Airworthiness Directives; Gulfstream Model GV-SP Series Airplanes, 18253-18254 [E6-5253]

Download as PDF Federal Register / Vol. 71, No. 69 / Tuesday, April 11, 2006 / Proposed Rules 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. § 39.13 [Amended] 2. The Federal Aviation Administration (FAA) amends § 39.13 by removing amendment 39–14396 (70 FR 72595, December 6, 2005) and adding the following new airworthiness directive (AD): Boeing: Docket No. FAA–2006–24369; Directorate Identifier 2006–NM–001–AD. Comments Due Date (a) The FAA must receive comments on this AD action by May 26, 2006. Affected ADs (b) This AD supersedes AD 2005–25–03. Applicability (c) This AD applies to Boeing Model 737– 600, –700, –700C, and –800 series airplanes, certificated in any category; as identified in Boeing Alert Service Bulletin (ASB) 737– 53A1222, Revision 2, dated October 20, 2005. Unsafe Condition (d) This AD results from full-scale fuselage fatigue testing on a splice fitting that failed prior to the design objective on Boeing Model 737–800 series airplanes, and a report of a cracked splice fitting on an operational airplane. We are issuing this AD to prevent cracking of the existing fitting, which may result in cracking through the skin and consequent decompression of the flight cabin. Compliance (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. hsrobinson on PROD1PC70 with PROPOSALS Restatement of Certain Requirements of AD 2005–25–03 Replacing the Splice Fittings (f) Replace the splice fittings with new splice fittings in accordance with the Accomplishment Instructions of Boeing ASB 737–53A1222, Revision 2, dated October 20, 2005, at the times specified in paragraph (f)(1) or (f)(2) of this AD, as applicable. Before further flight, do any related investigative actions by accomplishing all the applicable actions specified in the Accomplishment Instructions. (1) For airplanes that have accumulated fewer than 13,500 total flight cycles as December 21, 2005 (the effective date of AD 2005–25–03): Replace prior to the accumulation of 13,500 total flight cycles, or within 1,000 flight cycles after December 21, 2005, whichever occurs later. (2) For airplanes that have accumulated 13,500 or more total flight cycles as of December 21, 2005: Replace at the later of the times specified in paragraphs (f)(2)(i) and (f)(2)(ii) of this AD. VerDate Aug<31>2005 15:25 Apr 10, 2006 Jkt 208001 18253 (i) Prior to the accumulation of 18,000 total flight cycles, or within 1,000 flight cycles after December 21, 2005, whichever occurs first. (ii) Within 90 days after December 21, 2005. DEPARTMENT OF TRANSPORTATION New Requirements of This AD [Docket No. FAA–2005–23249; Directorate Identifier 2005–NM–219–AD] Repetitive Inspections (g) Within 24,000 flight cycles after accomplishing the actions specified in paragraph (f) of this AD, perform an external detailed inspection of the skin just below each splice fitting, in accordance with the Accomplishment Instructions of Boeing ASB 737–53A1222, Revision 2, dated October 20, 2005. Thereafter, repeat the external detailed inspections at intervals not to exceed 24,000 flight cycles. Corrective Actions (h) If any cracking is found during any inspection required by this AD, prior to further flight, repair in accordance with a method approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, or with a method approved in accordance with the procedures specified in paragraph (j) of this AD. Acceptable Method of Compliance (i) Replacing the splice fitting and any related investigative actions before December 21, 2005 (the effective date of AD 2005–25– 03), in accordance with Boeing Service Bulletin 737–53–1222, dated June 6, 2002; or Boeing ASB 737–53A1222, Revision 1, dated January 30, 2003, is acceptable for compliance with the requirements of paragraph (f) of this AD. Alternative Methods of Compliance (AMOCs) (j)(1) The Manager, Seattle 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 § 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) An AMOC that provides an acceptable level of safety may be used for any repair required by this AD, if it is approved by an Authorized Representative for the Boeing Commercial Airplanes Delegation Option Authorization Organization who has been authorized by the Manager, Seattle ACO, to make those findings. For a repair method to be approved, the repair must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (4) AMOCs approved previously in accordance with AD 2005–25–03, amendment 39–14396, are approved as AMOCs for the corresponding provisions of paragraphs (f) and (h) of this AD. Issued in Renton, Washington, on March 31, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06–3442 Filed 4–10–06; 8:45 am] BILLING CODE 4910–13–P PO 00000 Frm 00023 Fmt 4702 Sfmt 4702 Federal Aviation Administration 14 CFR Part 39 RIN 2120–AA64 Airworthiness Directives; Gulfstream Model GV–SP Series Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Proposed rule; withdrawal. AGENCY: SUMMARY: The FAA withdraws a notice of proposed rulemaking (NPRM) that proposed a new airworthiness directive (AD) for certain Gulfstream Model GV– SP series airplanes. The proposed AD would have required an inspection to determine the serial number of the antiskid control unit (ACU) in the right electronics equipment rack, and replacement of the ACU with a new or serviceable ACU if necessary. Since the proposed AD was issued, we have received new data that indicate the identified unsafe condition has been corrected on all airplanes that would have been affected by the NPRM, and on all ACUs in the affected range of serial numbers. Accordingly, the proposed AD is withdrawn. ADDRESSES: You may examine the 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 U.S. Department of Transportation, 400 Seventh Street, SW., Room PL–401, Washington, DC. This docket number is FAA–2005–23249; the directorate identifier for this docket is 2005–NM– 219–AD. FOR FURTHER INFORMATION CONTACT: Darby Mirocha, Aerospace Engineer, Systems and Equipment Branch, ACE– 119A, FAA, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite 450, Atlanta, Georgia 30349; telephone (770) 703–6095; fax (770) 703–6097. SUPPLEMENTARY INFORMATION: Discussion We proposed to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) with a notice of proposed rulemaking (NPRM) for a new AD for certain Gulfstream Model GV–SP series airplanes. That NPRM was published in E:\FR\FM\11APP1.SGM 11APP1 18254 Federal Register / Vol. 71, No. 69 / Tuesday, April 11, 2006 / Proposed Rules the Federal Register on December 9, 2005 (70 FR 73173). The NPRM would have required an inspection to determine the serial number of the antiskid control unit (ACU) in the right electronics equipment rack, and replacement of the ACU with a new or serviceable ACU if necessary. The NPRM resulted from a report that an airplane temporarily lost normal braking function during landing rollout on a pre-delivery flight. The proposed actions were intended to prevent loss of normal braking function, which could result in a runway overrun that could cause injury to flightcrew or passengers or damage to the airplane. hsrobinson on PROD1PC70 with PROPOSALS Actions Since NPRM Was Issued Since we issued the NPRM, Gulfstream Aerospace has provided data that indicate the identified unsafe condition has been corrected on all airplanes that would have been affected by the NPRM, and on all ACUs in the affected range of serial numbers (S/Ns). Gulfstream Aerospace therefore requests that we withdraw the NPRM. We agree with the commenter. Request To Incorporate by Reference (IBR) the Service Information The Modification and Replacement Parts Association (MARPA) requests that we either publish the relevant service information with the AD, or IBR it with the NPRM. If we IBR rather than publish the relevant service information, then MARPA further requests that we identify the S/Ns of the defective ACUs in the AD. As justification, MARPA states that parts purveyors and maintenance facilities cannot identify the defective parts unless we specify them in the AD because they do not possess the proprietary service information referenced in the NPRM. For the same reason, MARPA states that those in the alternative parts industry (operating under 14 CFR 21.303) also cannot identify any parts manufacturer approval (PMA) parts equivalent to the defective ACUs. MARPA asserts that there are many ACUs in its PMA database that also may be affected by unsafe condition identified in the NPRM. MARPA also comments on our practice of IBR and referencing propriety service information. MARPA asserts that if we IBR proprietary service information with a public document, such as an AD, then that service information loses its protected status and becomes a public document. Also, MARPA claims that IBR requires we provide a copy of the relevant service information to the Director of the VerDate Aug<31>2005 15:25 Apr 10, 2006 Jkt 208001 Federal Register before the NPRM can be published. MARPA further states that: ‘‘Merely referencing a service document without incorporation thus becomes an ‘‘end run’’ around the publication requirement while still requiring possession of a proprietary document in order to comply with the law.’’ MARPA believes our practice of IBR is flawed legally where it is impossible to comply with the requirements of an AD without first obtaining the necessary propriety service information. Although we acknowledge MARPA’s comments, we do not agree with its request, since the identified unsafe condition has been corrected on all airplanes that would have been affected by the NPRM and on all ACUs in the affected range of S/Ns. Those affected parts are ACUs having part number 1159SCL501–1 and S/Ns 355 through 400 inclusive. The unsafe condition identified in the NPRM was caused by the installation of incorrect capacitors in the affected ACUs only. Since that NPRM addresses a quality control issue limited to a range of S/Ns, we find that the MARPA’s statements regarding PMA equivalent parts are not relevant to that particular NPRM. We have one correction regarding MARPA’s comments on our practice of IBR and referencing propriety service information; we are required to provide a copy of any relevant service information to the Director of the Federal Register for publication of a final rule, not an NPRM. We are currently reviewing our practice of referencing proprietary service information. Once we have thoroughly examined all aspects of this issue, and have made a final determination, we will consider whether our current practice needs to be revised. FAA’s Conclusions Upon further consideration, we have determined that the actions that would have been required by the NPRM have already been accomplished on all affected airplanes, and that the identified unsafe condition has been corrected on all affected ACUs. Accordingly, the NPRM is withdrawn. Withdrawal of the NPRM does not preclude the FAA from issuing another related action or commit the FAA to any course of action in the future. Regulatory Impact Since this action only withdraws an NPRM, it is neither a proposed nor a final rule and therefore is not covered under Executive Order 12866, the Regulatory Flexibility Act, or DOT PO 00000 Frm 00024 Fmt 4702 Sfmt 4702 Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Safety. The Withdrawal Accordingly, we withdraw the NPRM, Docket No. FAA–2005–23249, Directorate Identifier 2005–NM–219– AD, which was published in the Federal Register on December 9, 2005 (70 FR 73173). Issued in Renton, Washington, on March 31, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E6–5253 Filed 4–10–06; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 71 [Docket No. FAA–2006–23902; Airspace Docket No. 06–AGL–01] Proposed Modification of Class E Airspace; Fremont, MI Federal Aviation Administration, (FAA), DOT. ACTION: Notice of proposed rulemaking. AGENCY: SUMMARY: This document proposes to modify Class E airspace at Fremont, MI. Standard Instrument Approach Procedures have been developed for Fremont Municipal Airport, Fremont, MI. Controlled airspace extending upward from 700 feet or more above the surface of the earth is needed to contain aircraft executing these approaches. This action would increase the area of the existing controlled airspace for Fremont, MI. DATES: Comments must be received on or before June 5, 2006. ADDRESSES: Send comments on the proposal to the Docket Management System, U.S. Department of Transportation, Room Plaza 401, 400 Seventh Street, SW., Washington, DC 20590–0001. You must identify the docket Number FAA–2006–23901/ Airspace Docket No. 06–AGL–01, at the beginning of your comments. You may also submit comments on the Internet at https://dms.dot.gov. You may review the public docket containing the proposal, any comments received, and any final disposition in person in the Dockets Office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Office (telephone E:\FR\FM\11APP1.SGM 11APP1

Agencies

[Federal Register Volume 71, Number 69 (Tuesday, April 11, 2006)]
[Proposed Rules]
[Pages 18253-18254]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-5253]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-23249; Directorate Identifier 2005-NM-219-AD]
RIN 2120-AA64


Airworthiness Directives; Gulfstream Model GV-SP Series Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Proposed rule; withdrawal.

-----------------------------------------------------------------------

SUMMARY: The FAA withdraws a notice of proposed rulemaking (NPRM) that 
proposed a new airworthiness directive (AD) for certain Gulfstream 
Model GV-SP series airplanes. The proposed AD would have required an 
inspection to determine the serial number of the anti-skid control unit 
(ACU) in the right electronics equipment rack, and replacement of the 
ACU with a new or serviceable ACU if necessary. Since the proposed AD 
was issued, we have received new data that indicate the identified 
unsafe condition has been corrected on all airplanes that would have 
been affected by the NPRM, and on all ACUs in the affected range of 
serial numbers. Accordingly, the proposed AD is withdrawn.

ADDRESSES: You may examine the 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 U.S. 
Department of Transportation, 400 Seventh Street, SW., Room PL-401, 
Washington, DC. This docket number is FAA-2005-23249; the directorate 
identifier for this docket is 2005-NM-219-AD.

FOR FURTHER INFORMATION CONTACT: Darby Mirocha, Aerospace Engineer, 
Systems and Equipment Branch, ACE-119A, FAA, Atlanta Aircraft 
Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite 
450, Atlanta, Georgia 30349; telephone (770) 703-6095; fax (770) 703-
6097.

SUPPLEMENTARY INFORMATION:

Discussion

    We proposed to amend part 39 of the Federal Aviation Regulations 
(14 CFR part 39) with a notice of proposed rulemaking (NPRM) for a new 
AD for certain Gulfstream Model GV-SP series airplanes. That NPRM was 
published in

[[Page 18254]]

the Federal Register on December 9, 2005 (70 FR 73173). The NPRM would 
have required an inspection to determine the serial number of the anti-
skid control unit (ACU) in the right electronics equipment rack, and 
replacement of the ACU with a new or serviceable ACU if necessary. The 
NPRM resulted from a report that an airplane temporarily lost normal 
braking function during landing rollout on a pre-delivery flight. The 
proposed actions were intended to prevent loss of normal braking 
function, which could result in a runway overrun that could cause 
injury to flightcrew or passengers or damage to the airplane.

Actions Since NPRM Was Issued

    Since we issued the NPRM, Gulfstream Aerospace has provided data 
that indicate the identified unsafe condition has been corrected on all 
airplanes that would have been affected by the NPRM, and on all ACUs in 
the affected range of serial numbers (S/Ns). Gulfstream Aerospace 
therefore requests that we withdraw the NPRM. We agree with the 
commenter.

Request To Incorporate by Reference (IBR) the Service Information

    The Modification and Replacement Parts Association (MARPA) requests 
that we either publish the relevant service information with the AD, or 
IBR it with the NPRM. If we IBR rather than publish the relevant 
service information, then MARPA further requests that we identify the 
S/Ns of the defective ACUs in the AD. As justification, MARPA states 
that parts purveyors and maintenance facilities cannot identify the 
defective parts unless we specify them in the AD because they do not 
possess the proprietary service information referenced in the NPRM. For 
the same reason, MARPA states that those in the alternative parts 
industry (operating under 14 CFR 21.303) also cannot identify any parts 
manufacturer approval (PMA) parts equivalent to the defective ACUs. 
MARPA asserts that there are many ACUs in its PMA database that also 
may be affected by unsafe condition identified in the NPRM.
    MARPA also comments on our practice of IBR and referencing 
propriety service information. MARPA asserts that if we IBR proprietary 
service information with a public document, such as an AD, then that 
service information loses its protected status and becomes a public 
document. Also, MARPA claims that IBR requires we provide a copy of the 
relevant service information to the Director of the Federal Register 
before the NPRM can be published. MARPA further states that: ``Merely 
referencing a service document without incorporation thus becomes an 
``end run'' around the publication requirement while still requiring 
possession of a proprietary document in order to comply with the law.'' 
MARPA believes our practice of IBR is flawed legally where it is 
impossible to comply with the requirements of an AD without first 
obtaining the necessary propriety service information.
    Although we acknowledge MARPA's comments, we do not agree with its 
request, since the identified unsafe condition has been corrected on 
all airplanes that would have been affected by the NPRM and on all ACUs 
in the affected range of S/Ns. Those affected parts are ACUs having 
part number 1159SCL501-1 and S/Ns 355 through 400 inclusive. The unsafe 
condition identified in the NPRM was caused by the installation of 
incorrect capacitors in the affected ACUs only. Since that NPRM 
addresses a quality control issue limited to a range of S/Ns, we find 
that the MARPA's statements regarding PMA equivalent parts are not 
relevant to that particular NPRM.
    We have one correction regarding MARPA's comments on our practice 
of IBR and referencing propriety service information; we are required 
to provide a copy of any relevant service information to the Director 
of the Federal Register for publication of a final rule, not an NPRM. 
We are currently reviewing our practice of referencing proprietary 
service information. Once we have thoroughly examined all aspects of 
this issue, and have made a final determination, we will consider 
whether our current practice needs to be revised.

FAA's Conclusions

    Upon further consideration, we have determined that the actions 
that would have been required by the NPRM have already been 
accomplished on all affected airplanes, and that the identified unsafe 
condition has been corrected on all affected ACUs. Accordingly, the 
NPRM is withdrawn.
    Withdrawal of the NPRM does not preclude the FAA from issuing 
another related action or commit the FAA to any course of action in the 
future.

Regulatory Impact

    Since this action only withdraws an NPRM, it is neither a proposed 
nor a final rule and therefore is not covered under Executive Order 
12866, the Regulatory Flexibility Act, or DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979).

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

The Withdrawal

    Accordingly, we withdraw the NPRM, Docket No. FAA-2005-23249, 
Directorate Identifier 2005-NM-219-AD, which was published in the 
Federal Register on December 9, 2005 (70 FR 73173).

    Issued in Renton, Washington, on March 31, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E6-5253 Filed 4-10-06; 8:45 am]
BILLING CODE 4910-13-P
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.