Airworthiness directives › 2024-05-03
AD 2024-05-03 Airworthiness Directives; The Boeing Company Airplanes
Models named: 767-200, -300, -300F, -400ER series, 767-2C series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to The Boeing Company airplanes, certificated in any category, identified in paragraphs (c)(1) and (2) of this AD. (1) Model 767-200, -300, -300F, and -400ER series airplanes, as identified in Boeing Alert Requirements Bulletin 767-53A0301 RB, Revision 2, dated May 24, 2023. (2) Model 767-2C series airplanes, line numbers 1065, 1066, 1067, 1069, 1091, 1092, 1098, 1100, 1102, 1104, 1107, 1109, 1111, 1113, 1114, 1116, 1117, 1119, 1120, 1122, 1124, 1126, 1128, 1129, 1131, 1132, 1134, 1135, 1137, 1139, 1143, 1145, 1147, 1149, 1151, 1154, 1156, 1158, 1160, 1162, 1164, 1166, 1168, 1170, 1172, 1174, 1176, 1178, 1181, 1184, 1188, 1192, 1196, 1200, 1202, 1205, 1207, 1210, 1213, 1216, 1219, 1223, 1226, 1230, 1234, 1236, 1238, 1241, 1243, 1246, 1248, 1250, 1252, 1254, 1257, 1259, 1261, 1264, 1267, 1269, 1271, and 1273.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
For Model 767-200, -300, -300F, -400ER series airplanes: Except as specified by paragraph (h) of this AD, at the applicable times specified in the “Compliance” paragraph of Boeing Alert Requirements Bulletin 767-53A0301 RB, Revision 2, dated May 24, 2023, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 767-53A0301 RB, Revision 2, dated May 24, 2023. Note 1 to paragraph (g): Guidance for accomplishing the actions required by this AD can be found in Boeing Alert Service Bulletin 767-53A0301, Revision 2, dated May 24, 2023, which is referred to in Boeing Alert Requirements Bulletin 767-53A0301, Revision 2, dated May 24, 2023.
Unsafe condition
This AD was prompted by a report of cracks found on the forward entry door and forward service door cutout aft lower corner fuselage skin and bear strap. The FAA is issuing this AD to address undetected fatigue cracks. The unsafe condition, if not addressed, could result in a principal structural element losing its limit load capability, adversely affecting the airplane's structural integrity.
Affected ADs
None.
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