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AD/CIRRUS/9 - Rudder and Aileron Rigging
Cirrus Design SR20 and SR22 Series AeropCirrus Design SR20 and SR22 Series Aeroplanes
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Cirrus Design SR20 and SR22 Series Aeroplanes
| AD/CIRRUS/9 | Rudder and Aileron Rigging | 5/2008 |
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<table cellspacing="0" cellpadding="0" style="margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Applicability:</span></p></td><td style="width:413.9pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Cirrus Design Corporation </span><span>Model SR20 aeroplanes, serial numbers (SN) 1005 through 1861, and Model SR22 aeroplanes, SN 0002 through 2333, SN 2335 through 2419, and SN 2421 through 2437 all inclusive.</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 style="width:413.9pt; 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 rudder, aileron, and rudder-aileron interconnect rigging; correct any out-of-rig condition; and replace the attaching hardware for the rudder-aileron interconnect in accordance with Cirrus Service Bulletin No. SB 2X-27-14 R3, dated 10 October 2007.</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>Report to CASA via the Service Difficulty Reporting (SDR) system </span><span style="text-decoration:underline">any</span><span> out-of-rig conditions discovered as a result of the inspection detailed in Requirement 1 of this AD.</span></p><p style="margin-top:12pt; margin-left:21.3pt"><span>Include the following information in the report.</span></p><table cellspacing="0" cellpadding="0" style="width:100%; margin-top:0pt; margin-bottom:0pt; border:0.75pt solid #000000; border-collapse:collapse"><tbody><tr style="height:19.85pt"><td style="width:48.98%; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:middle"><p style="margin-top:0pt; margin-left:34.3pt; margin-bottom:0pt; text-indent:-21.25pt"><span>1.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Inspection Performed By:</span></p></td><td style="width:49.92%; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:middle"><p style="margin-top:0pt; margin-left:36.05pt; margin-bottom:0pt; text-indent:-21.25pt"><span>2.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Telephone:</span></p></td></tr><tr style="height:19.85pt"><td style="width:48.98%; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:middle"><p style="margin-top:0pt; margin-left:34.3pt; margin-bottom:0pt; text-indent:-21.25pt"><span>3.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Aircraft Model:</span></p></td><td style="width:49.92%; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:middle"><p style="margin-top:0pt; margin-left:36.05pt; margin-bottom:0pt; text-indent:-21.25pt"><span>4.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Aeroplane Serial Number:</span></p></td></tr><tr style="height:31.2pt"><td style="width:48.98%; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:middle"><p style="margin-top:0pt; margin-left:34.3pt; margin-bottom:0pt; text-indent:-21.25pt"><span>5.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Aircraft Total Hours Time-in-Service:</span></p></td><td style="width:49.92%; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:middle"><p style="margin-top:0pt; margin-left:36.05pt; margin-bottom:0pt; text-indent:-21.25pt"><span>6.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Date of inspection detailed in Requirement 1 of this AD:</span></p></td></tr><tr style="height:19.85pt"><td style="width:48.98%; border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:top"><p style="margin-top:3pt; margin-left:34.3pt; margin-bottom:0pt; text-indent:-21.25pt"><span>7.a.</span><span style="width:3.92pt; text-indent:0pt; display:inline-block"> </span><span>Do any of the aircraft logs contain entries describing flight control system maintenance, preventative maintenance, or alteration:</span><br><br><span>___ Yes ___ No</span></p></td><td style="width:49.92%; border-top:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding:0.38pt; vertical-align:top"><p style="margin-top:3pt; margin-left:36pt; margin-bottom:12pt; text-indent:-21.25pt"><span>7.b.</span><span style="width:3.25pt; text-indent:0pt; display:inline-block"> </span><span>If Yes, copy the log book entry(s) and include the date of the entry.</span></p></td></tr><tr style="height:33.15pt"><td colspan="2" style="border-top:0.75pt solid #000000; padding:0.38pt; vertical-align:middle"><p style="margin-top:0pt; margin-left:34.3pt; margin-bottom:0pt; text-indent:-21.25pt"><span>8.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Inspection Results: (Report only if an out-of-rig condition is found, and describe the out-of-rig condition as accurate and detailed as possible):</span></p></td></tr></tbody></table><p class="Note" style="margin-bottom:12pt"><span>Note 1:</span><span> </span><span>There is no need to report if there are no out-of-rig conditions discovered.</span></p><p class="Note" style="margin-top:12pt"><span>Note 2:</span><span> </span><span>FAA AD 2008-03-16 Amdt 39-15367 dated 29 January 2008 refers.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Compliance:</span></p></td><td style="width:413.9pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>Within the next 25 hours time-in-service (TIS) after the effective date of this AD or within the next 3 months after the effective date of this AD, whichever occurs first.</span></p></td></tr></tbody></table>