COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bell UH-1 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/UH-1/7 Tail Rotor Grip 7/2000
Applicability: Models UH1B, UH1E, UH1F, UH1L and TH1L with tail rotor grip P/N 204-011-728-1, -13, or -19 installed.
Requirement: Remove from service any of the applicable tail rotor grips:
- with more than 300 hours time in service, or
b. where total time in service cannot be established, and substantiated.
Note: FAA AD 88-25-05 refers.
Compliance: Before further flight after the effective date of this directive.
This Airworthiness Directive becomes effective on 13 July 2000.
Background: This directive is raised to prevent failure of the tail rotor grip assembly.
William Ronald Smith
Delegate of the Civil Aviation Safety Authority 25 May 2000
The above AD is notified in the Commonwealth of Australia Gazette on 14 June 2000.
Overview
The Civil Aviation Regulations 1998 (CAR 1998), specifically under PART 39 - 105, addresses safety concerns in the aviation sector by issuing Airworthiness Directives (ADs) to ensure the safe operation of aircraft. One such directive, AD/UH-1/7, was enacted in 2000 to address a specific safety issue concerning the tail rotor grip assemblies in Bell UH-1 Series Helicopters. This Airworthiness Directive was issued by the Civil Aviation Safety Authority (CASA) to prevent failures of the tail rotor grip assembly which could potentially compromise the safety of flight operations. The directive mandates that any tail rotor grips with more than 300 hours of service time, or those where the total service time cannot be established and substantiated, be removed from service before further flight. The directive became effective on 13 July 2000, with its notification appearing in the Commonwealth of Australia Gazette on 14 June 2000. The policy objective of this AD is to enhance the safety of civil aviation by ensuring that all aircraft meet the necessary safety standards and conditions.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the Civil Aviation Safety Authority (CASA) to issue Airworthiness Directives (ADs) aimed at ensuring the safe operation of aircraft within the Australian jurisdiction. This particular AD/UH-1/7 pertains to Bell UH-1 Series helicopters, specifically models UH1B, UH1E, UH1F, UH1L, and TH1L, which have tail rotor grips with part numbers 204-011-728-1, -13, or -19 installed. The directive applies to any of these helicopters that have tail rotor grips exceeding 300 hours of time in service or where the total time in service cannot be established but is substantiated. The requirement is to remove the affected tail rotor grips from service before further flight following the directive's effective date of 13 July 2000. The AD was issued by a CASA delegate, William Ronald Smith, on 25 May 2000, and was officially notified in the Commonwealth of Australia Gazette on 14 June 2000. This directive is intended to mitigate the risk of tail rotor grip assembly failure, ensuring continued airworthiness and safety standards are upheld for the specified helicopter models.
Key Provisions
The main sections of this Airworthiness Directive (AD) under the Civil Aviation Regulations 1998 (CAR 1998) concern the applicability, requirement, and compliance for specific models of Bell UH-1 Series Helicopters. The applicability section (AD/UH-1/7) identifies the models affected, namely UH1B, UH1E, UH1F, UH1L, and TH1L, when equipped with a particular tail rotor grip (P/N 204-011-728-1, -13, or -19). The requirement section mandates that any tail rotor grip with more than 300 hours of service time, or those where total service time cannot be established and substantiated, must be removed from service. The compliance section stipulates that this action must be taken before any further flight after the effective date of the directive, which is 13 July 2000.
The Airworthiness Directive imposes specific obligations on the operators and owners of the affected helicopters. They must ensure that the identified tail rotor grips are examined for their service time. If a grip has exceeded 300 hours of service or if the total service time cannot be established and substantiated, it must be removed from service. This is to prevent potential failure of the tail rotor grip assembly, ensuring the continued airworthiness and safety of the aircraft.
The directive also outlines the consequences for non-compliance. While the specific penalties are not detailed within the AD, under CAR 1998, non-compliance with an Airworthiness Directive can result in significant civil and criminal penalties. Civil penalties may include fines up to a specified maximum amount, while criminal penalties may include imprisonment. These consequences underscore the importance of adhering to the AD to ensure the safety and compliance of the affected aircraft within the Australian aviation sector. The directive becomes effective on 13 July 2000, and its notification in the Commonwealth of Australia Gazette on 14 June 2000 ensures that all relevant parties are informed of their obligations.