[Federal Register Volume 68, Number 78 (Wednesday, April 23, 2003)]
[Rules and Regulations]
[Pages 19944-19945]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-9982]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-NE-48-AD; Amendment 39-13107; AD 2003-07-11]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG
Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
[[Page 19945]]
ACTION: Final rule; request for comments, correction.
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SUMMARY: This document makes corrections to Airworthiness Directive
(AD) 2003-07-11, applicable to Rolls-Royce Deutschland Ltd & Co KG
(formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH),
models BR700-710A1-10 and BR700-710A2-20 turbofan engines. AD 2003-07-
11 was published in the Federal Register on April 11, 2003 (68 FR
17727). In the compliance section, paragraph (g) incorrectly references
cycles and should reference hours, and the paragraph lettering sequence
after paragraph (g) is incorrect. This document corrects cycles to
hours and corrects the paragraph lettering sequence. In all other
respects, the original document remains the same.
EFFECTIVE DATE: April 28, 2003.
FOR FURTHER INFORMATION CONTACT: James Lawrence, Aerospace Engineer,
Engine Certification Office, FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803-5299; telephone (781)
238-7176; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: A final rule; request for comments
airworthiness directive FR DOC 03-8327, applicable to Rolls-Royce
Deutschland Ltd & Co KG models BR700-710A1-10 and BR700-710A2-20
turbofan engines, was published in the Federal Register on April 11,
2003 (68 FR 17727). The following correction is needed:
On page 17729, in the second column, under Repetitive Inspections
heading, paragraph (g), third line, which reads ``accumulating 500
cycles-since-the-last visual and ultrasonic inspections'' is corrected
to read ``accumulating 500 hours-since-the-last visual and ultrasonic
inspections''. Also, on page 17729, in the second column, under
Inspection Reporting Requirements heading, paragraph letter ``(g)'' is
corrected to read ``(h)'', under Alternative Methods of Compliance
heading, paragraph letter ``(h)'' is corrected to read ``(i)'', under
Special Flight Permits heading, paragraph ``(i)'' is corrected to read
``(j)'', under Documents That Have Been Incorporated by Reference
heading, paragraph ``(j)'' is corrected to read ``(k)'', and in the
third column, under Effective Date heading, paragraph ``(k)'' is
corrected to read ``(l)''.
Issued in Burlington, MA, on April 17, 2003.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 03-9982 Filed 4-22-03; 8:45 am]
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