AD 90-25-05 R1

AD Final Rules - 90-25-05R1_Correction.pdf
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AD Number:
90-25-05 R1
Document Type:
AD Final Rules
Docket Number:
FAA-2007-0412
Subject Heading:
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-200...Show more
Subject:
Corrosion prevention and control program
Status:
Current
Citation:
(Federal Register: January 7, 2008 (Volume 73, Number 4))
Citation Publish Date:
01/07/2008
Effective Date:
01/22/2008
Make:
The Boeing Company
Model:
747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...Show more
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
90-25-05
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
CORRECTION: (Federal Register: February 14, 2008 (Volume 73, Number 31); Page 8589-8591;\nwww.access.gpo.gov/su_docs/aces/aces140.html)
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[Federal Register: February 14, 2008 (Volume 73, Number 31)]


[Rules and Regulations]


[Page 8589-8591]


From the Federal Register Online via GPO Access [wais.access.gpo.gov]


[DOCID:fr14fe08-5]


––––––––––––––––––––––––––––––––––


DEPARTMENT OF TRANSPORTATION


Federal Aviation Administration


14 CFR Part 39


[Docket Nos. FAA-2007-0410, FAA-2007-0411, and FAA-2007-0412; Directorate Identifiers


2007-NM-338-AD, 2007-NM-291-AD, and 2007-NM-290-AD; Amendments 39-15325, 39-15326,


39-15327; ADs 2008-01-02, 2004-07-22 R1, and 90-25-05 R1]


RIN 2120-AA64


Airworthiness Directives; Viking Air Limited Model (Caribou) DHC-4 and (Caribou) DHC-4A


Airplanes; and Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-


200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes


AGENCY:
 
Federal Aviation Administration (FAA), Department of Transportation (DOT).


ACTION:
 
Final rule; corrections.


––––––––––––––––––––––––––––––––––


SUMMARY:
 
The FAA is correcting typographical errors in three existing airworthiness directives


(ADs) that were published in the Federal Register on January 8, 2008 (73 FR 1269); January 7, 2008


(73 FR 1052); and January 7, 2008 (73 FR 1055). The errors resulted in incorrect docket numbers.


One AD applies to all Viking Air Limited Model (Caribou) DHC-4 and (Caribou) DHC-4A airplanes.


The other two ADs apply to all Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-


200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes. The


Viking Air AD requires doing a fluorescent penetrant inspection for cracking of certain upper engine


mount bracket assemblies, and corrective actions if necessary. One of the Boeing ADs requires


revising the FAA-approved maintenance inspection program to include inspections that will give no


less than the required damage tolerance rating for each structural significant item, and repair of


cracked structure. The other Boeing AD requires implementing a corrosion prevention and control


program.


DATES:
 
AD 2008-01-02 is effective January 23, 2008. ADs 2004-07-22 R1 and 90-25-05 R1 are


effective January 22, 2008.


ADDRESSES:
 
You may examine the AD dockets on the Internet at http://www.regulations.gov; or


in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday,


except Federal holidays. The AD dockets contain this AD, the regulatory evaluation, any comments


received, and other information. The address for the Docket Office (telephone 800-647-5527) is the
2


Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West


Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590.


FOR FURTHER INFORMATION ON AD 2008-01-02, CONTACT:
 
George Duckett, Aerospace


Engineer, Airframe and Propulsion Branch, ANE-171, FAA, New York Aircraft Certification Office,


1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228-7325; fax (516)


794-5531.


FOR FURTHER INFORMATION ON ADs 2004-07-22 R1 and 90-25-05 R1, CONTACT:
 
Ivan


Li, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office,


1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 917-6437; fax (425) 917-


6590.


SUPPLEMENTARY INFORMATION:
 
We have issued the ADs identified in the following table.


Affected ADs


AD –
 
Affects –
 
And requires –


2008-01-02, amendment


39-15325 (73 FR 1269,


January 8, 2008), issued


December 20, 2007


All Viking Air Limited Model


(Caribou) DHC-4 and (Caribou)


DHC-4A airplanes


A fluorescent penetrant inspection


(FPI) for cracking of certain upper


engine mount bracket assemblies,


and corrective actions if necessary.


2004-07-22 R1,


amendment 39-15326 (73


FR 1052, January 7,


2008), issued


December 26, 2007


All Boeing Model 747-100,


747-100B, 747-100B SUD,


747-200B, 747-200C,


747-200F, 747-300, 747-400,


747-400D, 747-400F, 747SR,


and 747SP series airplanes


Revising the FAA-approved


maintenance inspection program to


include inspections that will give


no less than the required damage


tolerance rating for each structural


significant item, and repair of


cracked structure.


90-25-05 R1, amendment


39-15327 (73 FR 1055,


January 7, 2008), issued


December 26, 2007


All Boeing Model 747-100,


747-100B, 747-100B SUD,


747-200B, 747-200C,


747-200F, 747-300, 747-400,


747-400D, 747-400F, 747SR,


and 747SP series airplanes


Implementing a corrosion


prevention and control program.


(That AD revised an earlier AD by


removing future type-certificated


models from the applicability.)


As published, those ADs specify incorrect docket numbers throughout the preamble and


regulatory text. Docket numbers are assigned by the Federal Document Management System. We


have been informed that incorrect docket numbers were assigned. The correct docket information is


provided in the following table.


Corrected AD Docket Numbers


AD number
 
Original docket number
 
Corrected docket number


AD 2008-01-02
 
FAA-2008-0410
 
FAA-2007-0410


2004-07-22 R1
 
FAA-2008-0411
 
FAA-2007-0411


AD 90-25-05 R1
 
FAA-2008-0412
 
FAA-2007-0412