Airworthiness Directives; Airbus Airplanes

---
identifier: "/us/fr/C1-2012-5859"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; Airbus Airplanes"
title_number: 0
title_name: "Federal Register"
section_number: "C1-2012-5859"
section_name: "Airworthiness Directives; Airbus Airplanes"
positive_law: false
currency: "2012-03-26"
last_updated: "2012-03-26"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "C1-2012-5859"
document_type: "rule"
publication_date: "2012-03-26"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "77 FR 17327"
fr_volume: 77
docket_ids:
  - "Docket No. FAA-2011-1087"
  - "Directorate Identifier 2011-NM-032-AD"
  - "Amendment 39-16967"
  - "AD 2012-04-11"
---


#  [Corrected]

**Correction**

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

**14 CFR Part 39**

§ 39.13

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

|  |
| --- |
|  |
| 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) |