[Federal Register: December 14, 2004 (Volume 69, Number 239)]
[Rules and Regulations]
[Page 74412-74413]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr14de04-5]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2004-18579; Directorate Identifier 2004-CE-19-AD;
Amendment 39-13892; AD 2004-23-01]
RIN 2120-AA64
Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-7
Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2004-23-01, which was published in the Federal Register on
November 9, 2004 (69 FR 64832), and applies to certain Pilatus Aircraft
Ltd. (Pilatus) Model PC-7 airplanes with any Lear Romec RR53710B type
or Lear Romec RR53710K fuel booster pump (Pilatus part number
968.84.11.401; 968.84.11.403; or 968.84.11.404) installed. We
incorrectly referenced the amendment number as Amendment 39-13856. The
correct amendment number is Amendment 39-13892. This action corrects
the regulatory text.
DATES: The effective date of this AD remains December 27, 2004.
FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4059; facsimile: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Discussion
On September 8, 2004, FAA issued AD 2004-23-01, Amendment 39-13856
[[Page 74413]]
(69 FR 64832, November 9, 2004), which applies to certain Pilatus
Aircraft Ltd. (Pilatus) Model PC-7 airplanes with any Lear Romec
RR53710B type or Lear Romec RR53710K fuel booster pump (Pilatus part
number 968.84.11.401; 968.84.11.403; or 968.84.11.404) installed.
This AD requires you to check the airplane logbook to determine
whether any installed fuel booster pump has been modified with spiral
wrap to protect the wire leads and has the suffix letter ``B'' added to
the serial number of the fuel booster pump identification plate.
If any installed fuel booster pump has not been modified, you are
required to inspect any installed fuel booster pump wire lead for
defects; if defects are found, replace the fuel booster pump with a
modified fuel booster pump with spiral wrap that protects the wire
leads; or if no defects are found, install spiral wrap to protect any
wire leads and add the suffix letter ``B'' to the serial number of the
fuel booster pump identification plate.
The pilot is allowed to do the logbook check. If the pilot can
positively determine that the fuel booster pump wire leads with spiral
wrap are installed following the service information and that the
suffix letter ``B'' is included in the serial number of the fuel
booster pump identification plate, no further action is required.
Need for the Correction
The FAA incorrectly referenced the amendment number as Amendment
39-13856. The correct amendment number is Amendment 39-13892. This
correction is needed to ensure that the amendment number is correct and
to eliminate misunderstanding in the field.
Correction of Publication
Accordingly, the publication of November 9, 2004 (69 FR 64832), of
Amendment 39-13856; AD 2004-23-01, which was the subject of FR Doc. 04-
24717, is corrected as follows:
On page 64832, column 1, lines 18 and 19, replace Amendment 39-
13856 with Amendment 39-13892.
Sec. 39.13 [Corrected]
0
On page 64833, in Sec. 39.13 [Amended], revise the phrase ``Amendment
39-13856'' to read, ``Amendment 39-13892''.
0
Action is taken herein to correct this reference in AD 2004-23-01 and
to add this AD correction to Sec. 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
The effective date remains December 27, 2004.
Issued in Kansas City, Missouri, on December 8, 2004.
Sandra J. Campbell,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 04-27320 Filed 12-13-04; 8:45 am]
BILLING CODE 4910-13-P