Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes

[Federal Register Volume 70, Number 1 (Monday, January 3, 2005)]
[Rules and Regulations]
[Pages 10-11]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-28666]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2000-NM-409-AD; Amendment 39-13853; AD 2004-22-25]
RIN 2120-AA64


Airworthiness Directives; Boeing Model 767-200, -300, and -300F 
Series Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document corrects an error that appeared in airworthiness 
directive (AD) 2004-22-25, which was published in the Federal Register 
on November 9, 2004 (69 FR 64839). The error resulted in the incorrect 
reference to cable spacers. This AD is applicable to certain Boeing 
Model 767-200, -300, and -300F series airplanes. This AD requires a 
one-time inspection for discrepancies of all wire bundles, including 
certain power feeder cables, of the electrical system in the forward 
cargo compartment ceiling at certain stations; and corrective actions 
if necessary.

DATES: Effective December 14, 2004.

FOR FURTHER INFORMATION CONTACT: Elias Natsiopoulos, Aerospace 
Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft 
Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-
4056; telephone (425) 917-6478; fax (425) 917-6590.

SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2004-22-25, 
amendment 39-13853, applicable to certain Boeing Model 767-200, -300, 
and -300F series airplanes, was published in the Federal Register on 
November 9, 2004 (69 FR 64839). That AD requires a one-time inspection 
for discrepancies of all wire bundles, including certain power feeder 
cables, of the electrical system in the forward cargo compartment 
ceiling at certain stations; and corrective actions if necessary.
    As published, the third cell of paragraph (a)(2)(ii) of Table 1 of 
AD 2004-22-25 states, ``* * * install sleeving, lacing tape, cable 
spacers, and straps,'' in accordance with Boeing Alert Service Bulletin 
767-24A0128, Revision 3, dated June 24, 2004 (cited as the appropriate 
service information for accomplishing the required actions). We 
incorrectly specified ``cable spacers'' as part of the installation 
requirements if the clearance between the power feeder cables and cargo 
liner standoffs is less

[[Page 11]]

than 0.13 inch. The service bulletin does not describe procedures for 
installation of cable spacers in that area. Therefore, we have 
determined that ``cable spacers'' should be removed from the 
requirements of paragraph (a)(2)(ii) of Table 1 of that AD.
    Since no other part of the regulatory information has been changed, 
the final rule is not being republished in the Federal Register.
    The effective date of this AD remains December 14, 2004.


Sec.  39.13  [Corrected]

0
On page 64842, in Table 1, paragraph (a)(2)(ii) of AD 2004-22-25 is 
corrected to read as follows:
* * * * *

                       Table 1.--Clearance Between Wire Bundles and Cargo Liner Standoffs
----------------------------------------------------------------------------------------------------------------
   If the clearance between the--                          Is--                                 Then--
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(i) Wire bundles and cargo liner     0.25 inch or more..............................  No further action is
 standoffs.                                                                            required by this AD.
                                     Between 0.13 and 0.25 inch.....................  Install sleeving and
                                                                                       lacing tape.
                                     Less than 0.13 inch............................  Install sleeving, lacing
                                                                                       tape, cable spacers, and
                                                                                       straps.
(ii) Power feeder cables and cargo   0.13 inch or more..............................  No further action is
 liner standoffs.                                                                      required by this AD.
                                     less than 0.13 inch............................  Install sleeving, lacing
                                                                                       tape, and straps.
----------------------------------------------------------------------------------------------------------------

* * * * *

    Issued in Renton, Washington, on December 22, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 04-28666 Filed 12-30-04; 8:45 am]
BILLING CODE 4910-13-P

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