COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Robinson R22 Series Helicopters
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
AD/R22/49 Main Rotor Drive Shaft Yoke Half Assembly 12/2000
TX
Applicability: Model R22 helicopters, with a yoke half assembly part number A203-5 installed. Requirement: 1. Inspect each yoke for evidence of cracking, refer to Figure A.
If a yoke is cracked, before further flight, replace the yokes with serviceable yokes, part number A203-7. Both yokes must be replaced with yokes part number A203- 7.
2. Determine the Lot identifier of each yoke, P/N A203-5.
If the Lot identifier is from 24 through 43, if it is in letter code, or if it is illegible, replace yokes part number A203-5, with serviceable yokes part number A203-7. Yoke part number A203-7 cannot be installed with yoke part number A203-5.
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Note: Emergency FAA AD 2000-20-51 and Robinson R22 Service Bulletin SB-88A refer.
Determining that the installed yokes, part number A203-5, are not in the lots affected by this Directive, or replacing yokes, part number A203-5 with yokes part number A203-7, is terminating action for the requirements of this Directive.
Compliance: 1. Before further flight after 9 October 2000, and thereafter before the first flight of each day.
2. Before further flight after 1 January 2001.
This Directive shall be entered on the Maintenance Release as maintenance required. The Requirement 1 visual inspection may be performed and certified by the Pilot in Command. In which case, a copy of this Directive is to be carried in the aircraft.
This Airworthiness Directive becomes effective on 9 October 2000.
Background: The FAA received several reports of cracks in the yoke half assembly during pre- flight inspections. The cracked yokes were still in service and functioned for an unknown duration. This condition, if not corrected, could result in separation of the yokes from the main rotor drive shaft and subsequent loss of control of the helicopter.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 6 October 2000
The above AD is notified in the Commonwealth of Australia Gazette on 9 October 2000.
Overview
The Civil Aviation Regulations 1998 (CAR 1998) were enacted to ensure the safety and efficiency of civil aviation in Australia, providing a comprehensive framework for the regulation of aircraft and aviation activities. One specific legislative instrument under CAR 1998 is the Airworthiness Directive issued by the Civil Aviation Safety Authority (CASA) to address safety concerns identified in certain aircraft. For instance, AD/R22/49 pertains to Robinson R22 Series Helicopters and mandates inspections and replacements of specific yoke components to mitigate the risk of cracks leading to potential loss of control. The policy objective behind such directives is to proactively address safety hazards and maintain the highest standards of aviation safety. This legislative instrument was introduced to fill the gap in ensuring that specific aviation products meet safety requirements, thereby protecting both the public and aviation personnel.
Scope and Application
The Airworthiness Directive (AD) R22/49 issued by the Civil Aviation Safety Authority (CASA) applies to Robinson R22 Series helicopters that have a yoke half assembly part number A203-5 installed. The AD requires specific actions to be taken to address the risk of cracking in the yoke half assembly, which could lead to the separation of the yokes from the main rotor drive shaft and loss of control of the helicopter. The directive applies nationally across the Commonwealth of Australia and mandates that inspections and necessary replacements of the yokes must be performed before further flight, with specific compliance dates outlined. The directive is applicable to all persons or entities operating these helicopters within Australia, including private and commercial operators. Any deviation from the AD's requirements could result in non-compliance with civil aviation safety standards, potentially leading to enforcement actions by CASA. The AD can be extended or modified through subordinate instruments, ensuring that safety standards are continuously updated in response to new information or developments in the aviation industry.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish an Airworthiness Directive (AD) concerning the Robinson R22 series helicopters. This AD mandates specific actions to address the identified safety concerns with the yoke half assembly of these helicopters. Section 12/2000TX of the AD applies to model R22 helicopters equipped with a yoke half assembly part number A203-5. The requirement section outlines the necessary steps to ensure airworthiness: first, each yoke must be inspected for any evidence of cracking, and if cracks are found, both yokes must be replaced with serviceable yokes part number A203-7. Second, the Lot identifier of each yoke, P/N A203-5, must be determined; if the Lot identifier is within the range of 24 through 43, or if it is illegible, the yokes must also be replaced with part number A203-7. These replacements are mandatory to prevent potential separation from the main rotor drive shaft, which could lead to loss of control.
The obligations imposed by this AD are clear and precise. Operators of model R22 helicopters must ensure that the specified inspections and replacements are carried out. Specifically, the inspections must be performed before further flight after 9 October 2000, and before the first flight of each day thereafter. Following 1 January 2001, these inspections and replacements must occur before any further flight. Moreover, the compliance section mandates that this directive be recorded on the Maintenance Release as maintenance required. If the visual inspection is performed and certified by the Pilot in Command, a copy of this AD must be carried in the aircraft.
Failure to comply with the requirements of this Airworthiness Directive can lead to significant consequences. Under the Civil Aviation Regulations 1998, violations may result in civil or criminal penalties. Although the specific penalties are not detailed in the AD, it is understood that non-compliance with airworthiness directives can lead to hefty fines and potential prosecution under civil aviation laws. Furthermore, operating a helicopter with unaddressed safety issues could result in severe operational disruptions, endangering lives and property, and potentially leading to catastrophic outcomes. The AD becomes effective immediately upon its publication, underscoring the urgency and importance of adhering to its stipulations.