72 FR 192 pgs. 56618-56619 - Airworthiness Directives; Rolls-Royce plc RB211 Trent 500 Series Turbofan Engines; Correction
Type: RULEVolume: 72Number: 192Pages: 56618 - 56619
Docket number: [Docket No. FAA-2007-27955; Directorate Identifier 2007-NE-15-AD; Amendment 39-15201; AD 2007-19-10]
FR document: [FR Doc. E7-19610 Filed 10-3-07; 8:45 am]
Agency: Transportation Department
Sub Agency: Federal Aviation Administration
Official PDF Version: PDF Version
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: Christopher.spinney@faa.gov ; telephone (781) 238-7175; fax (781) 238-7199.
Christopher Spinney, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; e-mail: Christopher.spinney@faa.gov ; telephone (781) 238-7175; fax (781) 238-7199.
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:
§ 39.13 [Corrected]
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".
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