14 CFR Part 39

14910-13-PI

DEPARTMENT OF TRANSPORT AnON

federal Aviation Administration

iD:30

IDocket No. FAA-10lO-++++; Directorate Identifier 2009-NM-247-ADj Amendm

\0A~t)39-**;AD2010_J.fi-)-O I

\ RJN 212Q-AA64

Airworthiness Directives; The Boeing Company Model 767·200, -300, and -300F

Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for conunents. OJ S'"MiIOl

OIITJ~GS\'MOOL.

SUMMARY: We are superseding a new airworthiness directive (AD) for the products N1TIAL.'itSXi

listed above. That AD currently requires repetitive inspections for fatigue cracking and An!

corrosion of the upper link fuse pin of the nac&Ile struts, and related investigative and

I

COITcctiveactions ifnecessary. The existing AD also provides temlinating action for th

repetitive inspections. This AD revises certain criteria for the tenllinating action. This

was prompted by two reports of cracked UPPC11ink fuse pins. We are issuing this AD t

prevent fatigue cracking or corrosion of the u~per link fuse pin, which could result in

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failure of the fuse pin and consequent reduced structural integrity of the nacelle strut a A'IE

possible separation of the strut and engine fr0T the airplane during flight.

DATES: This AD is effective [IJ'ISERT DATf 15 DAYS AFTER DATE OF

PUBLICATION IJ'ITHE FEDERAL REGISTER].

The Director of the Federal Register a~provcd the incorporation by reference 0 aUTThG~'-""IIOL

certain publication listed in the AD as of [INSERT DATE 15 DAYS AFTER DATE 0

PUBLICATION IN THE FEDERAL REGISl'ER].
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DEPARTMENT OF TRANSPORTATION

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DATES: This AD is effective [INSERT DATE 15 DAYS AFrER DATE OF

PUBLICATION IN THE FEDERAL REGISTER].

repetitive inspections. This AD revises certain criteria for the terminating action. This AD

The Director of the Federal Register approved the incorporation by reference of a

certain publication listed in the AD as of [INSERT DATE 15 DAYS AFTER DATE OF

PUBLICATION IN THE FEDERAL REGISTER].

prevent fatigue cracking or corrosion of the upper link fuse pin

r

which could result in

failure of the fuse pin and consequent reduced structural integri1tyof the nacelle strut and

possible separation of the strut and engine from the airplane during flight.

was prompted by tWOreports of cracked upper link fuse pins. We are issuing this AD to

corrosion of the upper link fuse pin of the nacelle struts, and related investigative and

corrective actions if necessary. The existing AD also provides ierminating action for the

I

Airworthiness Directives; The Boeing Company Model 767-200, -300, and -300F

S

· . I I enes Alrp anes

39-**; AD 2010-**-**)

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments. I

SUMMARY: We are superseding a new airworthiness directive (AD) for the products

listed above, That AD currently requires repetitive inspections for fatigue cracking and

federal Aviation Administration

14 CFR Part 39 I

[Docket No. fAA-2010-++++; Directorate Identifier 2009-NM-247-AD; Amendment

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