77 FR 58 pg. 17327 - Airworthiness Directives; Airbus Airplanes
Type: RULEVolume: 77Number: 58Page: 17327
Docket number: [Docket No. FAA-2011-1087; Directorate Identifier 2011-NM-032-AD; Amendment 39-16967; AD 2012-04-11]
FR document: [FR Doc. C1-2012-5859 Filed 3-23-12; 8:45 am]
Agency: Transportation Department
Sub Agency: Federal Aviation Administration
Official PDF Version: PDF Version
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-1087; Directorate Identifier 2011-NM-032-AD; Amendment 39-16967; AD 2012-04-11]
RIN 2120-AA64
Airworthiness Directives; Airbus Airplanes
Correction
In rule document 2012-5859 appearing on pages 14679-14681 in the issue of March 13, 2012, make the following correction:
§ 39.13 [Corrected]
On page 14680, in § 39.13, in the third column, the table is corrected to read as set forth below:
| 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) |
[FR Doc. C1-2012-5859 Filed 3-23-12; 8:45 am]
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