Published 2007-10-04 · Federal Register document E7-19610
Airworthiness Directives; Rolls-Royce plc RB211 Trent 500 Series Turbofan Engines; Correction
Publication summary
The FAA is correcting airworthiness directive (AD) 2007-19-10. That AD applies to Rolls-Royce plc RB211 Trent 500 series turbofan engines. We published that AD in the Federal Register on September 18, 2007 (72 FR 53108). The compliance limit of 2,190 cycles-since-new is incorrect in two places. This document corrects that compliance limit to 2,910 cycles-since-new. In all other respects, the original document remains the same.
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- federal_register_ad_metadata_2007-daaa03e810180273
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- daaa03e81018027354d93b79e2a5f918dd4e1ce116086c5ab24f0dfd782528aa
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2007-19-10
- Effective date printed in this edition
- Unknown
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Official source · 2007-10-04
Publication text
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Read the complete official publication text
[Federal Register Volume 72, Number 192 (Thursday, October 4, 2007)]
[Rules and Regulations]
[Pages 56618-56619]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-19610]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27955; Directorate Identifier 2007-NE-15-AD;
Amendment 39-15201; AD 2007-19-10]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce plc RB211 Trent 500 Series
Turbofan Engines; Correction
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting airworthiness directive (AD) 2007-19-10.
That AD applies to Rolls-Royce plc RB211 Trent 500 series turbofan
engines. We published that AD in the Federal Register on September 18,
2007 (72 FR 53108). The compliance limit of 2,190 cycles-since-new is
incorrect in two places. This document corrects that compliance limit
to 2,910 cycles-since-new. In all other respects, the original document
remains the same.
DATES: Effective Date: Effective October 4, 2007.
FOR FURTHER INFORMATION CONTACT: Christopher Spinney, Aerospace
Engineer, Engine Certification Office, FAA, Engine and Propeller
Directorate, 12 New England Executive Park, Burlington, MA 01803; e-
mail: [email protected]; telephone (781) 238-7175; fax (781)
238-7199.
[[Page 56619]]
SUPPLEMENTARY INFORMATION: On September 18, 2007 (72 FR 53108), we
published a final rule AD, FR Doc. E7-18324, in the Federal Register.
That AD applies to Rolls-Royce plc RB211 Trent 500 series turbofan
engines. We need to make the following corrections:
Sec. 39.13 [Corrected]
0
On page 53109, in the second column, in the FAA's Determination and
Requirements of This AD paragraph, in the 22nd line, ``2,190 cycles-
since-new'' is corrected to read ``2,910 cycles-since-new''.
0
On page 53110, in the second column, in paragraph (e)(1), in the 7th
line, ``2,190 cycles-since-new'' is corrected to read ``2,910 cycles-
since-new''.
Issued in Burlington, Massachusetts, on September 28, 2007.
Francis A. Favara,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. E7-19610 Filed 10-3-07; 8:45 am]
BILLING CODE 4910-13-P
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