DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

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ACTION: Final rule.

above. This AD requires repetitive inspections for cracks in the fuselage skin and bac

[Docket No. FAA-2010-0796; Directorate Identifier 2010-NM-007-AD;

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Amendment 3.9-"*; AD ***'*-"'*-**[

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RIN 2120-AA64

ACENCY: Federal Aviation Administration (FAA), DOT.

Ainvorthincss Directives; The Boeing Company Model 767-300 Serles Alrplancs

SUMMARY: We arc adopting a new air..vorthincss directive (AD) n)l" the products Ii.

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structure at the lower very high frequency (VI-IF) antenna cutout at station I 197 +- 99

baseplate at station 1197 + 99. We arc issuing this AD to detce! and correct fatigue en ks

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in the fuselage skin and internal backup structure, which could resull in rapid \&

between sLringers 39 Jen and 39 right. and correclive actions if necessary. Certain rep' ~e

terminate certain Inspection requirements. This AD was prompted by reporLs 01-cracki

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found in the section 46 fuselage lower skin around the periphery ofLhc VHF antenna _2- -

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decompression of the airplane,

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PUBLlCATION IN TilE FEDERAL REGISTER].

Conunercial Airplanes, Attention: Data & Services Management, P.O. 1301'3707,

ADDRESSES: For service information identified in this AD, contact Boeing

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certain publication listed in the AD as of [INSERT DATE 35 DA YS AFTER DATE ( F

DATES: This AD is effective [lNSERT DATE 35 DAYS AFTER DATE OF

PUBLICATION IN THE FEDERAL REGISTER]

The Director of the Federal Register appro\'Cd the incorporation by reference

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DEI'ART!I1ENT OF TRANSPORT AnON 'CNCURilWCI'5

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Federal A"iation Administration

14 CFR Part 39

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The Director of the Federal Register approved the lllcorporation by reference

PUBLICATION IN THE FEDERAL REGISTER].

certam publicati,on ]j~ted in the AD us of [INSERT DATE 35 DA YS AFTER DATE

Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707,

ADDRESSES: For service information identiftcd in this AD, contaci Boeing

DATES: This AD is effective (lNSERT DATE 35 DAYS AFTER DATE OF

PUBLlCATJON IN THE FEDERAL REGISTER].

decompression of the airplane.

above. This AD requires repetitive lllspections for cracks in the fuselage skin and bac

(Docket No. FAA-2010-0796j Directorate Identifier 2010-NM-OO?-AD;

Amendment 39-*:*; AD ****-**-'"*]

Airworthiness Directives; The Boeing Company Model 767-300 Series Airplanes

RIN 2120-AA64

structure at the lower very high frequency (VHF) amenna cutout at station 1197 + 99 ,',mM.$JMG

between stringers 39 left and 39 right, and corrective actions if necessary. CerL:iin rep _\ f=t,¢...(J ~

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tcnninate certain inspection requirements. This AD was prompted by reports of crackj' .o:%J'tl 'l i:l

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it1Und in tbe section 46 fuselage lower skin around the periphery of the VHF antenna 5' G NmJ'l.>;,lSIG

baseplate at station 1197 + 99. We arc issuing this AD to detect and correct fatigue cr ks5ee.--

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in the fuselage skin and ioLernal backup stmcture, which could result in rapid ~

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

SUMMARY: We are adopting a new airworthiness directive (AD) for the products J.i

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