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