AD/B727/112 Amdt 1 - Fuselage Forward Lower Body Skin

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Legislation au F2006B02635 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 727 Series Aeroplanes

 

AD/B727/112

Amdt 1


Fuselage Forward Lower Body Skin 7/90

 

Applicability: All Boeing 727-200.

 

Requirement: Action in accordance with Boeing Alert SB 727-53A0203 Rev 1.

 

Note: FAA AD 89-23-13 Amendment 39-6388 refers.

 

Compliance: Prior to 5 December 1989, unless previously accomplished within the last 6 months, and thereafter at intervals not exceeding 12 calendar months until preventive modification is carried out.

 

Background: Country of origin AD. Overseas aircraft found to have cracks 1200 mm long. Initial inspection has found cracks on one local aircraft. Amendment 1 references Revision 1 to the Requirement document. This requires repeat inspections until preventive modification is carried out, deletes specific line numbers and quotes FAA AD.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B02635, address the specific issue of ensuring the airworthiness of Boeing 727-200 aeroplanes by mandating compliance with certain safety directives. Enacted by the Commonwealth of Australia, these regulations are overseen by the Civil Aviation Safety Authority (CASA) and are designed to fill the gap in maintaining consistent and stringent safety standards across the aviation industry. The policy objective is to prevent potential safety hazards, such as fuselage cracks, by implementing regular inspections and required actions as specified in relevant Boeing Service Bulletins and Federal Aviation Administration directives. These regulations aim to ensure that all Boeing 727-200 aircraft meet the necessary safety requirements, thereby enhancing the overall safety of civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, as amended, under the jurisdiction of the Civil Aviation Safety Authority, include specific directives concerning the airworthiness of Boeing 727 Series Aeroplanes. Specifically, AD/B727/112 Amendment 1 pertains to the fuselage forward lower body skin of all Boeing 727-200 aircraft. The regulation mandates that these aircraft must comply with the requirements set out in Boeing Alert SB 727-53A0203 Revision 1. The directive applies to all Boeing 727-200 aircraft regardless of their location within Australia, thereby encompassing both domestic and potentially foreign-registered aircraft operating within Australian airspace. Compliance with this directive is mandatory for all affected aircraft, necessitating inspections and actions in line with the specified Boeing Service Bulletin prior to a certain date, with ongoing inspections at intervals not exceeding 12 months until a preventive modification is implemented. This directive is a direct reflection of an original country-specific airworthiness directive from the Federal Aviation Administration, which was prompted by the discovery of significant cracks in the fuselage of Boeing 727 aircraft, both domestically and internationally.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives for Boeing 727 Series Aeroplanes. Within this, AD/B727/112 Amendment 1 addresses the fuselage forward lower body skin (Section 7/90). This directive applies to all Boeing 727-200 aircraft and mandates action in accordance with Boeing Alert Service Bulletin (SB) 727-53A0203 Rev 1. It is noteworthy that this directive references FAA AD 89-23-13 Amendment 39-6388, which pertains to similar issues identified in overseas aircraft. The requirement is to conduct an inspection as per the specified Boeing Alert SB before 5 December 1989. If the inspection has already been completed within the last six months, it is not necessary to repeat the inspection before this date. However, once the specified date has passed, inspections must be conducted at intervals not exceeding 12 calendar months until a preventive modification is implemented. This ensures ongoing safety and compliance with the directive. Entities and parties governed by these regulations must ensure that inspections are conducted in accordance with the outlined Boeing Alert SB. They must maintain records of all inspections and any subsequent actions taken to address any findings, such as repairs or modifications. The regulations emphasise the importance of timely compliance to prevent potential safety hazards related to the fuselage forward lower body skin. Failure to comply with the AD/B727/112 Amendment 1 can result in significant legal and operational consequences. Non-compliance may lead to penalties under the Civil Aviation Act 1988, which includes fines and potential criminal charges. The maximum penalties can vary, but they are designed to enforce strict adherence to safety directives to protect the public and maintain the integrity of the aviation industry. It is essential for all operators to be aware of these requirements and ensure full compliance to avoid any adverse consequences.

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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.