AD 2010-16-01 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135ER, -135KE, -135KL, and -135LR Airplanes, and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes

Models named: EMB-135ER, -135KE, -135KL, -135LR, EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135ER, -135KE, -135KL, and -135LR airplanes, and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes; certificated in any category; except for Model EMB-145LR airplanes modified according to Brazilian Supplemental Type Certificate 2002S06-09, 2002S06-10, or 2003S08-01. Note 1: This AD requires revisions to certain operator maintenance documents to include new inspections. Compliance with these inspections is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (h) of this AD. The request should include a description of changes to the required inspections that will ensure the continued operational safety of the airplane.

Unless already done, do the following actions. (1) Before December 16, 2008, revise the ALS of the ICA to incorporate Section A2.5.2, Fuel System Limitation Items, of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007, except as provided by paragraph (g) of this AD. Except as required by paragraph (g) of this AD, for all tasks identified in Section A2.5.2 of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007, the initial compliance times start from the applicable times specified in Table 1 of this AD; and the repetitive inspections must be accomplished thereafter at the interval specified in Section A2.5.2 of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007, except as provided by paragraphs (f)(3) and (h) of this AD. Table 1—Initial Inspections Reference No. Description Compliance time (whichever occurs later) Threshold Grace period 28-11-00-720-001-A00 Functionally Check critical bonding integrity of selected conduits inside the wing tank, Fuel Pump and FQIS connectors at tank wall by conductivity measurements Before the accumulation of 30,000 total flight hours Within 90 days after December 16, 2008. 28-17-01-720-001-A00 Functionally Check critical bonding integrity of Fuel Pump, VFQIS and Low Level SW connectors at tank wall by conductivity measurements Before the accumulation of 30,000 total flight hours Within 90 days after December 16, 2008. 28-21-01-220-001-A00 Inspect Electric Fuel Pump Connector Before the accumulation of 10,000 total flight hours Within 90 days after December 16, 2008. 28-23-03-220-001-A00 Inspect Pilot Valve harness inside the conduit Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. 28-23-04-220-001-A00 Inspect Vent Valve harness inside the conduit Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. 28-27-01-220-001-A00 Inspect Electric Fuel Transfer Pump Connector Before the accumulation of 10,000 total flight hours Within 90 days after December 16, 2008. 28-41-03-220-001-A00 Inspect FQIS harness for clamp and wire jacket integrity Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. 28-41-07-220-001-A00 Inspect VFQIS and Low Level SW Harness for clamp and wire jacket integrity Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. (2) Within 90 days after July 30, 2008 (the effective date of AD 2008-13-14), revise the ALS of the ICA to incorporate items 1, 2, and 3 of Section A2.4, Critical Design Configuration Control Limitation (CDCCL), of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007. (3) After accomplishing the actions specified in paragraphs (f)(1) and (f)(2) of this AD, no alternative inspections, inspection intervals, or CDCCLs may be used unless the inspections, intervals, or CDCCLs are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (h) of this AD. New Requirements of This AD

Unless already done, do the following actions. (1) Before December 16, 2008, revise the ALS of the ICA to incorporate Section A2.5.2, Fuel System Limitation Items, of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007, except as provided by paragraph (g) of this AD. Except as required by paragraph (g) of this AD, for all tasks identified in Section A2.5.2 of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007, the initial compliance times start from the applicable times specified in Table 1 of this AD; and the repetitive inspections must be accomplished thereafter at the interval specified in Section A2.5.2 of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007, except as provided by paragraphs (f)(3) and (h) of this AD. Table 1—Initial Inspections Reference No. Description Compliance time (whichever occurs later) Threshold Grace period 28-11-00-720-001-A00 Functionally Check critical bonding integrity of selected conduits inside the wing tank, Fuel Pump and FQIS connectors at tank wall by conductivity measurements Before the accumulation of 30,000 total flight hours Within 90 days after December 16, 2008. 28-17-01-720-001-A00 Functionally Check critical bonding integrity of Fuel Pump, VFQIS and Low Level SW connectors at tank wall by conductivity measurements Before the accumulation of 30,000 total flight hours Within 90 days after December 16, 2008. 28-21-01-220-001-A00 Inspect Electric Fuel Pump Connector Before the accumulation of 10,000 total flight hours Within 90 days after December 16, 2008. 28-23-03-220-001-A00 Inspect Pilot Valve harness inside the conduit Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. 28-23-04-220-001-A00 Inspect Vent Valve harness inside the conduit Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. 28-27-01-220-001-A00 Inspect Electric Fuel Transfer Pump Connector Before the accumulation of 10,000 total flight hours Within 90 days after December 16, 2008. 28-41-03-220-001-A00 Inspect FQIS harness for clamp and wire jacket integrity Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. 28-41-07-220-001-A00 Inspect VFQIS and Low Level SW Harness for clamp and wire jacket integrity Before the accumulation of 20,000 total flight hours Within 90 days after December 16, 2008. (2) Within 90 days after July 30, 2008 (the effective date of AD 2008-13-14), revise the ALS of the ICA to incorporate items 1, 2, and 3 of Section A2.4, Critical Design Configuration Control Limitation (CDCCL), of Appendix 2 of EMBRAER EMB135/ERJ140/EMB145 Maintenance Review Board Report MRB-145/1150, Revision 11, dated September 19, 2007. (3) After accomplishing the actions specified in paragraphs (f)(1) and (f)(2) of this AD, no alternative inspections, inspection intervals, or CDCCLs may be used unless the inspections, intervals, or CDCCLs are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (h) of this AD. New Requirements of This AD