Fairchild (Swearingen) SA226 and SA227 SFairchild (Swearingen) SA226 and SA227 Series Aeroplanes

Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

<table cellspacing="0" cellpadding="0" style="width:510.3pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr style="height:5.1pt"><td rowspan="5" style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Applicability:</span></p></td><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Models</span></p></td><td style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Serial Numbers</span></p></td></tr><tr style="height:5.1pt"><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>SA226-AT</span></p></td><td style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>AT001 through AT074</span></p></td></tr><tr style="height:5.1pt"><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>SA226-TC</span></p></td><td style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>TC201 through TC419</span></p></td></tr><tr style="height:5.1pt"><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>SA227-AC</span></p></td><td style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>AC406, AC415, AC416, AC420 through AC456, AC458 through AC469, and AC471 through AC478</span></p></td></tr><tr style="height:5.1pt"><td style="width:101pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>SA227-AT</span></p></td><td style="width:302.85pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>AT423 through AT469</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Requirement:</span></p></td><td colspan="2" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; margin-bottom:12pt; text-indent:-21.3pt"><span>1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>Inspect the cargo door lower belt frames at the cargo latch receptacles for cracks in accordance with Part A of the Accomplishment Instructions section in Fairchild Aircraft SA226 Series Service Bulletin 226-53-007, issued 7 May 1981, revised 17 February 1992; or SA227 Series Service Bulletin 227-53-003, issued 29 January 1986, revised 13 February 1986; as applicable.</span></p><p style="margin-top:12pt; margin-left:21.3pt; margin-bottom:12pt; text-indent:-21.3pt"><span>2.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>If cracks are found, accomplish the following:</span></p><p style="margin-top:12pt; margin-left:42.55pt; margin-bottom:12pt; text-indent:-21.25pt"><span>-</span><span style="width:17.25pt; text-indent:0pt; display:inline-block"> </span><span>For belt frames located at Fuselage Station (FS) 438.060 and FS 491.060, repair the belt frame by installing angle part number (P/N) 27-22206-009 or 27-22206-010, in accordance with the Fairchild Aircraft SA226 / 227 Structural Repair Manual (SRM), Section 53-90-20, initial issue 1 March 1983, Revision 24, dated 27 August 1997; or Fairchild Aircraft Approved Repair Procedure (ARP) 53-30-9701, dated 28 July 1997.</span><span> </span><span>The reinforcement doublers (P/N 27-22206-007 and -008) are also needed together with this repair.</span></p><p style="margin-top:12pt; margin-left:42.55pt; text-indent:-21.25pt"><span>-</span><span style="width:17.25pt; text-indent:0pt; display:inline-block"> </span><span>For belt frames located at FS 454.501, FS 455.726, FS 473.392, and FS 474.657, replace all four belt frames with new design frames, P/N</span><br><span>27-22207-008, 27-22208-005, and 27-22207-007, respectively, in accordance with the SA226 / 227 SRM, Section 53-90-20; or, ARP</span><br><span>53-30-9701.</span><span> </span><span>No reinforcement doublers are needed for these four new design belt frames.</span></p></td></tr></tbody></table>