COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Casa 212 Series Aeroplanes
AD/CASA/16 Rudder Control 3/94 DM
Applicability: All Model C-212 aircraft.
Requirement: 1. Action in accordance with CASA Communication COM 212-245.
2. Action in accordance with CASA Service Bulletin 212-27-47.
Note: Spanish DGCA AD 01/93 refers.
Compliance: 1. Prior to each flight, until CASA Service Bulletin 212-27-47 is accomplished.
2. Prior to 31 May 1994.
Background: The Spanish DGCA requires an interim limitation on rudder pedal adjustment and then modification action in order to achieve the appropriate values of rudder surface deflection for required flying handling qualities, regardless of the selected rudder pedal assembly adjustment.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA), were enacted to ensure the safety and efficiency of civil aviation in Australia. Part 39, specifically Airworthiness Directives, contains provisions that aim to address safety issues in specific aircraft types, such as the CASA 212 series aeroplanes. One such directive, AD/CASA/16, addresses the rudder control mechanism for all Model C-212 aircraft. The directive was introduced to rectify a safety concern regarding the rudder surface deflection values and flying handling qualities. The directive mandates compliance with CASA Communication COM 212-245 and CASA Service Bulletin 212-27-47, with an interim limitation on rudder pedal adjustment and subsequent modification action as outlined by the Spanish Directorate General of Civil Aviation (DGCA). The overarching policy objective is to ensure that all flights meet the required safety standards before operation.
This legislative instrument ensures that all Model C-212 aircraft are compliant with specific safety requirements before each flight and by a specified date, in this case, prior to 31 May 1994. The directive references Spanish DGCA AD 01/93 to ensure international safety standards are met. By implementing these measures, the Civil Aviation Regulations 1998 aim to maintain high safety standards in civil aviation, thereby protecting passengers, crew, and the public.
Scope and Application
The Civil Aviation Safety Authority (CASA) regulations, specifically PART 39 - 105 of the Civil Aviation Regulations 1998, apply to all Model C-212 aircraft. These regulations mandate compliance with certain airworthiness directives to ensure safety and proper handling of the aircraft. The directive requires action in accordance with CASA Communication COM 212-245 and CASA Service Bulletin 212-27-47, and references a corresponding Spanish DGCA AD 01/93. Compliance must be achieved prior to each flight until the measures outlined in CASA Service Bulletin 212-27-47 are completed, and all actions must be finalised before 31 May 1994. This regulation is part of a broader set of rules designed to maintain the airworthiness of these aircraft, ensuring that they meet safety standards set by CASA and international counterparts like the Spanish DGCA.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, specify an Airworthiness Directive (AD) for Casa 212 Series Aeroplanes, specifically focusing on rudder control (AD/CASA/16). The directive is applicable to all Model C-212 aircraft (Section 1). The main requirements, as outlined in the AD, necessitate adherence to CASA Communication COM 212-245 and CASA Service Bulletin 212-27-47 (Section 1). The directive notes a reference to Spanish DGCA AD 01/93, indicating alignment with international safety standards (Section 1). Compliance with these requirements must be ensured prior to each flight until the CASA Service Bulletin 212-27-47 is accomplished, and also before 31 May 1994 (Section 1).
Operators of Casa 212 Series Aeroplanes are obligated to follow the specific actions detailed in CASA Communication COM 212-245 and CASA Service Bulletin 212-27-47. This includes implementing interim limitations on rudder pedal adjustment and subsequent modifications to achieve the required rudder surface deflection values for satisfactory flight handling qualities (Section 1). The operators must ensure that these actions are undertaken in compliance with the specified timelines to maintain airworthiness standards (Section 1). The directive is clear in its requirement for pre-flight checks to confirm that all mandated procedures are completed (Section 1).
Failure to comply with the Airworthiness Directive may result in serious consequences. Although specific offences and penalties are not detailed in the extract, non-compliance with ADs can typically lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Potential outcomes may include grounding of the aircraft, fines, or other regulatory penalties. The exact penalties are governed by broader civil aviation regulations and can vary based on the severity and frequency of the breach (Section 1). It is essential for operators to adhere strictly to the directive to avoid any legal repercussions.