03-31850. Airworthiness Directives; Titeflex Corporation; Correction  

  • Start Preamble

    AGENCY:

    Federal Aviation Administration, DOT.

    ACTION:

    Final rule; correction.

    SUMMARY:

    This document makes corrections to Airworthiness Directive (AD) 2003-23-05 applicable to certain Titeflex Corporation hoses installed on Boeing 737-300, -400, -500, -600, -700, -700C, -800, -900, 747-400, 757-200, -300, 767-200, -300, and -300F airplanes, that was published in the Federal Register on November 19, 2003 (68 FR 65157). The AD number is incorrect in the Preamble Section and in the Regulatory Section five corrections are needed in Table 1. This document corrects these errors. In all other respects, the original document remains the same.

    EFFECTIVE DATE:

    Effective December 30, 2003.

    Start Further Info

    FOR FURTHER INFORMATION CONTACT:

    Terry Fahr, Aerospace Engineer, Boston Aircraft Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7155; fax (781) 238-7199.

    End Further Info End Preamble Start Supplemental Information

    SUPPLEMENTARY INFORMATION:

    A final rule AD, FR Doc. 03-28730, applicable to certain Titeflex Corporation hoses installed on Boeing 737-300, -400, -500, -600, -700, -700C, -800, -900, 747-400, 757-200, -300, 767-200, -300, and -300F airplanes, was published in the Federal Register on November 19, 2003 (68 FR 65157). The following corrections are needed:

    [Corrected]
    Start Amendment Part

    On page 65157, in the first column, in the Preamble Section, in the fifth line, “39-13369; AD 2003-23-05-AD “ is corrected to read “39-13369; AD 2003-23-05”. Also, on page 65158, in Table 1, the following changes are made:

    End Amendment Part Start Amendment Part

    In the fifth column, for item (2) 737-600, -700, -700C, -800, and -900 airplanes, first line, “737-26A1109, Revision 12, dated May 8, 2003” is corrected to read “737-26A1109, Revision 2, dated May 8, 2003”.

    End Amendment Part Start Amendment Part

    In the second column, for item (3) 747-400 airplanes, “BACH5R0186XX” is corrected to read “BACH5S0186XX” and “BACH5S0080YY” is deleted.

    End Amendment Part Start Amendment Part

    In the second column, for item (4) 757-200 airplanes, under BACH5S0110XN, add “No number” and add in the third column on the same line, “109422”.

    End Amendment Part Start Amendment Part

    Also, on page 65159, in Table 1, in the second column, for item (5) 757-300 Start Printed Page 75116airplanes, under BACH5S0074XN, add: “Optional 453N2240-33”

    End Amendment Part Start Signature

    Issued in Burlington, MA, on December 19, 2003.

    Peter A. White,

    Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service.

    End Signature End Supplemental Information

    [FR Doc. 03-31850 Filed 12-29-03; 8:45 am]

    BILLING CODE 4910-13-P

Document Information

Effective Date:
12/30/2003
Published:
12/30/2003
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; correction.
Document Number:
03-31850
Dates:
Effective December 30, 2003.
Pages:
75115-75116 (2 pages)
Docket Numbers:
Docket No. 2002-NE-22-AD, Amendment 39-13369, AD 2003-23-05
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
03-31850.pdf