Document ID: chunk:federal_register_of_legislation:F2009L03433:body:0:p2
Version: federal_register_of_legislation:F2009L03433
Segment Type: other
Provision Reference: 
Character Range: 4213–7385

aeroplanes - M7 Aerospace SA227 Series SB 227-24-002, revised 21 November 2008; or Fairchild Aircraft Corporation SA227 Series SB 24-002, revised 15 February 1984.
      3. For model SA226-AT, SA226-T, SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-CC, and SA227-DC (C-26B) aeroplanes, all S/N, inspect electrical wires and components, hydraulic tube assemblies, and bleed air tube assemblies at the left hand and right hand (LH/RH) inboard wing leading edge/battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed-through locations into the LH/RH inboard keelson for any evidence of chafing or arcing.
      The above Requirement is to be accomplished using service information as follows:
        For Models SA226-AT, SA226-T, and SA226-TC aeroplanes - M7 Aerospace SA226 Series SB 226-24-036, revised 21 November 2008; or M7 Aerospace SA226 Series SB 226-24-036, issued 19 September 2007;

        For Models SA227-AC (C-26A) and SA227-AT, aeroplanes - M7 Aerospace SA227 Series SB 227-24-019, revised 21 November 2008; or M7 Aerospace SA227 Series SB 227-24-019, issued 19 September 2007; or

        For Models SA227-CC and SA227-DC (C-26B) aeroplanes - SA227 Series Commuter Category SB CC7-24-010, revised 21 November 2008; or SA227 Series Commuter Category SB CC7-24-010, issued 19 September 2007.

                4. For model SA227-BC (C-26A) aeroplanes, all S/N, inspect the main battery leads running forward from the battery compartment for any evidence of insulation deterioration following M7 Aerospace SA227 Series SB 227-24-001, revised
                21 November 2008.
                5. For model SA227-BC (C-26A) aeroplanes, all S/N, inspect electrical wires and components, hydraulic tube assemblies, and bleed air tube assemblies at LH/RH inboard wing leading edge/battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed-through locations into the LH/RH inboard keelson for any evidence of insulation deterioration, chafing, or arcing following M7 Aerospace SA227 Series SB 227-24-019, revised 21 November 2008.
                6. For all model and S/N aeroplanes, clear, repair, and/or replace all electrical wires and components, hydraulic tube assemblies, and bleed air tube assemblies, in the inspection area and feed-through locations that show any sign of insulation deterioration, chafing, or arcing, as required following the applicable service information referenced in Requirements 1, 3, 4 and 5.
             Note 1:  Although not a requirement of this Directive, Swearingen Aviation Corporation SA226 Series SB 57-010, revised 15 December 1975, may be incorporated on those aeroplanes that have not installed the access panel.  Installation of the access panel will simplify the incorporation of the service bulletins referenced in this Directive and future inspections of the areas of concern.
             Note 2:  This Directive supersedes AD/SWSA226/96 Amdt 1 which will be cancelled.  Any inspection accomplished in accordance with AD/SWSA226/96 or Amdt 1 that is equivalent to any inspection required by this Directive is acceptable for compliance with this Directive and the 12 month interval for