[Federal Register: August 19, 2003 (Volume 68, Number 160)]
[Rules and Regulations]
[Page 49686]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr19au03-2]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NE-34-AD; Amendment 39-13257; AD 2003-16-04]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney Canada Turboprop
Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2003-16-04 that applies to Pratt & Whitney Canada (PWC) engine
models PW118, PW118A, PW118B, PW119B, PW119C, PW120, PW120A, PW121,
PW121A, PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B, PW125B,
PW126, PW126A, PW127, PW127B, PW127E, PW127F, PW127G, PW127H, and
PW127J turboprop engines that was published in the Federal Register on
August 6, 2003. Certain engine models were incorrectly included in the
preamble section, under Summary and Supplementary Information, and in
the regulatory section under Applicability. In addition, airplanes on
which these engines are installed were incorrectly included in the
regulatory section, under Applicability. This document corrects these
items. In all other respects, the original document remains the same.
EFFECTIVE DATE: Effective August 6, 2003.
FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-
7178; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc 03-19840, that
applies to Pratt & Whitney Canada (PWC) engine models PW118, PW118A,
PW118B, PW119B, PW119C, PW120, PW120A, PW121, PW121A, PW123, PW123B,
PW123C, PW123D, PW123E, PW123AF, PW124B, PW125B, PW126, PW126A, PW127,
PW127B, PW127E, PW127F, PW127G, PW127H, and PW127J turboprop engines,
was published in the Federal Register on August 6, 2003 (68 FR 46441).
The following corrections are needed:
On page 46441, in the third column, in the preamble section, under
SUMMARY, in the first paragraph, in the first, second, third, and
fourth lines, ``PW123AF, PW124B, PW125B, PW126, PW126A, PW127, PW127B,
PW127E, PW127F, PW127G, PW127H, and PW127J turboprop engines'' is
corrected to read `` PW123AF, PW124B, PW125B, PW126A, PW127, PW127E,
PW127F, and PW127G turboprop engines''.
On page 46441, in the third column, in the preamble section, under
SUPPLEMENTARY INFORMATION, in the first paragraph, in the ninth, tenth,
eleventh, and twelfth lines, ``PW123AF, PW124B, PW125B, PW126, PW126A,
PW127, PW127B, PW127E, PW127F, PW127G, PW127H, and PW127J turboprop
engines'' is corrected to read `` PW123AF, PW124B, PW125B, PW126A,
PW127, PW127E, PW127F, and PW127G turboprop engines''.
Sec. 39.13 [Corrected]
0
On page 46442, in the third column, in the regulatory section, under
Applicability, in the first paragraph, in the seventh, eighth, and
ninth lines, ``PW125B, PW126, PW126A, PW127, PW127B, PW127E, PW127F,
PW127G, PW127H, and PW127J turboprop engines.'' is corrected to read
``PW125B, PW126A, PW127, PW127E, PW127F, and PW127G turboprop
engines.''.
0
On page 46442, in the third column, in the regulatory section, under
Applicability, in the first paragraph, in the sixteenth, seventeenth,
and eighteenth lines, ``EMB-120; Fairchild Dornier 328, Fokker 50 and
60; Ilyushin IL-114-100; BAE Systems (Operations) Ltd. ATP; and XIAN
MA-60.'' is corrected to read ``EMB-120; Fairchild Dornier 328, Fokker
50; and BAE Sysems (Operations) Ltd. ATP.''.
Issued in Burlington, MA, on August 13, 2003.
Marc J. Bouthillier,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 03-21153 Filed 8-18-03; 8:45 am]
BILLING CODE 4910-13-P