AD/R22/16 Amdt 4 - Lower Actuator Bearing

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06421 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Robinson R22 Series Helicopters

 

AD/R22/16

Amdt 4


Lower Actuator Bearing 13/94

 

Applicability: All series R22 helicopters.

 

Requirement: Inspect lower bearing assembly P/N A007-3 for fitment of roller bearing assembly P/N A181-4. If the bearing P/N is unknown or if roller bearing assembly P/N A181-4 has not been fitted, action in accordance with Robinson SB 63.

 

Compliance: Unless previously carried out, within 25 hours time in service from 8 December 1994 or by 31 January 1995, whichever occurs first. Thereafter, reinspect at each maintenance release issue.

 

Background: Due to the low in-service life of the fan shaft ball bearing the manufacturer has previously introduced a replacement roller bearing. Failure of a fan shaft bearing can resulted in total loss of engine power to the main rotor. This amendment mandates fitment of the roller bearing and a repetitive check to confirm the roller bearing installation after failure of a commercial ball bearing caused a helicopter accident.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended, were enacted to regulate civil aviation safety and ensure the safety of aircraft operations within Australia. One specific legislative instrument, F2006B06421, pertains to the Robinson R22 Series Helicopters and was introduced to address the problem of low in-service life of the fan shaft ball bearing in these helicopters, which could potentially lead to the total loss of engine power to the main rotor. This safety concern was highlighted following a helicopter accident caused by the failure of a commercial ball bearing. The objective of this particular Airworthiness Directive (AD/R22/16 Amendment 4) is to mandate the inspection and replacement of the lower bearing assembly, ensuring the fitment of the specified roller bearing assembly to prevent future incidents. The compliance requirement stipulates that the action must be taken within a specified timeframe, either 25 hours of service from 8 December 1994 or by 31 January 1995, with further reinspections at each maintenance release issue thereafter. This directive is enacted by the Civil Aviation Safety Authority under the authority of the Civil Aviation Act 1988.

Scope and Application

The Civil Aviation Regulations 1998, as amended, specifically under PART 39 - 105, mandates strict adherence to the Airworthiness Directives concerning the Robinson R22 Series Helicopters. This directive applies universally to all R22 helicopters operating within the Australian jurisdiction, overseen by the Civil Aviation Safety Authority. The regulation requires mandatory inspection of the lower bearing assembly P/N A007-3 to ensure the fitment of the specified roller bearing assembly P/N A181-4. Non-compliance with this directive can lead to severe consequences, including total loss of engine power to the main rotor, as evidenced by previous incidents where the failure of a commercial ball bearing led to accidents. The directive stipulates that the inspection must be conducted within 25 hours from 8 December 1994 or by 31 January 1995, whichever is later, and subsequent inspections must occur at each maintenance release issue. This regulation leaves no room for deviation and ensures that all Robinson R22 helicopters are maintained to the highest safety standards. The scope of the Civil Aviation Regulations 1998 extends to the national level, ensuring uniform safety standards across all states and territories of Australia. The regulations are meticulously crafted to cover all aspects of helicopter operation, maintenance, and safety, with specific directives such as AD/R22/16 underscoring the importance of detailed checks and compliance with manufacturer specifications. While the regulations apply broadly, they do not specify any exclusions or exemptions, thereby enforcing a stringent safety regime for all Robinson R22 helicopters within Australia. The Civil Aviation Safety Authority retains the power to extend or restrict the application of these directives through subordinate instruments, ensuring that the regulations can adapt to evolving safety concerns and technological advancements.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, include specific Airworthiness Directives (AD) that are critical for maintaining the safety of aircraft in Australia. One such directive, AD/R22/16 Amendment 4, pertains to the Robinson R22 Series Helicopters, specifically focusing on the lower actuator bearing. According to section 13/94 of the directive, all series R22 helicopters are required to inspect the lower bearing assembly P/N A007-3 to ensure it is fitted with the roller bearing assembly P/N A181-4. If the bearing part number is unknown or if the roller bearing assembly P/N A181-4 has not been fitted, the directive refers to Robinson Service Bulletin 63 for the necessary actions. This inspection must be carried out within 25 hours of time in service from 8 December 1994 or by 31 January 1995, whichever occurs first. After this initial compliance, the bearing must be reinspected at each maintenance release issue. Operators and owners of Robinson R22 Series Helicopters are mandated to adhere to these inspection requirements as outlined in the Civil Aviation Regulations. They must ensure that the specified inspection and replacement of the bearing assembly are completed within the stipulated timeframes. Failure to comply with these requirements can lead to significant safety risks, as the low in-service life of the fan shaft ball bearing has previously resulted in total loss of engine power to the main rotor, potentially leading to accidents. These obligations are not merely procedural but are critical to the ongoing airworthiness and safety of the aircraft. Failure to comply with the provisions of AD/R22/16 Amendment 4 can have serious consequences. The Civil Aviation Regulations 1998 impose stringent penalties for non-compliance. The consequences of not adhering to these directives can include severe penalties under the Civil Aviation Act 1988. Specifically, non-compliance with an Airworthiness Directive can result in fines and potential criminal charges. The maximum penalty for operating an aircraft that does not comply with an applicable AD can be substantial, reflecting the high importance placed on ensuring aircraft safety through these regulatory measures. Therefore, it is imperative for operators and owners to ensure strict adherence to these directives to avoid legal repercussions and to maintain the highest standards of aviation safety.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.