Commonwealth legislation

AD/TB 200/1 - Fuel System - Flowmeter Pipe Integrity

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This Directive requires owners/operators of Socata TB 200 aeroplanes not fitted with SOCATA Modification No.150 to check the fuel flowmeter pipe for tightness and to replace the pipe with the Mod 150 part per SOCATA Service Bulletin No. 10-108-73 Rev 1. The initial check must occur within 10 flight hours and thereafter at every scheduled inspection; replacement is required within 150 hours or by 9 December 1999. It implements the country-of-origin airworthiness authority’s integrity requirement.

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AD/TB 200/1 - Fuel System - Flowmeter Pipe Integrity

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Aerospatiale (Socata) TB 200 Series Aeroplanes

AD/TB 200/1 Fuel System - Flowmeter Pipe Integrity 9/99

Applicability: All Socata TB 200 aircraft not equipped with SOCATA Modification No. 150 (Fuel Flowmeter Pipe).

Requirement: 1. Check the tightness of the fuel flowmeter pipe in accordance with SOCATA SB No. 10-108-73 Rev 1, dated March 1999.

Replace the fuel flowmeter pipe (SOCATA Mod 150) according to SOCATA SB No. 10-108-73 Rev 1, dated March 1999.

Note: DGAC 1999-061(A)R1 dated 05 May 1999 refers.

Compliance: 1. Within the next 10 flight hours after the effective date of this Directive and thereafter at every scheduled aircraft inspection.

Within 150 hours after the effective date of this directive, or 9 December 1999, whichever occurs first.

This Airworthiness Directive becomes effective on 9 September 1999.

Background: The measures outlined in this Directive are deemed necessary to ensure the integrity of the fuel flowmeter pipe and reflect the Country of Origin Airworthiness Authority’s requirements.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

1 AD/TB 200/1 - Fuel System - Flowmeter Pipe Integrity