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AD/CESSNA 337/30 - Pitot Tube Installation
Cessna 337 Series AeroplanesCessna 337 Series Aeroplanes
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Cessna 337 Series Aeroplanes
| AD/CESSNA 337/30 | Pitot Tube Installation | 6/2008 |
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<table cellspacing="0" cellpadding="0" style="width:510.3pt; 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 colspan="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Model 337 series aircraft modified in accordance with United States Federal Aviation Administration (FAA) Supplemental Type Certificate (STC) SA1627WE with the following serial numbers:</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:58.45pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>337-0058 337-0063 337-0124 337-0205 337-0220 337-0291 337-0305 337-0327 337-0332 337-0443 337-0502 337-0540</span></p></td><td style="width:60.2pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>337-0549 337-0566 337-0577 337-0685 337-0695 337-0726 337-0728 337-0732 337-0741 337-0817 337-0822 337-0836</span></p></td><td style="width:60.15pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>337-0880, 337-0882, 337-0896 337-0916 337-0925 337-0929 337-0938 337-0942 337-0946 337-0947 337-0959 337-0963</span></p></td><td style="width:60.2pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>337-0970 337-0977 337-0992 337-0996 337-1019 337-1036 337-1044 337-1052 337-1062 337-1072 337-1073 337-1079</span></p></td><td style="width:53.05pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>337-1082 337-1091 337-1108 337-1118 337-1124 337-1139 337-1154 337-1159 337-1162 337-1175 337-1177 337-1180</span></p></td><td style="width:69pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>337-1192 337-1210 337-1232 337-1258 337-1262 337-1274 337-1276 337-1303 337-1307</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span></span></p></td><td colspan="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 1:</span><span> </span><span>STC SA1627WE which was originally held Robertson Aircraft Corporation, </span><span>839 West Perimeter Rd</span><span>, </span><span>Renton</span><span>, </span><span>WA</span><span>, the STC is now held by Sierra Industries Ltd, </span><span>122 Howard Langford Dr</span><span>, </span><span>Uvalde</span><span>, </span><span>TX</span><span>.</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="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>If not previously accomplished, rework the extended pitot tube by installation of Robertson Kit No. 14-118-100 in accordance with Robertson modification instructions No 14-118-10 dated 23 January 1975.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 2:</span><span> </span><span>The requirements of this Directive may have been accomplished prior to the aircraft’s arrival in Australia and the aircraft’s maintenance records may indicate compliance with FAA AD 75-09-05, this is considered acceptable for compliance with this Directive.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 3:</span><span> </span><span>FAA AD 75-09-05 Amdt 39-2177 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 colspan="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Within 100 hours time in service after the effective date of this Directive.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="6" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>This Airworthiness Directive becomes effective on 5 June 2008.</span></p></td></tr></tbody></table>