Airworthiness Directives; Rolls-Royce Deutschland (RRD) (Formerly Rolls-Royce, plc) Tay 611-8, Tay 620-15, Tay 620-15/20, Tay 650-15, Tay 650-15/10, and Tay 651-54 Turbofan Engines; Correction

[Federal Register Volume 70, Number 16 (Wednesday, January 26, 2005)]
[Rules and Regulations]
[Page 3614]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-1392]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2004-NE-11-AD; Amendment 39-13922; AD 2004-26-10]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce Deutschland (RRD) (Formerly 
Rolls-Royce, plc) Tay 611-8, Tay 620-15, Tay 620-15/20, Tay 650-15, Tay 
650-15/10, and Tay 651-54 Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes corrections to Airworthiness Directive 
(AD) 2004-26-10. That AD applies to certain RRD Tay 611-8, Tay 620-15, 
Tay 620-15/20, Tay 650-15, Tay 650-15/10, and Tay 651-54 turbofan 
engines with ice-impact panels installed in the low pressure (LP) 
compressor case. That AD was published in the Federal Register on 
January 6, 2005 (70 FR 1172). This document corrects the same service 
bulletin paragraph number reference in 17 locations of the compliance 
section. This document also corrects an inspection limit and a service 
bulletin number in the compliance section. In all other respects, the 
original document remains the same.

EFFECTIVE DATE: Effective January 26, 2005.

FOR FURTHER INFORMATION CONTACT: Jason Yang, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-
7747; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule; request for comments AD, FR 
Doc. 05-40, that applies to certain RRD Tay 611-8, Tay 620-15, Tay 620-
15/20, Tay 650-15, Tay 650-15/10, and Tay 651-54 turbofan engines with 
ice-impact panels installed in the low pressure (LP) compressor case, 
was published in the Federal Register on January 6, 2005 (70 FR 1172). 
The following corrections are needed:


Sec.  39.13  [Corrected]

0
On page 1174, in the third column, in paragraph (f)(1), ``paragraph 
3.E.'' is corrected to read ``paragraphs 3.C. through 3.E''.
0
On page 1175, in the first column, in paragraphs (f)(2), (g)(1), 
(g)(2), (g)(3), (j)(1), and (j)(2), ``paragraph 3.E'' is corrected to 
read ``paragraphs 3.C. through 3.E'' in six locations.
0
On page 1175, in the second column, in paragraphs (k)(1), (k)(2), 
(k)(3), (n)(2), and (o)(1), ``paragraph 3.E'' is corrected to read 
``paragraphs 3.C. through 3.E'' in five locations.
0
On page 1175, in the third column, in paragraphs (o)(2), (p)(1), 
(p)(2), (p)(3), and (s)(2), ``paragraph 3.E'' is corrected to read 
``paragraphs 3.C. through 3.E'' in five locations.
0
On page 1175, in the third column, in paragraph (s)(1), ``3,000 CSLI'' 
is corrected to read ``3,000 hours-since-last-inspection''.
0
On page 1175, in the third column, in paragraph (s)(2), ``TAY-72-1638'' 
is corrected to read ``TAY-72-1639''.

    Issued in Burlington, MA, on January 19, 2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 05-1392 Filed 1-25-05; 8:45 am]
BILLING CODE 4910-13-P

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