Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes, 28250 [06-4424]
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28250
Federal Register / Vol. 71, No. 94 / Tuesday, May 16, 2006 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Need for the Correction
[Docket No. FAA–2005–21275; Directorate
Identifier 2005–CE–28–AD; Amendment 39–
14515; AD 2006–01–11 R1]
RIN 2120–AA64
Airworthiness Directives; The Cessna
Aircraft Company Models 208 and
208B Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
cprice-sewell on PROD1PC66 with RULES
SUMMARY: This document makes a
correction to Airworthiness Directive
(AD) 2006–01–11 R1, which published
in the Federal Register on March 16,
2006 (71 FR 13538), and applies to all
The Cessna Aircraft Company (Cessna)
Models 208 and 208B airplanes. AD
2006–01–11 R1 requires the installation
of a pilot assist handle and deicing
boots on the cargo pod and landing gear
fairings; and the incorporation of
changes to the Pilot’s Operating
Handbook (POH) and FAA-approved
Airplane Flight Manual (AFM). Current
language in paragraph (e)(4) of AD
2006–01–11 R1 regarding the placard
requirement inadvertently states: ‘‘You
may insert a copy of this AD into the
appropriate sections of the POH to
comply with this action.’’ This does not
meet the intent of the AD. This
document corrects that paragraph by
removing the language referenced
above.
DATES: The effective date of this AD
(2006–01–11 R1) remains February 22,
2006.
FOR FURTHER INFORMATION CONTACT:
Robert P. Busto, Aerospace Engineer,
Wichita Aircraft Certification Office,
FAA, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946–
4157; facsimile: (316) 946–4107.
SUPPLEMENTARY INFORMATION:
Discussion
On March 10, 2006, the FAA issued
AD 2006–01–11 R1, Amendment 39–
14515 (71 FR 13538, March 16, 2006),
which applies to all Cessna Models 208
and 208B airplanes. AD 2006–01–11 R1
requires the installation of a pilot assist
handle and deicing boots on the cargo
pod and landing gear fairings; and the
incorporation of changes to the Pilot’s
Operating Handbook (POH) and FAAapproved Airplane Flight Manual
(AFM). Current language in paragraph
(e)(4) of AD 2006–01–11 R1 regarding
the placard requirement inadvertently
VerDate Aug<31>2005
15:11 May 15, 2006
states: ‘‘You may insert a copy of this
AD into the appropriate sections of the
POH to comply with this action.’’ This
does not meet the intent of the AD.
Jkt 208001
This correction is needed to not allow
a method of compliance that was
inadvertently included in the AD and
does not address the unsafe condition.
Correction of Publication
Accordingly, the publication of March
16, 2006 (71 FR 13538), of Amendment
39–14515; AD 2006–01–11 R1, which
was the subject of FR Doc. 06–2546, is
corrected as follows:
I
§ 39.13
[Corrected]
On page 13540, in § 39.13 [Amended],
in paragraph (e)(4), in the Procedures
column, remove the following text:
‘‘You may insert a copy of this AD into the
appropriate sections of the POH to comply
with this action.’’
Action is taken herein to correct this
reference in AD 2006–01–11 R1 and to
add this AD correction to § 39.13 of the
Federal Aviation Regulations (14 CFR
39.13).
The effective date remains February
22, 2006.
Issued in Kansas City, Missouri, on May 5,
2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 06–4424 Filed 5–15–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2004–19982; Directorate
Identifier 2004–NM–142–AD; Amendment
39–14597; AD 2006–10–13]
RIN 2120–AA64
Airworthiness Directives; Airbus Model
A330–223, –321, –322, and –323
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
Airbus Model A330–223, –321, –322,
and –323 airplanes. This AD requires
repetitive inspections of the firewall of
the lower aft pylon fairing (LAPF), and
corrective actions if necessary. This AD
also provides an optional terminating
PO 00000
Frm 00022
Fmt 4700
Sfmt 4700
action for the repetitive inspections.
This AD results from reports of cracking
of the LAPF firewall. We are issuing this
AD to detect and correct this cracking,
which could reduce the effectiveness of
the firewall and result in an
uncontrolled engine fire.
DATES: This AD becomes effective June
20, 2006.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of June 20, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, room PL–401,
Washington, DC.
Contact Airbus, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France,
for service information identified in this
AD.
FOR FURTHER INFORMATION CONTACT: Tim
Backman, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2797;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness
directive (AD) docket on the Internet at
https://dms.dot.gov or in person at the
Docket Management Facility office
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The Docket Management Facility office
(telephone (800) 647–5227) is located on
the plaza level of the Nassif Building at
the street address stated in the
ADDRESSES section.
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to all Airbus Model A330–223,
–321, –322, and –323 airplanes. That
NPRM was published in the Federal
Register on January 4, 2005 (70 FR 317).
That NPRM proposed to require
repetitive inspections of the firewall of
the lower aft pylon fairing (LAPF), and
corrective actions if necessary.
Explanation of New Relevant Service
Information
Since we issued the NRPM, Airbus
has issued Service Bulletin A330–54–
3022, dated May 25, 2005. That service
bulletin describes procedures for
replacing the existing LAPF assemblies
with improved parts. Doing this
replacement eliminates the need for the
E:\FR\FM\16MYR1.SGM
16MYR1
]]>Agencies
[Federal Register Volume 71, Number 94 (Tuesday, May 16, 2006)]
[Rules and Regulations]
[Page 28250]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-4424]
[[Page 28250]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21275; Directorate Identifier 2005-CE-28-AD;
Amendment 39-14515; AD 2006-01-11 R1]
RIN 2120-AA64
Airworthiness Directives; The Cessna Aircraft Company Models 208
and 208B Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2006-01-11 R1, which published in the Federal Register on March
16, 2006 (71 FR 13538), and applies to all The Cessna Aircraft Company
(Cessna) Models 208 and 208B airplanes. AD 2006-01-11 R1 requires the
installation of a pilot assist handle and deicing boots on the cargo
pod and landing gear fairings; and the incorporation of changes to the
Pilot's Operating Handbook (POH) and FAA-approved Airplane Flight
Manual (AFM). Current language in paragraph (e)(4) of AD 2006-01-11 R1
regarding the placard requirement inadvertently states: ``You may
insert a copy of this AD into the appropriate sections of the POH to
comply with this action.'' This does not meet the intent of the AD.
This document corrects that paragraph by removing the language
referenced above.
DATES: The effective date of this AD (2006-01-11 R1) remains February
22, 2006.
FOR FURTHER INFORMATION CONTACT: Robert P. Busto, Aerospace Engineer,
Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946-4157; facsimile: (316) 946-4107.
SUPPLEMENTARY INFORMATION:
Discussion
On March 10, 2006, the FAA issued AD 2006-01-11 R1, Amendment 39-
14515 (71 FR 13538, March 16, 2006), which applies to all Cessna Models
208 and 208B airplanes. AD 2006-01-11 R1 requires the installation of a
pilot assist handle and deicing boots on the cargo pod and landing gear
fairings; and the incorporation of changes to the Pilot's Operating
Handbook (POH) and FAA-approved Airplane Flight Manual (AFM). Current
language in paragraph (e)(4) of AD 2006-01-11 R1 regarding the placard
requirement inadvertently states: ``You may insert a copy of this AD
into the appropriate sections of the POH to comply with this action.''
This does not meet the intent of the AD.
Need for the Correction
This correction is needed to not allow a method of compliance that
was inadvertently included in the AD and does not address the unsafe
condition.
Correction of Publication
0
Accordingly, the publication of March 16, 2006 (71 FR 13538), of
Amendment 39-14515; AD 2006-01-11 R1, which was the subject of FR Doc.
06-2546, is corrected as follows:
Sec. 39.13 [Corrected]
On page 13540, in Sec. 39.13 [Amended], in paragraph (e)(4), in
the Procedures column, remove the following text:
``You may insert a copy of this AD into the appropriate sections
of the POH to comply with this action.''
Action is taken herein to correct this reference in AD 2006-01-11
R1 and to add this AD correction to Sec. 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
The effective date remains February 22, 2006.
Issued in Kansas City, Missouri, on May 5, 2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 06-4424 Filed 5-15-06; 8:45 am]
BILLING CODE 4910-13-P
