure it conforms with the profile detailed in either Dowty Rotol SB 32-37 dated September 1962 or Dowty Rotol Drawing 200061330 (Section 2/78). If the latch does not conform to the specified profile, it must be replaced before any further flight can be undertaken (Section 2/78).
The obligations imposed by this directive include a stringent inspection requirement for the nose landing gear down lock latch. Operators of Fokker F27 series aeroplanes must ensure that the inspection is conducted according to the specified criteria and that any non-conforming latches are replaced as necessary. This inspection must be carried out unless it has already been completed since 1 October 1977, and it must occur within 300 hours of time in service after 30 December 1977 (Section 2/78). This ensures that the aircraft remains compliant with airworthiness standards and is safe for operation.
Failure to comply with the requirements set out in AD/F27/93 may result in severe consequences. The regulations stipulate that the non-compliance with airworthiness directives can lead to various civil and criminal penalties. Although the specific penalties are not detailed in the provided text, it is known that non-compliance with civil aviation safety directives can result in substantial fines, potential grounding of the aircraft, and even prosecution. Operators must adhere to these directives to avoid any legal repercussions and to maintain the safety and airworthiness of their aircraft.