COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 95 (Travelair) Series Aeroplanes
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/BEECH 95/26 and issues the following 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/BEECH 95/26
Amdt 1
Applicability: All models.
Wing Attach Fittings, Bolts and Nuts 12/2000
Requirement: 1. Remove and inspect the wing bolts, washers and nuts in accordance with Beechcraft Shop Manual 95-590001-1C6 as revised August 31 1995, Section 4.
2. Retire wing bolts, washers and nuts from service and replace with new hardware in accordance with Beechcraft Shop Manual 9 95-590001-1C6 Section 4. Render unserviceable all hardware retired.
Compliance: 1. Unless inspection has already been accomplished in accordance with the Requirement Document, initially inspect before 5 calendar years from initial installation. Re-inspect at intervals not to exceed 5 calendar years.
2. Retire before 15 calendar years after initial installation. This Amendment becomes effective on 30 November 2000.
Background: The initial issue of this Airworthiness Directive became effective on 31 March 1985 and made mandatory the inspection and replacement periods for the wing attachment hardware as detailed in the Travel Air Shop Manual.
This Amendment updates the revision status of the Travel Air Shop Manual.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 17 October 2000
The above AD is notified in the Commonwealth of Australia Gazette on 1 November 2000.
Overview
The Civil Aviation Regulations 1998, particularly Part 39 - 105, addresses safety concerns in civil aviation through the issuance of Airworthiness Directives by the Civil Aviation Safety Authority (CASA). One such directive, AD/BEECH 95/26, targets the Beechcraft 95 (Travelair) Series Aeroplanes, aiming to ensure the safe operation of these aircraft by mandating regular inspections and replacements of critical wing attachment components. This directive was enacted to address potential safety hazards associated with the wing attach fittings, bolts and nuts of these aeroplanes. CASA, acting under the authority granted by the Civil Aviation Act 1988, issued this directive to mitigate risks and ensure compliance with safety standards, thus safeguarding the public and maintaining the integrity of the civil aviation system.
Scope and Application
The Airworthiness Directive (AD) AD/BEECH 95/26 applies to all models of the Beechcraft 95 (Travelair) series aeroplanes. The directive is issued by the Civil Aviation Safety Authority (CASA) and mandates specific actions to address identified safety concerns regarding the wing attach fittings, bolts, and nuts. This regulatory requirement encompasses the inspection and replacement of the aforementioned hardware to ensure compliance with safety standards. The directive applies to all instances where the specified aircraft models are operated within the Commonwealth of Australia and mandates adherence to the CASA’s prescribed timelines and procedures. The directive is effective from 30 November 2000, as detailed in the legislative instrument. Exemptions or exclusions are not explicitly stated within the text, implying that all specified aircraft must comply with the AD requirements. The directive's scope and application are further clarified through subordinate instruments, ensuring that all relevant parties are informed and compliant with the safety regulations.
Key Provisions
The main sections of this Airworthiness Directive (AD) concern the applicability, requirements, and compliance timelines for Beechcraft 95 (Travelair) series aeroplanes, specifically regarding the wing attach fittings, bolts, and nuts. The applicability section (AD/BEECH 95/26) states that this directive applies to all models of the Beechcraft 95 series. The requirement section stipulates that the wing bolts, washers, and nuts must be removed, inspected, retired from service, and replaced with new hardware as per the Beechcraft Shop Manual 95-590001-1C6 Section 4, with the hardware that is retired rendered unserviceable. The compliance section mandates that the initial inspection must be completed within five calendar years from the initial installation of the aircraft, with subsequent inspections to occur at intervals not exceeding five calendar years. The retired hardware must be replaced before 15 calendar years after the initial installation.
The AD imposes several obligations on the parties and entities it governs. Primarily, aircraft operators and maintenance personnel must ensure that the specified inspections and replacements of wing attach fittings, bolts, and nuts are conducted in accordance with the detailed instructions provided in the Beechcraft Shop Manual. The directive mandates rigorous inspection protocols to be adhered to within the specified timeframes to ensure ongoing airworthiness and safety of the aircraft. Additionally, any retired hardware must be properly disposed of or rendered unserviceable to prevent its reuse.
Failure to comply with the AD may result in various consequences, both civil and criminal. Civil Aviation Safety Authority (CASA) may take enforcement actions against non-compliant aircraft operators or maintenance entities. The severity of the penalties can range from fines to more severe sanctions such as suspension or revocation of the operator’s licence. The exact penalties are not specified in the AD itself but would be determined under the broader Civil Aviation Regulations 1998. Non-compliance with airworthiness directives is a serious matter, as it directly impacts the safety of the aircraft and those on board. Therefore, adherence to these regulations is critical to maintaining safe aviation practices.