### 14CFR 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 

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39-**;AD2010_J.fi-)-O 

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### Airworthiness Directives; The Boeing Company Model 767·200, -300, and -300F Series Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request forconunents. 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&Ilestruts, and related investigative and I 

### COITcctive

actions ifnecessary. The existing AD also provides temlinating action forth repetitive inspections. This AD revises certain criteria forthe tenllinating action. This was prompted by two reports ofcracked 

## UPPC11ink fuse pins. We are issuing this AD t prevent fatigue cracking or corrosion ofthe u~per link fuse pin, which could result in OUIINGSYMOOL

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### failure ofthe fusepin and consequent reduced structural integrity ofthe nacelle strut a A'IE 

### possible separation ofthe strut and engine fr0T the airplane during flight. DATES: This AD is effective [IJ'ISERT DATf 15DAYS AFTER DATE OF PUBLICATION IJ'ITHE FEDERAL REGISTER]. The Director ofthe Federal Register a~provcd the incorporation by 

### reference 0 

### aUTThG~'-""IIOL certain publication listed in the AD as of [INSERT DATE 15DAYS AFTER DATE 

## 0 PUBLICATION INTHE FEDERAL REGISl'ER].[4910~13-PI DEPARTMENT OF TRANSPORTATION

RIN 2120-AA64 OU1'N(i SWBOL :ONCUKRErK~S OUnNG S'MBOl



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DATES: This AD is effective [INSERT DATE 15 DAYS AFrER DATE OF PUBLICATION INTHE FEDERAL REGISTER]. repetitive inspections. This AD revises certain criteria forthe terminating action. This AD

The Director ofthe Federal Register approved the incorporation by reference ofa certain publication listed in the AD as of [INSERT DATE 15DAYS AFTER DATE OF PUBLICATION INTHE FEDERAL REGISTER]. prevent fatigue cracking or corrosion ofthe upper link fuse pin

## r which could result in failure of the fuse pin and consequent reduced structural integri1tyofthe nacelle strut and possible separation of the strut and engine from the airplane during flight. was prompted by tWO

reports ofcracked upper link fuse pins. We are issuing this AD to corrosion ofthe upper link fuse pin ofthe nacelle struts, and related investigative and corrective actions ifnecessary. The existing AD also provides ierminating action forthe 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 anew airworthiness directive (AD) forthe products listed above, That AD currently requires repetitive inspections for fatigue cracking and federal Aviation Administration 14CFR Part 39 

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

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