Airworthiness Directives: Boeing Model 767 200, 300, and 400ER Series Airplanes
Federal Register: March 18, 2008 (Volume 73, Number 53)
Proposed Rules
Page 14405-14408
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
DOCID:fr18mr08-20
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA-2008-0302; Directorate Identifier 2007-NM-323-AD
RIN 2120-AA64
Airworthiness Directives; Boeing Model 767-200, -300, and -400ER
Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
SUMMARY: The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Boeing Model 767-200, -300, and
-400ER series airplanes. The existing AD currently requires an inspection to determine if the door-mounted escape slide/rafts have certain part numbers. For those door-mounted escape slide/rafts having certain part numbers, the existing AD also currently requires an inspection for excessive tension of the firing cable, and procedures for providing slack in the firing cable or rerouting the firing cable if necessary. For certain airplanes, this proposed AD would require a review of the airplane maintenance records to determine if a certain service bulletin has been incorporated, or an inspection to determine if certain door-mounted escape slide/rafts are installed. This proposed
AD would also require modification of certain escape slide/rafts. This proposed AD results from reports of uncommanded inflation inside the airplane of a door-mounted escape slide/raft located in the passenger compartment. We are
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proposing this AD to prevent injury to maintenance personnel, passengers, and crew during otherwise normal operating conditions and to prevent interference with evacuation of the airplane during an emergency, due to uncommanded inflation of a door-mounted escape slide/ raft.
DATES: We must receive comments on this proposed AD by May 2, 2008.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to http:// www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For service information identified in this AD, contact Boeing
Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207.
Examining the AD Docket
You may examine the AD docket on the Internet at http:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone 800-647-5527) is in the
ADDRESSES section. Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Keith Ladderud, Aerospace Engineer,
Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 917-6435; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2008-0302;
Directorate Identifier 2007-NM-323-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD because of those comments.
We will post all comments we receive, without change, to http:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD.
Discussion
On June 7, 2005, we issued AD 2005-12-14, amendment 39-14130 (70 FR 34638, June 15, 2005), for certain Boeing Model 767-200, -300, and - 400ER series airplanes. That AD requires an inspection to determine if the door-mounted escape slide/rafts have certain part numbers. For those door-mounted escape slide/rafts having certain part numbers, that
AD also requires an inspection for excessive tension of the firing cable, and procedures for providing slack in the firing cable or rerouting the firing cable if necessary. That AD resulted from reports of uncommanded inflation inside the airplane of a door-mounted escape slide/raft located in the passenger compartment. We issued that AD to prevent injury to maintenance personnel, passengers, and crew during otherwise normal operating conditions and to prevent interference with evacuation of the airplane during an emergency, due to uncommanded inflation of a door-mounted escape slide/raft.
Actions Since Existing AD Was Issued
The preamble to AD 2005-12-14 specified that we considered the requirements ``interim action'' and that the manufacturer was developing a modification to address the unsafe condition. That AD explained that we might consider further rulemaking if a modification is developed, approved, and available. The manufacturer now has developed such a modification, and we have determined that further rulemaking is indeed necessary; this proposed AD follows from that determination. Boeing has issued Alert Service Bulletin 767-25A0395,
Revision 1, dated January 25, 2007, to provide instructions for accomplishing the modification.
Relevant Service Information
We have reviewed Revision 1 of Boeing Alert Service Bulletin 767- 25A0395. For Group 1 and 2 airplanes, the service bulletin describes procedures for doing either a records verification to determine if
Boeing Service Bulletin 767-25-0266 has been incorporated, or a general visual inspection to determine if any door-mounted escape slide/raft having part number (P/N) 5A3294-1, 5A3294-2, 5A3295-1, or 5A3295-3 is installed. For Group 1 and 2 airplanes, the service bulletin also describes procedures for doing the corrective action, which is to modify the escape slide/rafts, if Boeing Service Bulletin 767-25-0266 has been incorporated or if P/N 5A3294-1, 5A3294-2, 5A3295-1, or 5A3295-3 is installed. For Group 3, 4, 5 and 6 airplanes, the service bulletin describes procedures for modifying the door-mounted escape slide/rafts. Accomplishing the actions specified in the service information is intended to adequately address the unsafe condition.
The service bulletin refers to Goodrich Service Bulletin 5A3294/ 5A3295-25-362, dated July 25, 2006, as an additional source of service information for modifying a door-mounted escape slide/raft by replacing the firing cable with a longer cable and testing the regulator valve of the inflation trigger system for the door-mounted escape slide/raft.
FAA's Determination and Requirements of the Proposed AD
We have evaluated all pertinent information and identified an unsafe condition that is likely to develop on other products of the same type design. For this reason, we are proposing this AD, which would supersede AD 2005-12-14 and would retain the requirements of the existing AD. This proposed AD would also require accomplishing the actions specified in the service information described previously.
Costs of Compliance
There are about 1,225 airplanes of the affected design in the worldwide fleet. This proposed AD would affect about 355 airplanes of
U.S. registry.
The actions that are required by AD 2005-12-14 and retained in this proposed AD take up to about 6 work hours per airplane, at an average labor rate of $80 per work hour. Based on these figures, the estimated cost of the currently required actions for U.S. operators is $170,400, or is $480 per airplane.
The new proposed actions would take up to about 6 work hours per airplane, at an average labor rate of $80 per work hour. The parts manufacturer states that it will supply the required parts to operators at no cost. Based on these figures, the estimated cost of the new
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actions specified in this proposed AD for U.S. operators is $170,400, or $480 per airplane.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action.
Regulatory Findings
We have determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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.
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.
Sec. 39.13 [Amended] 2. The Federal Aviation Administration (FAA) amends Sec. 39.13 by removing amendment 39-14130 (70 FR 34638, June 15, 2005) and adding the following new airworthiness directive (AD):
Boeing: Docket No. FAA-2008-0302; Directorate Identifier 2007-NM- 323-AD.
Comments Due Date
(a) The FAA must receive comments on this AD action by May 2, 2008.
Affected ADs
(b) This AD supersedes AD 2005-12-14.
Applicability
(c) This AD applies to Boeing Model 767-200, -300, and -400ER series airplanes, certificated in any category, equipped with door- mounted escape slide/rafts.
Unsafe Condition
(d) This AD results from reports of uncommanded inflation inside the airplane of a door-mounted escape slide/raft located in the passenger compartment. We are issuing this AD to prevent injury to maintenance personnel, passengers, and crew during otherwise normal operating conditions and to prevent interference with evacuation of the airplane during an emergency, due to uncommanded inflation of a door-mounted escape slide/raft.
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.
Restatement of Requirements of AD 2005-12-14
Inspection for Part Numbers (P/Ns)
(f) Within 30 days after June 30, 2005 (the effective date of AD 2005-12-14), accomplish the actions in either paragraph (f)(1) or
(f)(2) of this AD.
(1) Perform a one-time inspection to determine if any Goodrich door-mounted escape slide/raft having P/N 5A3294-1, 5A3294-2, 5A3295-1, or 5A3295-3 is installed. If no slide/raft having any of those part numbers is installed, no further action is required by this paragraph, except for the requirements of paragraph (j) of this
AD.
(2) Perform a one-time check of the airplane maintenance records to determine if any Goodrich door-mounted escape slide/raft having
P/N 5A3294-1, 5A3294-2, 5A3295-1, or 5A3295-3 is installed. If it can be conclusively determined from the airplane maintenance records that no slide/raft having any of those part numbers is installed, no further action is required by this AD, except for the requirements of paragraph (j) of this AD.
Inspection for Excessive Tension on the Firing Cable
(g) If any door-mounted escape slide/raft with any part number specified in paragraph (f) of this AD is installed: Within 30 days after June 30, 2005, perform a tension check on the firing cable of the slide/raft, in accordance with Boeing Alert Service Bulletin 767-25A0390, dated May 13, 2005. If no excessive tension is detected, no further action is required by this AD, except for the requirements of paragraph (j) of this AD.
Note 1: Boeing Alert Service Bulletin 767-25A0390, dated May 13, 2005, references Goodrich Alert Service Bulletin 5A3294/5A3295- 25A356, dated May 11, 2005, as an additional source of service information.
Corrective Action for Excessive Tension on the Firing Cable
(h) If any excessive tension of the firing cable is detected, before further flight, do the applicable corrective actions in accordance with the Boeing Alert Service Bulletin 767-25A0390, dated
May 13, 2005.
Previous Accomplishment
(i) Inspections of the firing cables for excessive tension in accordance with Boeing Alert Service Bulletin 767-25A0390, dated May 13, 2005, that were accomplished before June 30, 2005, are acceptable for compliance with the requirements of paragraph (g) of this AD, provided that any applicable corrective action was completed.
Parts Installation
(j) As of June 30, 2005, no person may install on any airplane any Goodrich door-mounted escape slide/raft having P/N 5A3294-1, 5A3294-2, 5A3295-1, or 5A3295-3, unless the tension of the firing cable has been checked and the applicable corrective action completed in accordance with Boeing Alert Service Bulletin 767- 25A0390, dated May 13, 2005, or the escape slide/raft has been repacked in accordance with Goodrich Packing Instructions,
Evacuation Slide/Raft, Document 501636, Revision G, dated May 16, 2005; Goodrich Packing Instructions, Evacuation Slide/Raft, LH,
Document 501637, Revision E, dated May 16, 2005; or Goodrich Packing
Instructions, Evacuation Slide/Raft, RH, Document 501638, Revision
D, dated May 16, 2005; as applicable.
New Requirements of This AD
Modification
(k) For airplanes identified in Boeing Alert Service Bulletin 767-25A0395, Revision 1, dated January 25, 2007: Within 36 months after the effective date of this AD, do the applicable actions specified in paragraph (k)(1) or (k)(2) of this AD, by accomplishing all of the applicable actions specified in the service bulletin.
(1) For Group 1 and 2 airplanes as identified in the service bulletin: Review the airplane maintenance records to determine if
Boeing Service Bulletin 767-25-0266 has been incorporated, or do a general visual inspection to determine if any door-mounted escape slide/raft having P/N 5A3294-1, 5A3294-2, 5A3295-1, or 5A3295-3 is installed, and before further flight do all the
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applicable corrective actions. Doing the inspection before the effective date of this AD in accordance with paragraph (f)(1) of this AD is acceptable for compliance with the inspection specified in this paragraph.
(2) For Group 3, 4, 5, and 6 airplanes as identified in the service bulletin: Modify the escape slide/rafts.
Note 2: Boeing Alert Service Bulletin 767-25A0395, Revision 1, refers to Goodrich Service Bulletin 5A3294/5A3295-25-362, dated July 25, 2006, as an additional source of service information for modifying a door-mounted escape slide/raft.
Alternative Methods of Compliance (AMOCs)
(l)(1) The Manager, Seattle Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.
(2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA
Flight Standards District Office (FSDO), or lacking a PI, your local
FSDO.
(3) AMOCs approved previously in accordance with AD 2005-12-14, amendment 39-14130, are approved as AMOCs for the corresponding provisions of paragraphs (f), (g), (h), (i), and (j) of this AD.
Issued in Renton, Washington, on March 9, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane Directorate, Aircraft
Certification Service.
FR Doc. E8-5373 Filed 3-17-08; 8:45 am
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