AD 2003-09-04 R1

This amendment revises an existing airworthiness directive (AD), applicable to certain Bombardier Model CL-600-2B19 (Regional Jet series 100 & 440) airplanes, that currently requires revising the airworthiness limitations section of the Instructions for Continued Airworthiness by incorporating new structural inspection intervals for the pressure floor skin of the center fuselage at fuselage stations 460 and 513; repair if necessary; and submission of inspection findings to the airplane manufacturer. This amendment terminates the reporting requirement and includes a provision to allow removal of the referenced service information when the information specified in it is included in the general revisions of the maintenance manual. The actions specified in this AD are intended to detect and correct in a timely manner fatigue cracks of the pressure floor skin of the center fuselage at fuselage stations 460 and 513, which could result in failure of the pressure floor skin and consequent rapid decompression of the airplane during flight. This action is intended to address the identified unsafe condition.

Final rule; request for comments.

2003-09-04 R1 Bombardier, Inc. (Formerly Canadair): Amendment 39- 13305. Docket 2003-NM-179-AD. Revises AD 2003-09-04, Amendment 39- 13133. \n\n\tApplicability: Model CL-600-2B19 (Regional Jet series 100 & 440) airplanes, serial numbers 7003 through 7999 inclusive; certificated in any category. \n\n\tNote 1: This AD requires revisions to certain operator maintenance documents to include new inspections. Compliance with these inspections is required by 14 CFR Part 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with 14 CFR part 91.403(c), the operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. The request should include a description of changes to the required inspections that will ensure the continued damage tolerance of the affected structure. The FAA has provided guidance for this determination in Advisory Circular (AC) 25-1529. \n\n\tCompliance: Required as indicated, unless accomplished previously. \n\n\tTo detect and correct in a timely manner fatigue cracks of the pressure floor skin of the center fuselage at fuselage stations 460 and 513, which could result in failure of the pressure floor skin and consequent rapid decompression of the airplane during flight, accomplish the following: \n\nRevise Airworthiness Limitations (AWL) Section \n\n\t(a) Within 14 days after May 14, 2003 (the effective date AD 2003-09-04, amendment 39-13133), revise the AWL section of the Instructions for Continued Airworthiness by inserting a copy of Canadair Temporary Revision (TR) 2B-1230, Canadair Regional Jet Maintenance Requirements Manual, Part 2, Appendix B, ''Airworthiness Limitations,'' approved on July 26, 2002, by Transport Canada Civil Aviation (TCCA), into the AWL section. Thereafter, except as provided in paragraph (e)of this AD, no alternative structural inspection intervals may be approved for the pressure floor skin of the center fuselage at fuselage stations 460 and 513. \n\n\t(b) When the information in Canadair TR 2B-1230, Canadair Regional Jet Maintenance Requirements Manual, Part 2, Appendix B, ''Airworthiness Limitations,'' approved on July 26, 2002, by TCCA, is included in the general revisions of the maintenance manual, this TR may be removed. \n\nRepair and Revise AWL Section \n\n\t(c) If any crack is found during any inspection required by paragraph (a) of this AD, before further flight, do the actions specified in paragraphs (c)(1) and (c)(2) of this AD. \n\n\t(1) Repair per a method approved by either the Manager, New York Aircraft Certification Office (ACO), FAA; or TCCA (or its delegated agent). \n\n\t(2) Revise the AWL section of the Instructions for Continued Airworthiness by inserting a copy of the new airworthiness limitation and inspection requirements associated with the FAA-or TCCA-approved repair referred to in paragraph (c)(1) of this AD into the Canadair Regional Jet Maintenance Requirements Manual, Part 2, Appendix B, ''Airworthiness Limitations'' section. Thereafter, except as provided in paragraph (e) of this AD, no alternative structural inspection intervals specified in the FAA-or TCCA- approved repair may be approved for the pressure floor skin of the center fuselage at fuselage stations 460 and 513. \n\nReporting \n\n\t(d) Within 30 days after each inspection required by this AD, submit a report of the inspection results (both positive and negative findings) to Bombardier, Inc., Canadair, Aerospace Group, P.O. Box 6087, Station Centre-ville, Montreal, Quebec H3C 3G9, Canada; telephone (514) 855-5001, extension 58500; fax (514) 855- 8501. Information collection requirements contained in this AD have been approved by the Office of Management and Budget (OMB) under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C. 3501 et seq.) and have been assigned OMB Control Number 2120-0056. This requirement ends 4 years after the effective date of this AD. \n\nAlternative Methods of Compliance \n\n\t(e) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, New York ACO, FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, New York ACO. \n\n\tNote 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the New York ACO. \n\nSpecial Flight Permits \n\n\t(f) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. \n\nIncorporation by Reference \n\n\t(g) Unless otherwise specified inthis AD, the AWL revision shall be done in accordance with Canadair Temporary Revision 2B- 1230, Canadair Regional Jet Maintenance Requirements Manual, Part 2, Appendix B, ''Airworthiness Limitations,'' approved on July 26, 2002, by TCCA. (The approval date of this document is indicated only on page 2 of 2.) The incorporation by reference of that document was approved previously by the Director of the Federal Register as of May 14, 2003 (68 FR 22587, April 29, 2003). Copies may be obtained from Bombardier, Inc., Canadair, Aerospace Group, P.O. Box 6087, Station Centre-ville, Montreal, Quebec H3C 3G9, Canada. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or the FAA, New York Aircraft Certification Office, 10 Fifth Street, Third Floor, Valley Stream, New York; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. \n\n\tNote 3: The subject of this AD is addressed in Canadian airworthiness directive CF-2002-39, effective date October 25, 2002. \n\nEffective Date \n\n\t(h) This amendment becomes effective on October 7, 2003.

On April 21, 2003, the FAA issued AD 2003- 09-04, amendment 39-13133 (68 FR 22587, April 29, 2003), applicable to certain Bombardier Model CL-600-2B19 (Regional Jet series 100 & 440) airplanes, to require revising the airworthiness limitations (AWL) section of the Instructions for Continued Airworthiness by incorporating new structural inspection intervals for the pressure floor skin of the center fuselage at fuselage stations 460 and 513; repair if necessary; and submission of inspection findings to the airplane manufacturer. That action was prompted by a report of fatigue cracks on the pressure floor skin of the center fuselage at fuselage stations 460 and 513. The actions required by that AD are intended to detect and correct in a timely manner fatigue cracks of the pressure floor skin of the center fuselage at fuselage stations 460 and 513, which could result in failure of the pressure floor skin and consequent rapid decompression of the airplane during flight. \n\nComments \n\n\tInterested persons were afforded an opportunity to submit comments in response to AD 2003-09-04. Due consideration has been given to the comments received. \n\nRequest To Specify the Provisions of Referenced Temporary Revision (TR) \n\n\tOne commenter requests that AD 2003-09-04 be revised to specify the provisions of Canadair TR 2B-1230, Canadair Regional Jet Maintenance Requirements Manual, Part 2, Appendix B, ''Airworthiness Limitations,'' approved on July 26, 2002, by Transport Canada Civil Aviation (TCCA) as a method of compliance, rather than specifying insertion of the TR into the AWL section as the only means of compliance. The commenter states that there is no provision to maintain compliance when revising the maintenance manual with a formal revision that incorporates the TR text. \n\n\tWe agree. We have added a new paragraph (b) (subsequent paragraphs have been redesignated) stating, ''When the information in Canadair TR 2B-1230, Canadair Regional JetMaintenance Requirements Manual, Part 2, Appendix B, 'Airworthiness Limitations,' approved on July 26, 2002, by TCCA, is included in the general revisions of the maintenance manual, this TR may be removed.'' \n\nRequest To Eventually Terminate Reporting Requirement \n\n\tThe same commenter requests that the reporting requirement specified in paragraph (c) of AD 2003-09-04 be terminated after a reasonable period of time. The commenter states that, although data gathering is important, particularly when evaluating the need for continued compliance with the type of required inspection, continued compliance with the type of required inspection is a burden to operators. \n\n\tWe agree. The purpose of the reporting requirement is for the airplane manufacturer and TCCA to further analyze the need for follow- on action. After consulting with the airplane manufacturer and TCCA, we have determined that reporting inspection findings after four years would be burdensome to the operators and is unnecessary for gathering any salient information. Therefore, we have revised paragraph (d) of this AD by adding the following statement: ''This requirement ends 4 years after the effective date of this AD.'' \n\nFAA's Findings \n\n\tThis airplane model is manufactured in Canada and is type certificated for operation in the United States under the provisions of section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the applicable bilateral airworthiness agreement. Pursuant to this bilateral airworthiness agreement, TCCA has kept the FAA informed of the situation described above. The FAA has examined the findings of TCCA, reviewed all available information, and determined that AD action is necessary for products of this type design that are certificated for operation in the United States. \n\nExplanation of Requirements of Rule \n\n\tSince an unsafe condition has been identified that is likely to exist or develop on other airplanes of the same type design registered in the UnitedStates, this AD revises AD 2003-09-04 to continue to require revising the AWL section of the Instructions for Continued Airworthiness by incorporating new structural inspection intervals for the pressure floor skin of the center fuselage at fuselage stations 460 and 513; repair if necessary; and submission of inspection findings to the airplane manufacturer. This AD revises the existing AD by terminating the reporting requirement four years after the effective date of this AD. This AD also revises the existing AD by including a provision to allow removal of the referenced TR when the information specified in it is included in the general revisions of the maintenance manual. \n\nChanges to 14 CFR Part 39/Effect on the Proposed AD \n\n\tOn July 10, 2002, the FAA issued a new version of 14 CFR part 39 (67 FR 47997, July 22, 2002), which governs the FAA's airworthiness directives system. The regulation now includes material that relates to altered products, special flight permits, and alternative methods of compliance (AMOCs). However, for clarity and consistency in this AD, we have retained the language of AD 2003-09-04 regarding that material. \n\nDetermination of Rule's Effective Date \n\n\tSince a situation exists that requires the immediate adoption of this regulation, it is found that notice and opportunity for prior public comment hereon are impracticable, and that good cause exists for making this amendment effective in less than 30 days. \n\nComments Invited \n\n\tAlthough this action is in the form of a final rule that involves requirements affecting flight safety and, thus, was not preceded by notice and an opportunity for public comment, comments are invited on this rule. Interested persons are invited to comment on this rule by submitting such written data, views, or arguments as they may desire. Communications shall identify the Rules Docket number and be submitted in triplicate to the address specified under the caption ADDRESSES. All communications received on or before the closing date for comments will be considered, and this rule may be amended in light of the comments received. Factual information that supports the commenter's ideas and suggestions is extremely helpful in evaluating the effectiveness of the AD action and determining whether additional rulemaking action would be needed.\n \n\tSubmit comments using the following format: \n\nOrganize comments issue-by-issue. For example, discuss a request to change the compliance time and a request to change the service bulletin reference as two separate issues. \nFor each issue, state what specific change to the AD is being requested. \nInclude justification (e.g., reasons or data) for each request. \n\n\tComments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify the rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report that summarizes each FAA-public contact concerned with the substance of this AD will be filed in the Rules Docket. \n\n\tCommenters wishing the FAA to acknowledge receipt of their comments submitted in response to this rule must submit a self-addressed, stamped postcard on which the following statement is made: ''Comments to Docket Number 2003-NM-179-AD.'' The postcard will be date stamped and returned to the commenter. \n\nRegulatory Impact \n\n\tThe regulations adopted herein will not have a substantial direct effect on the 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. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132. \n\n\tThe FAA has determined that this regulation is an emergency regulation that must be issued immediately to correct an unsafe condition in aircraft, and that it is not a ''significant regulatory action'' under Executive Order 12866. It has been determined further that this action involves an emergency regulation under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). If it is determined that this emergency regulation otherwise would be significant under DOT Regulatory Policies and Procedures, a final regulatory evaluation will be prepared and placed in the Rules Docket. A copy of it, if filed, may be obtained from the Rules Docket at the location provided under the caption ADDRESSES. \n\nList of Subjects in 14 CFR Part 39 \n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. \n\nAdoption of the Amendment \n\nAccordingly, pursuant to 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: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n1. The authority citation forpart 39 continues to read as follows: \n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\nSec. 39.13 (Amended) \n\n2. Section 39.13 is amended by removing amendment 39-13133 (68 FR 22587, April 29, 2003), and by adding a new airworthiness directive (AD), amendment 39-13305, to read as follows: