AD/EMB-145/9 - Ventral Fuel Tank Refuelling Line (Cth)

Federal Register of Legislation

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AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Embraer EMB-135 and EMB-145 Series Aeroplanes AD/EMB-145/9 Ventral Fuel Tank Refuelling Line 8/2008

Applicability: 145590 145643 145645 145646 145649 145650 145654 145655 145662 145664 145666 145672 145674 145675 Requirement: Compliance: EMB-145XR model aircraft with serial numbers listed in Table 1. Table 1 145677 145727 145782 145681 145731 thru 145733 145786 145683 145735 145787 145684 145739 145791 145688 thru 145690 145741 145792 145693 145745 145799 145697 145746 14500805 145700 145749 14500808 145657 thru 145660 145703 thru 145705 145751 14500811 145708 145753 14500817 145712 145756 14500819 145714 145758 14500831 145718 145759 14500834 145719 145761 145721 145772 Unless previously accomplished, install a bonding jumper between the pilot valve line tube and the pressure refuelling system tube, after removing ventral fuel tank access panel 196FR, as described in the Embraer Service Bulletin 145-28-0026, original issue, or further revisions approved by the Brazilian Agência Nacional de Aviação Civil (ANAC). Note: ANAC AD 2006-12-01 refers. Within the next 10,000 hours time in service (TIS) for aircraft with less than 5,000 hours TIS, or within the next 5,000 hours TIS for aircraft with more than 5,000 hours, TIS after 4 January 2007 (the effective date ANAC AD 2006-12-01). This Airworthiness Directive becomes effective on 31 July 2008.

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Embraer EMB-135 and EMB-145 Series Aeroplanes AD/EMB-145/9 Ventral Fuel Tank Refuelling Line 8/2008

Applicability: EMB-145XR model aircraft with serial numbers listed in Table 1. Table 1 145590 145677 145727 145782 145643 145681 145731 thru 145733 145786 145645 145683 145735 145787 145646 145684 145739 145791 145649 145688 thru 145690 145741 145792 145650 145693 145745 145799 145654 145697 145746 14500805 145655 145700 145749 14500808 145657 thru 145660 145703 thru 145705 145751 14500811 145662 145708 145753 14500817 145664 145712 145756 14500819 145666 145714 145758 14500831 145672 145718 145759 14500834 145674 145719 145761 145675 145721 145772 Requirement: Unless previously accomplished, install a bonding jumper between the pilot valve line tube and the pressure refuelling system tube, after removing ventral fuel tank access panel 196FR, as described in the Embraer Service Bulletin 145-28-0026, original issue, or further revisions approved by the Brazilian Agência Nacional de Aviação Civil (ANAC). Note: ANAC AD 2006-12-01 refers. Compliance: Within the next 10,000 hours time in service (TIS) for aircraft with less than 5,000 hours TIS, or within the next 5,000 hours TIS for aircraft with more than 5,000 hours, TIS after 4 January 2007 (the effective date ANAC AD 2006-12-01). This Airworthiness Directive becomes effective on 31 July 2008.

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