Rules and Regulations. Final rule; correction

Agency: Federal Aviation Administration, DOT
Action: Final rule; correction
Citation: FR Doc. 02-16175 · RIN 2120-AA64 · Docket No. 99-NE-49-AD; Amendment 39-12670; AD 2002-05-02 · 14 CFR 39

Summary

This document makes a correction to Airworthiness Directive (AD) 2002-05-02, applicable to General Electric Company (GE) CF34-3A1 and -3B1 series turbofan engines. AD 2002-05-02 was published in the ** Federal Register ** on March 8, 2002 (67 FR 10606). Information in the Mandatory Inspections Requirements Table is incorrect in two places. In all other respects, the original document remains the same. EFFECTIVE DATE: April 12, 2002.

Supplementary Information

A final rule airworthiness directive FR DOC. 02-5527, applicable to General Electric Company (GE) CF34-3A1 and -3B1 series turbofan engines, was published in the Federal Register on March 8, 2002 (67 FR 10606). The following correction is needed: § 39.13 [Corrected] On page 10608, in AD 2002-05-02, in Table 804 Mandatory Inspection Requirements, in the Part nomenclature column, fourth line, “HPT Rotor Outer Torque Coupling (all)” is corrected to read “HPT Rotor Outer Torque Coupling” and in the eleventh line, “Stage 3-8 Compressor Rotor Spool (all)”, in the Mandatory inspection column for that line, “All Areas (FPI)” is corrected to read “All Non-coated Areas (FPI)”. Issued in Burlington, MA, on June 17, 2002. Jay J. Pardee, Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 02-16175 Filed 6-26-02; 8:45 am]