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Start Preamble
AGENCY:
Federal Aviation Administration, DOT.
ACTION:
Final rule; correction.
SUMMARY:
This document makes a correction to Airworthiness Directive (AD) 2003-19-15, applicable to Pratt & Whitney PW4000 series turbofan engines. AD 2003-19-15 was published in the Federal Register on September 30, 2003 (68 FR 56143). In the amendatory language, under § 39.13 [Amended], the amendment number of the new action was inadvertently omitted. This document corrects that omission. In all other respects, the original document remains the same.
EFFECTIVE DATE:
October 9, 2003.
Start Further InfoFOR FURTHER INFORMATION CONTACT:
Diane Cook, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7133; fax (781) 238-7199.
End Further Info End Preamble Start Supplemental InformationSUPPLEMENTARY INFORMATION:
A final rule airworthiness directive, FR Doc. 03-24486, applicable to Pratt & Whitney PW4000 series turbofan engines, was published in the Federal Register on September 30, 2003 (68 FR 56143). The following correction is needed:
Start Amendment PartOn page 56145, in the second column, under § 39.13 [Amended], in the sixth line, add “Amendment 39-13318.” after “Pratt & Whitney:”.
End Amendment Part Start SignatureIssued in Burlington, MA, on October 3, 2003.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification Service.
[FR Doc. 03-25577 Filed 10-8-03; 8:45 am]
BILLING CODE 4910-13-P
Document Information
- Effective Date:
- 10/9/2003
- Published:
- 10/09/2003
- Department:
- Federal Aviation Administration
- Entry Type:
- Rule
- Action:
- Final rule; correction.
- Document Number:
- 03-25577
- Dates:
- October 9, 2003.
- Pages:
- 58273-58273 (1 pages)
- Docket Numbers:
- Docket No. 2000-NE-47-AD, Amendment 39-13318, AD 2003-19-15
- RINs:
- 2120-AA64: Airworthiness Directives
- RIN Links:
- https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
- PDF File:
- 03-25577.pdf
- CFR: (1)
- 14 CFR 39