[Federal Register Volume 67, Number 44 (Wednesday, March 6, 2002)]
[Rules and Regulations]
[Page 10099]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-5260]



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  Federal Register / Vol. 67, No. 44 / Wednesday, March 6, 2002 / Rules 
and Regulations  

[[Page 10099]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-ANE-66; Amendment 39-12649; AD 2002-03-08]
RIN 2120-AA64


Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan 
Engines, Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule, correction.

-----------------------------------------------------------------------

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2002-03-08, applicable to Pratt & Whitney (PW) PW4000 series 
turbofan engines, that was published in the Federal Register on 
February 15, 2002 (67 FR 7061). An engine model number was 
inadvertently omitted from the regulatory information. This document 
corrects that omission. In all other respects, the original document 
remains the same.

EFFECTIVE DATE: April 16, 2002.

FOR FURTHER INFORMATION CONTACT: Robert McCabe, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803-5299; telephone (781) 
238-7138, fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD applicable to Pratt & 
Whitney (PW) Model PW4050, PW4052, PW4056, PW4060, PW4060A, PW4060C, 
PW4062, PW4152, PW4156, PW4156A, PW4158, PW4160, PW4460, PW4462, 
PW4650, PW4164, PW4168, PW4168A, PW4074, PW4074D, PW4077, PW4077D, 
PW4084, PW4084D, PW4090, PW4090D, and PW4098 turbofan engines, 
installed on but not limited to Airbus A300, A310, and A330 series, 
Boeing 747, 767, and 777 series, and McDonnell Douglas MD-11 series 
airplanes was published in the Federal Register on February 15, 2002 
(67 FR 7061). This AD superseded an AD that applied to the PW4090-3 
model as well. The PW4090-3 model was included in the Notice of 
Proposed Rulemaking and inadvertently left out of the final rule. The 
following correction is needed:


Sec. 39.13  [Corrected]

    On page 7062, in the Regulatory Information, in the sixth line of 
the third column, the engine model applicability is corrected to read 
``PW4090, PW4090-3, PW4090D, and PW4098 turbofan.'' Also, on page 7062, 
in the Regulatory Information, in the third column, the thirteenth line 
of paragraph (a) is corrected to read ``PW4090-3, PW4090D, and PW4098 
series turbofan.''

    Issued in Burlington, MA, on February 25, 2002.
Thomas A. Boudreau,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 02-5260 Filed 3-5-02; 8:45 am]
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