AD/TB10/14 Amdt 1 - Front Seat Safety Belts

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

Legislation au F2006B07281 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes

 

AD/TB10/14

Amdt 1


Front Seat Safety Belts 3/95

 

Applicability: All Model TB9, TB10 and TB200 series aircraft.

 

Requirement: Action in accordance with SOCATA Mandatory Service Bulletin 10.044.25 Amendment 1.

 

Note: DGAC AD 89-097(A)R1 refers.

 

Compliance: Prior to 2 March 1996, and thereafter at intervals not to exceed 12 calendar months.

 

Background:  Seat belt anchorage fittings are hidden by aircraft trim and therefore are not readily inspectable for corrosion.

 

Amendment 1 is issued to align this Directive with a revision of the Country of Origin AD which reduces the inspection interval.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, amended by the Legislative Instrument F2006B07281, address the issue of ensuring the airworthiness of specific aircraft models through the issuance of Airworthiness Directives. This particular amendment, AD/TB10/14, pertains to the Aerospatiale (Socata) TB9 and TB10 (Tobago) series aeroplanes and mandates that front seat safety belt anchorage fittings be inspected in accordance with Socata Mandatory Service Bulletin 10.044.25 Amendment 1. The problem this directive seeks to resolve is the hidden nature of these fittings, which can lead to undetected corrosion. By aligning with the revised Country of Origin Airworthiness Directive, the Civil Aviation Safety Authority aims to ensure ongoing compliance and safety, with inspections occurring at intervals not exceeding 12 months, particularly focusing on periods prior to 2 March 1996. The amendment was enacted by the Commonwealth of Australia, with the objective of maintaining and enhancing aviation safety standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105 concerning the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, mandates that all Model TB9, TB10, and TB200 series aircraft must adhere to certain safety directives. This regulation applies to these specific aircraft models and requires compliance with SOCATA Mandatory Service Bulletin 10.044.25 Amendment 1. This directive addresses the issue of seat belt anchorage fittings, which are concealed by aircraft trim and thus not easily inspectable for corrosion. The regulation requires that these inspections be conducted prior to 2 March 1996 and subsequently at intervals not exceeding 12 calendar months. The purpose of this regulation is to ensure the safety of passengers and crew by maintaining the integrity of the seat belt anchorages, and it extends its reach to all operators and owners of the specified aircraft models within Australia, aligning with international safety standards referenced by the DGAC AD 89-097(A)R1. There are no exclusions or exemptions noted within this directive, and its application is strictly enforced to uphold the highest safety standards in civil aviation.

Key Provisions

The main sections of the Civil Aviation Regulations 1998 under Part 39 - 105, specifically focusing on the Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes, include the Airworthiness Directives (ADs) such as AD/TB10/14 Amendment 1, which pertains to front seat safety belt installations (Section 39-105). This directive applies to all Model TB9, TB10, and TB200 series aircraft and mandates that actions be taken in accordance with SOCATA Mandatory Service Bulletin 10.044.25 Amendment 1. The requirement is that these actions must be completed to ensure compliance with the directive, as referenced by DGAC AD 89-097(A)R1. The directive specifies that compliance must occur before 2 March 1996 and thereafter at intervals not exceeding 12 calendar months. The Civil Aviation Regulations impose several obligations on the parties or entities governed by the Act. Owners and operators of the affected aircraft must ensure that the front seat safety belts are inspected and maintained according to the specified schedule and procedures outlined in the SOCATA bulletin. This involves thorough inspections to check for corrosion in the seat belt anchorage fittings, which are concealed by the aircraft trim and thus not easily visible. The regulations mandate that any identified issues must be rectified promptly to maintain the airworthiness of the aircraft, ensuring safety for all passengers and crew on board. Failure to comply with the AD/TB10/14 Amendment 1 and the mandated inspections can lead to serious consequences. Non-compliance with these airworthiness directives can result in penalties under the Civil Aviation Act 1988. If found in breach, parties may face both civil and criminal penalties. Civil penalties can include fines, while criminal penalties may include imprisonment, reflecting the seriousness of ensuring aviation safety. The exact penalties depend on the severity and circumstances of the breach, but the regulations aim to ensure that all aircraft maintain the highest safety standards at all times.

Legal classification tags

Area of Law
Civil Aviation Law
Instrument
Regulation
Concepts
Regulatory Standards
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness Directives

Interactions

Authorises

All Versions

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.