Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes, 16994 [06-3252]
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16994
Federal Register / Vol. 71, No. 65 / Wednesday, April 5, 2006 / Rules and Regulations
Adoption of the Amendment
Under the authority delegated to me
by the Administrator, the Federal
Aviation Administration amends part 39
of the Federal Aviation Regulations (14
CFR part 39) as follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
Federal Aviation Administration
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
I
2006–07–20 Turbomeca: Amendment 39–
14547. Docket No. FAA–2006–24239;
Directorate Identifier 2006–NE–09–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective May 5, 2006.
Unsafe Condition
(d) This AD results from Turbomeca
determining that Makila 1 A2 turboshaft
engines with software version 9 installed in
the digital electronic control unit (DECU),
under certain conditions, could experience a
free turbine overspeed and uncontained
failure. We are issuing this AD to prevent
overspeed and uncontained failure of the free
turbine and damage to the helicopter.
Compliance
(e) You are responsible for having the
actions required by this AD performed no
later than November 30, 2008, unless the
actions have already been done.
(f) Upgrade the software version in the
DECU from version 9 (TU 230C) to version
11 (TU 244C). Information on this upgrade
can be found in Turbomeca Mandatory
Service Bulletin No. 298 73 0244, dated
February 2, 2006.
(g) Version 11 (TU 244C) software must not
be intermixed on the helicopter with any
other DECU software version except version
9 (TU 230C).
rwilkins on PROD1PC63 with RULES
Alternative Methods of Compliance
(h) The Manager, Engine Certification
Office, has the authority to approve
alternative methods of compliance for this
AD if requested using the procedures found
in 14 CFR 39.19.
Related Information
(i) Direction Generale De L’Aviation Civile
airworthiness directive F–2006–029, dated
February 1, 2006, also addresses the subject
of this AD.
Jkt 208001
RIN 2120–AA64
Airworthiness Directives; The Cessna
Aircraft Company Models 208 and
208B Airplanes
SUMMARY: This document makes a
correction to Airworthiness Directive
(AD) 2006–06–06, which published in
the Federal Register on March 16, 2006
(71 FR 13533), and applies to all The
Cessna Aircraft Company (Cessna)
Models 208 and 208B airplanes. AD
2006–06–06 requires you to incorporate
information into the applicable section
of the Airplane Flight Manual (AFM)
and Pilots Operating Handbook (POH)
and requires installation of placards.
Current language in paragraph (f)(3) of
AD 2006–06–06 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.
The effective date of this AD
(2006–06–06) remains March 24, 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:
DATES:
Discussion
On March 10, 2006, the FAA issued
AD 2006–06–06, Amendment 39–14514
(71 FR 13533, March 16, 2006), which
applies to all Cessna Models 208 and
208B airplanes. AD 2006–06–06
requires you to incorporate information
into the applicable section of the AFM
and POH and requires installation of
PO 00000
Frm 00022
Fmt 4700
placards. Current language in paragraph
(f)(3) of AD 2006–06–06 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
[Docket No. FAA–2006–23648; Directorate
Identifier 2006–CE–07–AD; Amendment 39–
14514; AD 2006–06–06]
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
Applicability
(c) This AD applies to Turbomeca Makila
1 A2 turboshaft engines. These engines are
installed on, but not limited to, Eurocopter
AS 332 L2 helicopters.
16:22 Apr 04, 2006
14 CFR Part 39
AGENCY:
Affected ADs
(b) None.
VerDate Aug<31>2005
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
1. The authority citation for part 39
continues to read as follows:
I
§ 39.13
Issued in Burlington, Massachusetts, on
March 30, 2006.
Peter A. White,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 06–3253 Filed 4–4–06; 8:45 am]
Sfmt 4700
Accordingly, the publication of March
16, 2006 (71 FR 13533), of Amendment
39–14514; AD 2006–06–06, which was
the subject of FR Doc. 06–2544, is
corrected as follows:
I
§ 39.13
[Corrected]
On page 13536, in § 39.13 [Amended],
in paragraph (f)(3), 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 2006–06–06 and to add
this AD correction to § 39.13 of the
Federal Aviation Regulations (14 CFR
39.13).
The effective date remains March 24,
2006.
Issued in Kansas City, Missouri, on March
30, 2006.
David R. Showers,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 06–3252 Filed 4–4–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2005–22687; Airspace
Docket No. 05–AAL–23]
Establishment of Class E Airspace; St.
Paul Island, AK
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: This action revises Class E
airspace at St. Paul Island, AK to
provide adequate controlled airspace to
contain aircraft executing one new
Standard Instrument Approach
Procedure (SIAP), and five revised
SIAPs. This rule results in revised Class
E airspace extending upward from 700
feet (ft.) and 1,200 ft. above the surface
at St. Paul Island, AK.
E:\FR\FM\05APR1.SGM
05APR1
]]>Agencies
[Federal Register Volume 71, Number 65 (Wednesday, April 5, 2006)]
[Rules and Regulations]
[Page 16994]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-3252]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-23648; Directorate Identifier 2006-CE-07-AD;
Amendment 39-14514; AD 2006-06-06]
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) 2006-06-06, which published in the Federal Register on March 16,
2006 (71 FR 13533), and applies to all The Cessna Aircraft Company
(Cessna) Models 208 and 208B airplanes. AD 2006-06-06 requires you to
incorporate information into the applicable section of the Airplane
Flight Manual (AFM) and Pilots Operating Handbook (POH) and requires
installation of placards. Current language in paragraph (f)(3) of AD
2006-06-06 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 (2006-06-06) remains March 24,
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 2006-06-06, Amendment 39-14514
(71 FR 13533, March 16, 2006), which applies to all Cessna Models 208
and 208B airplanes. AD 2006-06-06 requires you to incorporate
information into the applicable section of the AFM and POH and requires
installation of placards. Current language in paragraph (f)(3) of AD
2006-06-06 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 13533), of
Amendment 39-14514; AD 2006-06-06, which was the subject of FR Doc. 06-
2544, is corrected as follows:
Sec. 39.13 [Corrected]
On page 13536, in Sec. 39.13 [Amended], in paragraph (f)(3), 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 2006-06-06
and to add this AD correction to Sec. 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
The effective date remains March 24, 2006.
Issued in Kansas City, Missouri, on March 30, 2006.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-3252 Filed 4-4-06; 8:45 am]
BILLING CODE 4910-13-P
