C1-2012-5859. Airworthiness Directives; Airbus Airplanes  

  • Start Preamble

    Correction

    In rule document 2012-5859 appearing on pages 14679-14681 in the issue of March 13, 2012, make the following correction:

    [Corrected]
    Start Amendment Part

    On page 14680, in § 39.13, in the third column, the table is corrected to read as set forth below:

    End Amendment Part

    Table 1—List of FWC Part Numbers Affected by This AD

    FWC Part Number
    350E017238484 (H1D1)
    350E016187171 (C5)
    350E017248685 (H1D2)
    350E017251414 (H1E1)
    350E017271616 (H1E2)
    350E018291818 (H1E3CJ)
    350E018301919 (H1E3P)
    350E018312020 (H1E3Q)
    350E053020202 (H2E2)
    350E053020303 (H2E3)
    350E053020404 (H2E4)
    350E053020606 (H2F2)
    350E053020707 (H2F3)
    350E053021010 (H2F3P)
    350E053020808 (H2F4)
    End Preamble

    [FR Doc. C1-2012-5859 Filed 3-23-12; 8:45 am]

    BILLING CODE 1505-01-D

Document Information

Comments Received:
0 Comments
Published:
03/26/2012
Department:
Federal Aviation Administration
Entry Type:
Rule
Document Number:
C1-2012-5859
Pages:
17327-17327 (1 pages)
Docket Numbers:
Docket No. FAA-2011-1087, Directorate Identifier 2011-NM-032-AD, Amendment 39-16967, AD 2012-04-11
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
c1-2012-5859.pdf
Supporting Documents:
» U.S. DOT/FAA- See Attachments
» U.S. DOT.FAA - See Attachments