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DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 (Docket No. Fi}.{\-20JO-0127; Directorate Identifier 2009-NM-242-ADj



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### 39-**; AD 2010-**-""*) Q



# ,lG-Oo R1N 2120-AA64 - 

### Airworthiness Directives; The Boeing Company Model 767 Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUM-MARY: We are adopting anew airworthiness directive (AD) forthe products list above. This AD requires adetailed inspection ofthe entryway door movable ceiling p for

### pin Il1igrationat either end ofthe hinge assembly and damage tothe pin; a detailed inspection for correct crimp atboth ends and damage tohinge stock; adetailed inspecti ofthe ceiling area for any visible cosmetic and/or tie-rod chaiing that could be caused b
amigrated hinge pin; and adetailed inspection ,forwire damage and/or breakage; and 

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### other specified and corrective actions ifnecessary. This AD results fiom reports of fault ROI}1'JN(] S1'''»OL 

### messages caused by improperly crimped hinge pins coming into contact with wires and

### b"~m~,~~,~,,,~-- causing damage. We are issuing this AD to detect and correct improperly crimped hing,~,",,",,

_ pins, which could damage tie rods and wire bundles, causing shorts in many systems, including the spar fuel shut off valve, oxygen mask deployment, and bumed wires, whj~,IJ'Th;"W','''''''''--- could be an ignition source 1nahidden area ofthe airplane. DATES: This AD iseffective [INSERT DATE 35 DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL REGISTER]. 

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1~IlIAL':;''''',1491Q-JJ-PJ DEPARTMENT OF TRANSPORTA nON ::<)NCIZI'<'H':;($ o<m~(iSY""Ol Federal A\'jation Administration 

### 14erR Part 39 IDocket No. FAA-20I0-0U?; Directo.-atc Identifier 2009-NM-242-AD; ~ 

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## /fN~-Ia;5 Amendment 39-**; AD 2010-**-**1 RIN 2.120-AA64

messages caused by improperly crimped hinge piryscoming into contact with wires and causing damage. We are issuing this 

### .W 10detect ,andcorrect improperly crimped hinge 

## , inspection [orcorrect crimp at both ends and damage to hinge stock; adetailed inspeCliol ArE \ i0 / 1.- 

## ,,-i.-~ orthe ceiling area for any visible cosmetic and/or lie-fad chafing thal could be caused by (lL," S'i. amigrated hinge pin; and adetailed inspection fOjwire damage and/or breakage; and other specified and corre.ctive actions ifnecessary. This AD results from reports of fault Airworthiness Directives; The Boeing Company Model 767 Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION, Final rule. \ 

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. SUMl\lARY: We are adopting anew airworthiness directive (AD) for the products lisle 

## A"'I I I to "l-•... -<;> above. This AD requires adetailed inspection of the entryway door movable cciUng pan 

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# I f,NM-l.~$ rOf pin migration ateither end of the hinge assembly and damage to the pin; adetailed 

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pins, which could damage lie rods and wire bundles, causing shorts in many systems, n~ including the spar fuel shut off valve, oxygen mask deployment, and burned wires, which ;8 -}l'7-/(;1 \ OUT1N~S,,,"OL

_ could be an ignition source in ahidden area of the airplane. r 

## W£ DATES: This AD iscffeclive [INSERT DATE 3sJ

## 1DAYS AFTER DATE OF PUBLICATION INTHE FEDERAL REGISTER].