[Federal Register Volume 64, Number 33 (Friday, February 19, 1999)]
[Rules and Regulations]
[Page 8233]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 99-4017]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-ANE-14; Amendment 39-11017; AD 99-03-03]
RIN 2120-AA64
Airworthiness Directives; Allison Engine Company Model AE 3007A
and AE 3007A1/1 Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 99-03-03 applicable to Allison Engine Company Model AE 3007A
turbofan engines that was published in the Federal Register on January
29, 1999 (64 FR 4525). A full authority digital electronic control
(FADEC) assembly part number (P/N) in the compliance section is
incorrect. This document corrects that P/N. In all other respects, the
original document remains the same.
EFFECTIVE DATE: February 19, 1999.
FOR FURTHER INFORMATION CONTACT: Kyri Zaroyiannis, Aerospace Engineer,
Chicago Aircraft Certification Office, FAA, Small Airplane Directorate,
2300 East Devon Avenue, Des Plaines, IL 60018; telephone (847) 294-
7836, fax (847) 294-7834.
SUPPLEMENTARY INFORMATION: A final rule airworthiness directive
applicable to Allison Engine Company Model AE 3007A and AE 3007A1/1
turbofan engines, was published in the Federal Register on January 29,
1999 (64 FR 4525). The following correction is needed:
Sec. 39.13 [Corrected]
On page 4526, in the third column, in the Compliance Section, in
paragraph (c), in the sixth line, ``2306867'' is corrected to read
``23068670''.
Issued in Burlington, MA, on February 8, 1999.
David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 99-4017 Filed 2-18-99; 8:45 am]
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