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PUBLICATION IN THE FEDERAL REGISTER].

c..:nain publications listed ill the 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 15 DAYS /'.•..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"<lliollby 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 to ccnain Modd 767-200. -300, and -300F s.:ries airplanes. The existing AD

engine due to corrosion damage and cracking Orb(llh fuse pillS on the same stl'UI.

ACTION: Final rul.:: requ.:st for comments.

a fraclur~d midspal' filse pin. We are issuing this AD 10 pre\ ent loss of the strut and

requires reduced repeal intervals for cen<lin inspectiollS This AD result~ frolll fIreport of

corrosion of cenain midspar fus.: pins_ and corrective anions if nccessar~. Th:ll AD also

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IDockel No. fAA.2010-t-+-++-i-; Directorate Identifier l009-NM-166-AD;

Amendment 39-**: AD "'~ a-Ol 0- 03 ~o8

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RIN 2120-AA64 "- \(0 \ '11--

(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 ofTransponation
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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 for comments.

SUMMARY; The FAA is superseding an ~xjs!ing airworthiness directive (AD) thai

applies to certain Model 767-100, -300, and -JOQF series airplanes. The existing AD

nliTently requires repetitive detailed and eddy curren! inspections to detecl cracks or

corrosion of certain midspar fuse pins, and corrective actions if necessary. That AD also

pnlvic!es optional terminating action, which ends the repetitive inspections. This new AD

requires reduced repeat intcrvnls for certain 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 of both fuse pillS on the same strut.

DATES: This AD becomes effective [INSERT DATE 15 DAYS AFTER DATE OF

PUBLICATION IN THE FEDERAL REGISTER]_

The Director orthe Federal Register approved the incorporaticm by reference of

certain publications listed in theAD as of[INSl:RT DATE 15 DAYS 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 in the AD

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DEPARTMENT OF TRANSPORTATION

Fcdual Aviation Administration

14CFR Part 39

[Dock.et No. 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

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Series Airplanes

AGENCY: Federall\viatiol1 Administration (FAA), Department of Transportation

(DOn.

ACTION: Final rule; request for comments.

SUMMARY: The FAA is superseding an existing airworthiness directive (AD) that

applies 10 certain Model 767-200, ~300, and -300F series airplanes_ The existing AD

currently requires repetitive detailed and eddy current inspections to detect cracks or

corrosion of certain midspar fuse pins, and corrective actions if necessary. 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 of the strut and

engine due to corrosion damage and cracking of both fuse pins on the same strut.

DATES: This AD becomes effective [INSERT DATE 15 DAYS AI·TER DATE OF

PUBLICATION IN THE fEDERAL REGISTER].

The Director oflhc Federal Register approved the incorporation by reference of

certaill publicaTions listed in the AD as of[INSERT DATE 15 DAYS AFJER DATE OF

PUBI JCATION IN THE FEDERAL REGISTER].

On March 5, 2001 (66 FR 8085. January 29, 200t), the Director of the Federal

Register approved the incorporation by reference of a certain publication listed in the AD.

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