Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes, 57221-57222 [05-19558]
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Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Proposed Rules
States, on the relationship between the
national Government and the States, or
on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that the proposed regulation:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this proposed AD and placed it in the
AD docket. See the ADDRESSES section
for a location to examine the regulatory
evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
came into contact with the blankets after the
light was inadvertently left on. We are
issuing this AD to prevent a possible
flammable condition, which could result in
smoke and fire in the forward crew rest area.
Compliance
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by removing amendment 39–11822 (65
FR 44672, July 19, 2000) and adding the
following new airworthiness directive
(AD):
McDonnell Douglas: Docket No. FAA–2005–
22557; Directorate Identifier 2005–NM–
147–AD.
Comments Due Date
(a) The FAA must receive comments on
this AD action by November 14, 2005.
BILLING CODE 4910–13–P
Restatement of the Requirements of AD
2000–14–12
Federal Aviation Administration
Applicability
(c) This AD applies to McDonnell Douglas
Model MD–11 and MD–11F airplanes,
certificated in any category, as identified
McDonnell Douglas Alert Service Bulletin
MD11–25A233, Revision 1, dated May 10,
2005.
Unsafe Condition
(d) This AD results from reports of burning
and smoldering blankets in the forward crew
rest area due to a reading light fixture that
VerDate Aug<31>2005
15:30 Sep 29, 2005
Jkt 205001
(f) For airplanes identified in McDonnell
Douglas Alert Service Bulletin MD11–
25A233, dated June 9, 1999: Within 6 months
after August 23, 2000 (the effective date of
AD 2000–14–12), replace the upper and
lower reading lights in the forward crew rest
area with a redesigned light fixture, in
accordance with McDonnell Douglas Alert
Service Bulletin MD11–25A233, dated June
9, 1999; or Revision 1, dated May 10, 2005.
After the effective date of this AD, do the
replacement in accordance with McDonnell
Douglas Alert Service Bulletin MD11–
25A233, Revision 1, dated May 10, 2005.
Note 1: McDonnell Douglas Alert Service
Bulletin MD11–25A233 refers to AIM
Aviation Service Incorporated Service
Bulletin AIM-MD11–25–2, Revision C, dated
March 8, 1999; and Revision D, dated March
16, 2005; as additional sources of service
information for replacing the upper and
lower reading lights in the forward crew rest
area.
New Requirements of This AD
(g) For all airplanes except those identified
in paragraph (f) of this AD: Within 6 months
after the effective date of this AD, do the
replacement specified in paragraph (f) of this
AD.
Parts Installation
(h) As of the effective date of this AD, no
person may install, on any airplane, a reading
lamp, part number (P/N) 2232, and light
fixture, P/N 0200500–001.
(i)(1) The Manager, Los Angeles Aircraft
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if
requested in accordance with the procedures
found in 14 CFR 39.19.
(2) Before using any AMOC approved in
accordance with 14 CFR 39.19 on any
airplane to which the AMOC applies, notify
the appropriate principal inspector in the
FAA Flight Standards Certificate Holding
District Office.
(3) AMOCs approved previously in
accordance with AD 2000–14–12,
amendment 39–11822, are approved as
AMOCs for the corresponding provisions of
this AD.
PO 00000
Frm 00016
DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
Replacement
Alternative Methods of Compliance (AMOCs)
Affected ADs
(b) This AD supersedes AD 2000–14–12.
Issued in Renton, Washington, on
September 21, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–19565 Filed 9–29–05; 8:45 am]
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
Replacement
§ 39.13
57221
Fmt 4702
Sfmt 4702
[Docket No. FAA–2005–22403; Directorate
Identifier 2005–NM–144–AD]
RIN 2120–AA64
Airworthiness Directives; Bombardier
Model DHC–8–400 Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM); correction.
AGENCY:
SUMMARY: The FAA is correcting a
typographical error in an NPRM that
was published in the Federal Register
on September 14, 2005 (70 FR 54316).
The error resulted in an incorrect
Docket No. The NPRM applies to certain
Bombardier Model DHC–8–400 series
airplanes. The NPRM would require an
inspection of the laminated shims for
cracks, damage, or extrusion between
the forward attachment fittings of the
horizontal stabilizer and the top rib of
the vertical stabilizer; a torque check of
the attachment bolts in the attachment
fittings of the front, middle, and rear
spars; and corrective actions if
necessary.
FOR FURTHER INFORMATION CONTACT:
George Duckett, Aerospace Engineer,
Airframe and Propulsion Branch, ANE–
171, FAA, New York Aircraft
Certification Office, 1600 Stewart
Avenue, suite 410, Westbury, New York
11590; telephone (516) 256–7525; fax
(516) 794–5531.
SUPPLEMENTARY INFORMATION: On
September 6, 2005, the FAA issued a
notice of proposed rulemaking (NPRM)
to amend 14 CFR part 39 to include an
AD that would apply to certain
Bombardier Model DHC–8–400 series
airplanes. That NPRM was published in
the Federal Register on September 14,
2005 (70 FR 54316). That NPRM
proposed to require an inspection of the
laminated shims for cracks, damage, or
extrusion between the forward
attachment fittings of the horizontal
stabilizer and the top rib of the vertical
stabilizer; a torque check of the
attachment bolts in the attachment
E:\FR\FM\30SEP1.SGM
30SEP1
57222
Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Proposed Rules
fittings of the front, middle, and rear
spars; and corrective actions if
necessary.
As published, that NPRM specifies an
incorrect Docket No. (i.e., FAA–2005–
20403) throughout preamble and the
regulatory text of the AD. The correct
Docket No. is FAA–2005–22403.
No other part of the regulatory
information has been changed;
therefore, the NPRM is not republished
in the Federal Register.
The last date for submitting comments
to the NPRM remains October 14, 2005.
§ 39.13
[Corrected]
In the Federal Register of September
14, 2005, on page 54318, in the first
column, paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES of
NPRM, Docket No. FAA–2005–22403,
Directorate Identifier 2005–NM–144–AD
is corrected to read as follows:
*
*
*
*
*
Bombardier, Inc. (Formerly de Havilland,
Inc.): Docket No. FAA–2005–22403;
Directorate Identifier 2005–NM–144–AD.
*
*
*
*
*
Issued in Renton, Washington, on
September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–19558 Filed 9–29–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22402; Directorate
Identifier 2005–NM–133–AD]
RIN 2120–AA64
Airworthiness Directives; Sabreliner
Model NA–265, NA–265–20, NA–265–
30, NA–265–40, NA–265–50, NA–265–
60, NA–265–65, NA–265–70, and NA–
265–80 Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM); correction.
AGENCY:
SUMMARY: The FAA is correcting a
typographical error in an NPRM that
was published in the Federal Register
on September 14, 2005 (70 FR 54318).
The error resulted in an incorrect
Docket No. The NPRM applies to certain
Sabreliner Model NA–265, NA–265–20,
NA–265–30, NA–265–40, NA–265–50,
NA–265–60, NA–265–65, NA–265–70,
and NA–265–80 series airplanes. The
VerDate Aug<31>2005
15:30 Sep 29, 2005
Jkt 205001
NPRM would require repetitive
inspections for discrepancies in the
front and rear spars of the wing in the
area of the wing center section, and in
the lugs on the rear spar and wing
trailing edge panel rib, and corrective
actions if necessary. The NPRM also
would require inspections for fuel leaks
of the front and rear spars of the wing,
and for discrepancies in the front and
rear spars of the wing in the area of the
wing center section, and in the lugs on
the rear spar and wing trailing edge
panel rib; and related investigative and
corrective actions, if necessary.
FOR FURTHER INFORMATION CONTACT: T.N.
Baktha, Aerospace Engineer, Airframe
Branch, ACE–118W, FAA, Wichita
Aircraft Certification Office, 1801
Airport Road, room 100, Mid-Continent
Airport, Wichita, Kansas 67209;
telephone (316) 946–4155; fax (316)
946–4407.
SUPPLEMENTARY INFORMATION: On
September 6, 2005, the FAA issued a
notice of proposed rulemaking (NPRM)
to amend 14 CFR part 39 to include an
AD that would apply to certain
Sabreliner Model NA–265, NA–265–20,
NA–265–30, NA–265–40, NA–265–50,
NA–265–60, NA–265–65, NA–265–70,
and NA–265–80 series airplanes. That
NPRM was published in the Federal
Register on September 14, 2005 (70 FR
54318). That NPRM proposed to require
repetitive inspections for discrepancies
in the front and rear spars of the wing
in the area of the wing center section,
and in the lugs on the rear spar and
wing trailing edge panel rib, and
corrective actions if necessary. That
NPRM also proposed to require
repetitive inspections for fuel leaks of
the front and rear spars of the wing, and
for discrepancies in the front and rear
spars of the wing in the area of the wing
center section, and in the lugs on the
rear spar and wing trailing edge panel
rib; and related investigative and
corrective actions, if necessary.
As published, that NPRM specifies an
incorrect Docket No. (i.e., FAA–2005–
20402) throughout preamble and the
regulatory text of the AD. The correct
Docket No. is FAA–2005–22402.
No other part of the regulatory
information has been changed;
therefore, the NPRM is not republished
in the Federal Register.
The last date for submitting comments
to the NPRM remains October 31, 2005.
§ 39.13
[Corrected]
In the Federal Register of September
14, 2005, on page 54320, in the third
column, paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES of
NPRM, Docket No. FAA–2005–22402,
PO 00000
Frm 00017
Fmt 4702
Sfmt 4702
Directorate Identifier 2005–NM–133–AD
is corrected to read as follows:
*
*
*
*
*
Sabreliner Corporation: Docket No. FAA–
2005–22402; Directorate Identifier 2005–
NM–133–AD.
*
*
*
*
*
Issued in Renton, Washington, on
September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–19557 Filed 9–29–05; 8:45 am]
BILLING CODE 4910–13–P
SOCIAL SECURITY ADMINISTRATION
20 CFR Part 411
RIN 0960–AF89
Amendments to the Ticket to Work and
Self-Sufficiency Program
Social Security Administration.
Notice of proposed rulemaking.
AGENCY:
ACTION:
SUMMARY: We are proposing to revise
our regulations for the Ticket to Work
and Self-Sufficiency Program (Ticket to
Work program), authorized by the
Ticket to Work and Work Incentives
Improvement Act of 1999. The Ticket to
Work program provides beneficiaries
with disabilities expanded options for
access to employment services,
vocational rehabilitation services, and
other support services. We are
proposing to make revisions to the
current rules to improve the overall
effectiveness of the program in assisting
beneficiaries to maximize their
economic self-sufficiency through work
opportunities. These revisions are based
on our vision of the future direction of
the Ticket to Work program, our
experience using the current rules, and
recommendations made by a number of
commenters on the program.
DATES: To be sure your comments are
considered, we must receive them by
December 29, 2005.
ADDRESSEES: You may give us your
comments by: using our Internet site
facility (i.e., Social Security Online) at
https://policy.ssa.gov/erm/
Rules+Open+To+Comment or the
Federal eRulemaking Portal: https://
www.regulations.gov; e-mail to
regulations@ssa.gov; by telefax to (410)
966–2830; or letter to the Commissioner
of Social Security, P.O. Box 17703,
Baltimore, MD 21235–7703. You may
also deliver them to the Office of
Regulations, Social Security
Administration, 107 Altmeyer Building,
6401 Security Boulevard, Baltimore, MD
21235–6401, between 8 a.m. and 4:30
E:\FR\FM\30SEP1.SGM
30SEP1
]]>Agencies
[Federal Register Volume 70, Number 189 (Friday, September 30, 2005)]
[Proposed Rules]
[Pages 57221-57222]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-19558]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22403; Directorate Identifier 2005-NM-144-AD]
RIN 2120-AA64
Airworthiness Directives; Bombardier Model DHC-8-400 Series
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM); correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting a typographical error in an NPRM that
was published in the Federal Register on September 14, 2005 (70 FR
54316). The error resulted in an incorrect Docket No. The NPRM applies
to certain Bombardier Model DHC-8-400 series airplanes. The NPRM would
require an inspection of the laminated shims for cracks, damage, or
extrusion between the forward attachment fittings of the horizontal
stabilizer and the top rib of the vertical stabilizer; a torque check
of the attachment bolts in the attachment fittings of the front,
middle, and rear spars; and corrective actions if necessary.
FOR FURTHER INFORMATION CONTACT: George Duckett, Aerospace Engineer,
Airframe and Propulsion Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, suite 410, Westbury, New
York 11590; telephone (516) 256-7525; fax (516) 794-5531.
SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued a
notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include
an AD that would apply to certain Bombardier Model DHC-8-400 series
airplanes. That NPRM was published in the Federal Register on September
14, 2005 (70 FR 54316). That NPRM proposed to require an inspection of
the laminated shims for cracks, damage, or extrusion between the
forward attachment fittings of the horizontal stabilizer and the top
rib of the vertical stabilizer; a torque check of the attachment bolts
in the attachment
[[Page 57222]]
fittings of the front, middle, and rear spars; and corrective actions
if necessary.
As published, that NPRM specifies an incorrect Docket No. (i.e.,
FAA-2005-20403) throughout preamble and the regulatory text of the AD.
The correct Docket No. is FAA-2005-22403.
No other part of the regulatory information has been changed;
therefore, the NPRM is not republished in the Federal Register.
The last date for submitting comments to the NPRM remains October
14, 2005.
Sec. 39.13 [Corrected]
In the Federal Register of September 14, 2005, on page 54318, in
the first column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES of
NPRM, Docket No. FAA-2005-22403, Directorate Identifier 2005-NM-144-AD
is corrected to read as follows:
* * * * *
Bombardier, Inc. (Formerly de Havilland, Inc.): Docket No. FAA-2005-
22403; Directorate Identifier 2005-NM-144-AD.
* * * * *
Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-19558 Filed 9-29-05; 8:45 am]
BILLING CODE 4910-13-P
