AD 2003-16-04

[Federal Register Volume 68, Number 160 (Tuesday, August 19, 2003)]
[Rules and Regulations]
[Page 49686]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 03-21153]


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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.

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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