Document ID: chunk:federal_register_of_legislation:F2006B07268:body:0
Version: federal_register_of_legislation:F2006B07268
Segment Type: other
Provision Reference: 
Character Range: 0–1289

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

 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.

             2. 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.

             2. 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.