(4910-I3-Pj

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

mOCk$;! No. FAA-2008-0295; Di.-ectorate Identifier 2007-NM-298-AD; Amendme

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RlN 2120-AA64

Ai.-worthincss Directives; The Boeing Company Model 757 Airplanes

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AGENCY: Federal Aviation Administration (FAA), Department ofTransportatioll

(DOT).

ACTION: Final rule.

SUMMARY: The FAA is adopting a new ainyorthiness directive (AD) for Model

757-200, -200PF, -lODCB, and -300 series airplanes. This AD requires an inspection 0

the two spring arms in the spin brake assemblies in the nose wheel well 10 determine if

the spring amlS are made of aluminum or composite material, and repetitive related

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investigative/corrective actions ifnecessary. This AD also provides options for

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

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

DATES: This AD becomes effective [INSERT DATE 35 DAYS AFTER DATE OF

,TO

tenninating the repetitive actions, This AD results from reports of cracked and broken

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aluminum springs, We are issuing this AD to detect and correct cracked or broken

springs. A cracked or broken spring could sepJate from the airplane and result in

potential hazard to persons or property on the Jound, or ingestion into the engine with

engine damage and potential shutdown, or damage to the airplane.

certain publication listed in the AD as of [INSERT DATE 35 DAYS AFTER DATE 0

PUBLICATION IN THE FEDERAL REGISTER].

PUBLICATION IN THE FEDERAL REGISTER].
14910-13-P)

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration ONCURR"NCCS

R.OUnNG SYMBOL

14 CFR Part 39

39-*'; AD **)

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(Docket No. FAA-2008-0295; Directorate Ide tiller 2007-NM-298-AD; Amendment . t-{d-d-e.li

DATE

1-30-10

RlN 2120-AA64

Ainvorthiness Directives; The Boeing Company Model 757 Airplanes

I

AGENCY: Federal Aviation Adminish"ation (F!A.A),Department of Transportation

ROUn"G SyMBOL

DATE;

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for Model DA~

757-200, -200PF, -200CB, and -300 series airplLes. This AD requires an inspection of Ro"~ny-sv2o, l =-

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. . b . b ak bl I b h I II d . .j. J t,"" / 7f!; t e two spnng 3mlS ill t e spm r e assem les In t e nose w ee we to etermme 1 NmALSlslq ~

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· d fl· I. I d . . I d f'i"l>.ue; "1""-

t le spnng arms are ma e 0 a ummum or compOSItematena ,an repetltJVere ate A~

investigative/corrective actions if necessary. Thi1sAD also includes a pm1s installation

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paragraph and provides options tor terminating the repetitive actions. This AD results ~

from reports of cracked and broken aluminum sJrings. We are issuing this AD to detect DATE

and correct cracked or broken springs. A crackel or broken spring could separate from «b tv j ROUTING SYMllOl

the airplane and result in potential hazard to persons or property on the grolllld, or I mTIALSI$IG

ingestion into the engine with engine damage and potential shutdown, or damage to the

(DOT).

ACTION: Final rule.

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airplane.

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DATES: This AD becomes effective [INSERT DATE 35 DAYS AFTER DATE OF

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PUBLICATION IN THE FEDERAL REGISTER].

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DATE

The Director of the Federal Register app oved the incorporation by reference of

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certain publication listed in the AD as of [INSEjT DATE 35 DAYS AFTER DATE OF

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PUBLICATION IN THE FEDERAL REGISTER].

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