Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes, 57221-57222 [05-19558]

Download as PDF 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 http://policy.ssa.gov/erm/ Rules+Open+To+Comment or the Federal eRulemaking Portal: http:// 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]


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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