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Docket ID: [Docket No. FAA-2007-0346; Directorate Identifier 2007-NM-202-AD; Amendment 39-15436; AD 2008-06-24]
RIN ID: RIN 2120-AA64
SUBJECT CATEGORY: Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 23, 2008.
DOCUMENT SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Boeing Model 737300, 400, and 500 series airplanes. This AD requires
an inspection to determine the manufacturer and manufacture date of the
oxygen masks in the passenger service unit and the lavatory and
attendant box assemblies, corrective action if necessary, and other
specified action. This AD results from a report that several passenger
masks with broken inline flow indicators were found following a mask
deployment. We are issuing this AD to prevent the inline flow
indicators of the passenger oxygen masks from fracturing and
separating, which could inhibit oxygen flow to the masks and
consequently result in exposure of the passengers and cabin attendants to hypoxia following a depressurization event.
[[Page 14667]]
SUMMARY: Boeing Model 737-300, 400, and 500 Series Airplanes,
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to certain Model Boeing 737300, 400, and 500 series airplanes. That NPRM was published in the Federal Register on December 19, 2007 (72 FR 71830). That NPRM proposed to require an inspection to determine the manufacturer and manufacture date of the oxygen masks in the passenger service unit (PSU) and the lavatory and attendant box assemblies, corrective action if necessary, and other specified action. Comments
We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public.
We reviewed the relevant data and determined that air safety and the public interest require adopting the AD as proposed.
There are about 1,956 airplanes of the affected design in the worldwide fleet. This AD affects about 646 airplanes of U.S. registry. The required actions take about 16 work hours per airplane, for an average of 180 oxygen masks per airplane distributed in about 45 PSUs/ oxygen boxes, at an average labor rate of $80 per work hour. Required parts cost about $6 per oxygen mask, or $1,080 per airplane. Based on these figures, the estimated cost of the AD for U.S. operators is $1,524,560, or $2,360 per airplane.
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.
This AD will not have federalism implications under Executive Order 13132. This AD 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.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive Order 12866,
(2) Is not a ``significant rule'' under 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.
You can find our regulatory evaluation and the estimated costs of compliance in the AD Docket.
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39AIRWORTHINESS 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 FAA amends Sec. 39.13 by adding the following new AD:
20080624 Boeing: Amendment 3915436. Docket No. FAA20070346; Directorate Identifier 2007NM202AD.
Effective Date
(a) This airworthiness directive (AD) is effective April 23, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Boeing Model 737300, 400, and 500
series airplanes, certificated in any category; as identified in
Boeing Special Attention Service Bulletin 737351099, dated April 9, 2007.
Unsafe Condition
(d) This AD results from a report that several passenger masks
with broken inline flow indicators were found following a mask
deployment. We are issuing this AD to prevent the inline flow
indicators of the passenger oxygen masks from fracturing and
separating, which could inhibit oxygen flow to the masks and
consequently result in exposure of the passengers and cabin attendants to hypoxia following a depressurization event.
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.
Inspection and Related Investigative/Corrective Actions if Necessary
(f) Within 60 months after the effective date of this AD, do a
general visual inspection to determine the manufacturer and
manufacture date of the oxygen masks in the passenger service unit
and the lavatory and attendant box assemblies, and do the applicable
corrective action and other specified action, by accomplishing all of the applicable actions specified in the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 73735
1099, dated April 9, 2007; except where the service bulletin
specifies repairing the oxygen mask assembly, replace it with a new [[Page 14668]]
or modified oxygen mask assembly having an improved flow indicator.
The corrective action and other specified action must be done before further flight.
Note 1: Boeing Special Attention Service Bulletin 737351099
refers to B/E Aerospace Service Bulletin 1740803501, dated
February 6, 2006; and Revision 1, dated May 1, 2006; as additional
sources of service information for modifying the oxygen mask
assembly by replacing the flow indicator with an improved flow indicator.
Alternative Methods of Compliance (AMOCs)
(g)(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.
Material Incorporated by Reference
(h) You must use Boeing Special Attention Service Bulletin 737
351099, dated April 9, 2007, to do the actions required by this AD, unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 981242207.
(3) You may review copies of the service information
incorporated by reference at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the
National Archives and Records Administration (NARA). For information
on the availability of this material at NARA, call 2027416030, or
go to: http://www.archives.gov/federal_register/code_of_federal_ regulations/ibr_locations.html.
Issued in Renton, Washington, on March 9, 2008.
Stephen P. Boyd,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E85276 Filed 31808; 8:45 am]
BILLING CODE 491013P
FOR FURTHER INFORMATION CONTACT Susan Letcher, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM150S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 980573356; telephone (425) 9176474; fax (425) 9176590.
14 CFR Part 39 40 CFR Part 52 14 CFR Part 71 33 CFR Part 165 50 CFR Part 679 26 CFR Part 1 40 CFR Part 180 47 CFR Part 73 33 CFR Part 117 50 CFR Part 17 44 CFR Part 67 50 CFR Part 648 14 CFR Part 97 33 CFR Part 100 40 CFR Part 63 50 CFR Part 622 26 CFR Part 301 50 CFR Part 660 39 CFR Part 111 40 CFR Part 300 44 CFR Part 65 40 CFR Part 271 40 CFR Parts 52 and 81 47 CFR Part 64 50 CFR Part 665 49 CFR Part 571 44 CFR Part 64 21 CFR Part 522 50 CFR Part 229 14 CFR Part 23