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# "" PUBLICATION IN THE FEDERAL REGISTER]. c..:nainpublications listed illthe AD as of [INSERT DATE 15 DAYS APTER DATE OF Register approved the incorpon:l\ion by reti:rencc of <I c8nain publication listed in the AD. DATES: This AD becomes efl'ectiv<,[fNSERT D:'\TE 15DAYS /' .•.. FTER DATE OF PUBLICATION IN THE FEDER,'\!. REGISTER].

On March 5.1001 (66 FR 8085, January ~9_200 I), Ill" Director Ofllw Pederal The Director ol-the Federal Register approved tile illCOrpul"<llioll by rdercilce of provides Optil1nalterminating action, which ends the repetitive il1Sp~·clions. This new AD federal Aviation AdministratiOIl

currcnlly rcquires repetitive detailed and edd) current inspections to deteci cracks or applies toccnain Modd 767-200. -300, and -300F s.:ries airplanes. The existing AD

engine due tocorrosion damage and cracking Orb(llh fuse pillSon the same stl'UI. ACTION: Final rul.:: requ.:st forcomments.

a fraclur~d midspal' filse pin. We are issuing this AD 10 pre\ ent loss of the strut and requires reduced repeal intervals forcen<lininspectiollS This AD result~ frolllfIreport of corrosion ofcenain midspar fus.: pins_and corrective anions ifnccessar~. Th:ll AD also



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(DOT). SUMMARY: The FAA is superseding an ~xisting aifIVOl1hill~S!> direCll\c (AD) that ,\irworthiness Directives: The Boeing Comp.1n) ~'Iodel 767-200. -300. and -300F Scries Airplanes AGENCY: Federal Aviation Adminismuion (FAA). Depanmem ofTransponation1491O-13-PI

DEPARTMENT OF TRANSPORTATION F'ederal Aviation Administration 14CFR Part 39 [Docket No. FAA-2010-+++++; Directorate Identifier 2009-NM-266-AD; Amendment 39-**; AD **1 RIN 2120-AA64 Airworthiness Directives; TIle Boeing Company' Model 767-200, -::iDa, and -300F Series Airplanes AGENCY; Federal Aviation Administration (FAA), Department ofTransportatioll (DOT). ACTION: Fillal rule: request forcomments. SUMMARY; The FAA is superseding an ~xjs!ing airworthiness directive (AD) thai applies to certain Model 767-100, -300, and -JOQFseries airplanes. The existing AD nliTently requires repetitive detailed and eddy curren! inspections todetecl cracks or corrosion ofcertain midspar fuse pins, and corrective actions ifnecessary. That AD also pnlvic!es optional terminating action, which ends the repetitive inspections. This new AD requires reduced repeat intcrvnls forcertain inspections_This AD results frol11a repOt1of a fractured rnidspar fuse pin. We are issuing this AD to prevent loss oflhe strut and engine due 10corrosion damage and cracking ofboth fuse pillSon the same strut. DATES: This AD becomes effective [INSERT DATE 15DAYS AFTER DATE OF PUBLICATION INTHE FEDERAL REGISTER]_ The Director orthe Federal Register approved the incorporaticm by reference of certain publications listed in theAD as of[INSl:RT DATE 15DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL REGISTER]. On March 5, 2001 (G6 FR S085, January 29, 2001), the Director oflhe Federal Register approved the incorporation by reference Ma certain publication liSled inthe AD :ONr.URRE"[ES oun"G snlllDl 

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Fcdual Aviation Administration 14CFR Part 39 [Dock.etNo. FAA-20 I0.+++++; Directorate Identifier 2009-NM-266-AD; Amendment 39·**; AD **1 RIN 2110-AA64 Airworthiness Directives; The Boeing Company Model 767-200, ~300, and -300F ,; ,sill - 

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Series Airplanes AGENCY: Federall\viatiol1 Administration (FAA), Department ofTransportation (DOn. ACTION: Final rule; request forcomments. SUMMARY: The FAA is superseding an existing airworthiness directive (AD) that applies 10certain Model 767-200, ~300, and -300F series airplanes_The existing AD currently requires repetitive detailed and eddy current inspections todetect cracks or corrosion ofcertain midspar fuse pins, and corrective actions ifnecessary. That AD also provides optional temlinating action, which ends the repetitive inspections_ This new AD requires reduced repeat intervals for certain inspections. This AD resul,s from a report of a fractured midspar fuse pin. We are issuing this AD to prevenl loss ofthe strut and engine due to corrosion damage and cracking ofboth fuse pins on the same strut. DATES: This AD becomes effective [INSERT DATE 15 DAYS AI·TER DATE OF PUBLICATION INTHE fEDERAL REGISTER]. The Director oflhc Federal Register approved the incorporation by reference of certaill publicaTions listed in the AD as of[INSERT DATE 15DAYS AFJER DATE OF PUBIJCATION INTHE FEDERAL REGISTER]. On March 5, 2001 (66 FR 8085. January 29, 200t), the Director of the Federal Register approved the incorporation by reference of acertain publication listed in the AD. ItlITIAt.$ISIG DAT~ OVTIm:; SYMBOL tllTIAlSISlG

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