Airworthiness Directives; General Electric Company GE90 Series Turbofan Engines; Correction

---
identifier: "/us/fr/02-10273"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; General Electric Company GE90 Series Turbofan Engines; Correction"
title_number: 0
title_name: "Federal Register"
section_number: "02-10273"
section_name: "Airworthiness Directives; General Electric Company GE90 Series Turbofan Engines; Correction"
positive_law: false
currency: "2002-04-29"
last_updated: "2002-04-29"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "02-10273"
document_type: "rule"
publication_date: "2002-04-29"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "67 FR 20890"
fr_volume: 67
docket_ids:
  - "Docket No. 98-ANE-39-AD"
  - "Amendment 39-12668"
  - "AD 2002-04-11"
fr_action: "Final rule; correction."
---


#  [Corrected]

**AGENCY:**

Federal Aviation Administration, DOT.

**ACTION:**

Final rule; correction.

**SUMMARY:**

This document makes a correction to Airworthiness Directive (AD) 2002-04-11 applicable to General Electric Company GE90 series turbofan engines that was published in the *Federal Register* on March 4, 2002 (67 FR 9582). The Table in the regulatory text section is incorrect. This document corrects that Table. In all other respects, the original document remains the same.

**EFFECTIVE DATE:**

April 8, 2002.

**FOR FURTHER INFORMATION CONTACT:**

Ian Dargin, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7178, fax (781) 238-7199.

**SUPPLEMENTARY INFORMATION:**

A final rule airworthiness directive (FR Doc. 02-5003) applicable to General Electric Company GE90 series turbofan engines, was published in the *Federal Register* on March 4, 2002 (67 FR 9582). The following corrections are needed:

§ 39.13

1. On page 9583, in the third column entitled, Inspect per engine manual chapter, in the third entry, (HPCR, Disk, Stage 7) “72-31-07-200-001-001 Fluorescent Penetrant Inspection (subtask 72-31-07-230-051), and 72-31-07-200-001-001 Eddy Current Inspection (subtask 72-31-07-250-051 or 72-31-07-230-052 or 72-31-07-230-053” is corrected to read “72-31-07-200-001-001 Fluorescent Penetrant Inspection (subtask 72-31-07-230-051), and 72-31-07-200-001-001 Eddy Current Inspection of the Rim Boltholes (subtask 72-31-07-250-051 or 72-31-07-250-052 or 72-31-07-250-053”.

2. On the same page, in the same column entitled, Inspect per engine manual chapter, in the nineth entry, (HPTR Disk, Stage 1) “72-53-02-200-001-002 Fluorescent Penetrant Inspection (subtask 72-53-02-160-051), and 72-53-02-200-001-002 Eddy Current Inspection of the Bore “ is corrected to read “72-53-02-200-001-002 Fluorescent Penetrant Inspection (subtask 72-53-02-230-052), and 72-53-02-200-001-002 Eddy Current Inspection of the Bore”.

Issued in Burlington, MA, on April 18, 2002.

Francis A. Favara,

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