Published 2011-03-08 · Federal Register document 2011-5292
Airworthiness Directives; Various Transport Category Airplanes Equipped With Chemical Oxygen Generators Installed in a Lavatory
Publication summary
This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 2011-04-09 that was sent previously by individual notices to the known U.S. owners and operators of affected airplanes identified above. This AD requires modifying the chemical oxygen generators in the lavatory. This AD was prompted by reports that the current design of these oxygen generators presents a hazard that could jeopardize flight safety. We are issuing this AD to eliminate this hazard.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:36.067984+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2011-e3661fa6ab35b428
- Source row
- results[65]
- Raw source SHA-256
- e3661fa6ab35b428e6e5ee3716d50c22e985c092328ad8ce2f0f440b962ae0cd
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2011-04-09
- Effective date printed in this edition
- Unknown
Read 11 complete recorded clauses
Effective Date
Effective Date
(a) This AD becomes effective March 14, 2011, to all persons
except those persons to whom it was made immediately effective by AD
2011-04-09, issued on February 10, 2011, which contained the
requirements of this amendment.
Exact source excerpt. Text positions 10718–10965, end exclusive, in the original decoded publication. SHA-256: 897dbc89a1abbb41b0be6798fb90b011547c749ffd65c24b5473f11524437209
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 10965–10994, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to transport category airplanes, in
passenger-carrying operations, that are equipped with any chemical
oxygen generator installed in any lavatory, and are:
(1) Operating under 14 CFR part 121; or
(2) U.S.-registered and operating under 14 CFR part 129, with a
maximum passenger capacity of 20 or greater.
Exact source excerpt. Text positions 10994–11350, end exclusive, in the original decoded publication. SHA-256: 63cc8fb00567ad6335e2a1ce30ffe7e94bc65bbaf16d51f1346f75fdbf448a03
Subject
Subject
(d) Joint Aircraft System Component (JASC)/Air Transport
Association (ATA) of America Code 35, Oxygen.
Exact source excerpt. Text positions 11350–11468, end exclusive, in the original decoded publication. SHA-256: 79655ee1e35ac813e30c37de323ba013c2defa6325c272eae5873150191b83b5
Unsafe Condition
Unsafe Condition
(e) This AD was prompted by reports that the current design of
chemical oxygen generators in the lavatories presents a hazard that
could jeopardize flight safety. We are issuing this AD to eliminate
this hazard.
Exact source excerpt. Text positions 11468–11706, end exclusive, in the original decoded publication. SHA-256: e8cc36dc7edb5600bb90ee655850ae49e7c2eb81ff7cd901a3c304119b2357ad
Compliance
Compliance
(f) Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11706–11808, end exclusive, in the original decoded publication. SHA-256: 76a8ec0548389ac4eaa60ddcc67a7a3de5aedefd320c767b7cf621baa6140ea8
Oxygen Generator Deactivation
Oxygen Generator Deactivation
(g) Within 21 days after the effective date of this AD, do the
actions specified in paragraphs (g)(1) and (g)(2) of this AD.
(1) Activate all chemical oxygen generators in the lavatories
until the generator oxygen supply is expended. An operator may also
remove the oxygen generator(s), in accordance with existing
maintenance practice, in lieu of activating it.
(2) For each chemical oxygen generator, after the generator is
expended (or removed), remove or re-stow the oxygen masks and close
the mask dispenser door.
Note 1: Chemical oxygen generators are considered a hazardous
material and subject to specific requirements under Title 49 CFR for
shipping. Oxygen generators must be expended prior to disposal but
are considered a hazardous waste; therefore, disposal must be in
accordance with all Federal, State, and local regulations. Expended
oxygen generators are forbidden in air transportation as cargo. For
more information, contact 1-800-HMR-4922.
[[Page 12558]]
Note 2: Design approval holders are not expected to release
service instructions for this action.
Exact source excerpt. Text positions 11808–12954, end exclusive, in the original decoded publication. SHA-256: fbcf4b6b3cf5b48dad05582d96c82b0bbd305bac5f359b4c0a788badf4f7d28e
Compliance with Federal Aviation Regulations
Compliance with Federal Aviation Regulations
(h) Notwithstanding the requirements of Sections 25.1447,
121.329, 121.333, and 129.13 of the Federal Aviation Regulations (14
CFR 25.1447, 121.329, 121.333, and 129.13), operators complying with
this AD are authorized to operate affected airplanes until this
action is superseded by other rulemaking.
Exact source excerpt. Text positions 12954–13311, end exclusive, in the original decoded publication. SHA-256: 75525fdb05689a2e3a554bf2e5e6838255d39400754c9bfb57e90c117bcda8c1
Parts Installation
Parts Installation
(i) After the effective date of this AD, no person may install a
chemical oxygen generator in any lavatory on any affected airplane.
Exact source excerpt. Text positions 13311–13470, end exclusive, in the original decoded publication. SHA-256: 506ba156daa2d3f127a40ee61be4e12de11aa309246595d87fc0f2be956d01f7
Special Flight Permit
Special Flight Permit
(j) Special flight permits, as described in Section 21.197 and
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197
and 21.199), are not allowed.
Alternative Methods of Compliance (AMOCs)
(k)(1) The Manager, Transport Standards Staff, ANM-110, FAA, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. Send information to an individual
identified in either paragraph (k)(1)(i) or (k)(1)(ii) of this AD.
(i) Jeff Gardlin, Aerospace Engineer, Cabin Safety Branch, ANM-
115, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone (425) 227-2136; fax (425)
227-1149; e-mail [email protected].
(ii) Robert Hettman, Aerospace Engineer, Propulsion and
Mechanical Systems Branch, ANM-112, FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-2683; fax (425) 227-1149; e-mail
[email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector or, lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
Exact source excerpt. Text positions 13470–14695, end exclusive, in the original decoded publication. SHA-256: 16705ec0a4c18448f0ec449b5845ebe5f7027b222a91cd82a19e8abf3cba31a5
Contact Information
Contact Information
(l) For technical information about this AD, contact:
(1) Jeff Gardlin, Aerospace Engineer, Cabin Safety Branch, ANM-
115, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone (425) 227-2136; fax (425)
227-1149; e-mail [email protected].
(2) Robert Hettman, Aerospace Engineer, Propulsion and
Mechanical Systems Branch, ANM-112, FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-2683; fax (425) 227-1149; e-mail
[email protected].
(m) For FAA Flight Standards information about this AD, contact
the manager at your local certificate management office (CMO) or
certificate management team (CMT).
Exact source excerpt. Text positions 14695–15444, end exclusive, in the original decoded publication. SHA-256: 05b36642bc691374841d05fc404137bb848d5c3570fef1234b71dce107f26f68
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2011-04-09 · 1 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: b7f150c546deb0a04d6600e28d62f3aaa5c2039ce468ad08823c7ea23b55a3cf. Source manifest: ca54abaea6ee228b4d82c755e3e6fefcdbc448724b5f095667508e23f60e5ef4.
Official source · 2011-03-08
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 76, Number 45 (Tuesday, March 8, 2011)]
[Rules and Regulations]
[Pages 12556-12558]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-5292]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-0157; Directorate Identifier 2010-NM-261-AD;
Amendment 39-16630; AD 2011-04-09]
RIN 2120-AA64
Airworthiness Directives; Various Transport Category Airplanes
Equipped With Chemical Oxygen Generators Installed in a Lavatory
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: This document publishes in the Federal Register an amendment
adopting airworthiness directive (AD) 2011-04-09 that was sent
previously by individual notices to the known U.S. owners and operators
of affected airplanes identified above. This AD requires modifying the
chemical oxygen generators in the lavatory. This AD was prompted by
reports that the current design of these oxygen generators presents a
hazard that could jeopardize flight safety. We are issuing this AD to
eliminate this hazard.
DATES: This AD becomes effective March 14, 2011 to all persons except
those persons to whom it was made immediately effective by AD 2011-04-
09, which contained the requirements of this amendment.
We must receive comments on this AD by April 22, 2011.
ADDRESSES: You may send comments by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> 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.
<bullet> 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.
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 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: Jeff Gardlin, Aerospace Engineer,
Cabin Safety Branch, ANM-115, FAA, Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington 98057-3356; telephone 425-227-
2136; fax 425-227-1149; e-mail [email protected]; or
Robert Hettman, Aerospace Engineer, Propulsion and Mechanical
Systems Branch, ANM-112, FAA, Transport Airplane Directorate, 1601 Lind
Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-2683;
fax (425) 227-1149; e-mail [email protected].
SUPPLEMENTARY INFORMATION: On February 10, 2011, we issued AD 2011-04-
09, which applies to certain passenger-carrying transport category
airplanes operating in 14 CFR part 121 air carrier service; or U.S.-
registered and operating under 14 CFR part 129, with a maximum
passenger capacity of 20 or greater; and equipped with any chemical
oxygen generator installed in any lavatory.
Background
This AD was prompted by reports that the current design of these
oxygen generators presents a hazard that could jeopardize flight
safety. We are issuing this AD to eliminate this hazard.
FAA's Determination and Requirements of This AD
Since the unsafe condition described is likely to exist or develop
on other airplanes of the same type design, we issued AD 2011-04-09 to
eliminate a hazard with chemical oxygen generators in the lavatory,
which, if not corrected, could jeopardize flight safety. The AD
requires either activating all chemical oxygen generators in the
lavatories until the generator oxygen supply is expended, or removing
the oxygen generator(s); and, for each chemical oxygen generator, after
the generator is expended (or removed), removing or re-stowing the
oxygen masks and closing the mask dispenser door.
We have determined that notice and opportunity for prior public
comment on AD 2011-04-09 were contrary to the public interest, and good
cause existed to make the AD effective immediately by individual
notices issued on February 10, 2011, to the known U.S. owners and
operators of certain passenger-carrying transport category airplanes
operating in 14 CFR part 121 air carrier service; or U.S.-registered
and operating under 14 CFR part 129, with a maximum passenger capacity
of 20 or greater; and equipped with any chemical oxygen generator
installed in any lavatory.
These conditions still exist, and the AD is hereby published in the
Federal Register as an amendment to section 39.13 of the Federal
Aviation Regulations (14 CFR 39.13) to make it effective to all
persons.
Differences Between This Federal Register Version and the Individual
Notices
This Federal Register version of the AD is different from the
individual notices previously issued. These individual notices
contained a time-limited flight crew notification procedure. This
procedure required that the pilot in command be notified that the
oxygen generators in the lavatories had been rendered inoperative, and
instructed the pilot in command to brief the crew that in the event of
a rapid
[[Page 12557]]
decompression the lavatories needed to be checked. Since flight crews
have been made aware of this AD by the actions in the individual
notices, and these procedures were to be applied for a limited time (30
days) only, the procedures are considered no longer necessary, and are
not included in this AD. Flight crews are still made aware of
corrective actions taken as a result of this AD since maintenance
activities are recorded and available to the flight crew using existing
maintenance procedures.
Related Rulemaking
We are currently planning to issue a special Federal Aviation
Regulation (SFAR) to address the regulatory compliance issues resulting
from carrying out the actions required by this AD until the type
certification and operational rules are modified.
This AD is applicable to U.S.-registered transport category
airplanes operating under 14 CFR part 129 as identified in paragraph
(c) of this AD. We will monitor actions taken by other airworthiness
authorities to implement the requirements of this AD into their own
fleets to determine if additional rulemaking actions are necessary.
Action by the State of Design
This AD is applicable to all transport category airplanes
identified in paragraph (c) of this AD. For the purposes of the FAA's
responsibility to notify other airworthiness authorities of continued
airworthiness issues under International Civil Aviation Organization
(ICAO) Annex 8, this AD is considered an action by the State of Design
for United States products.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2011-0157; Directorate Identifier 2010-NM-261-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this 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 AD.
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
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.
List of Subjects in 14 CFR Part 39
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 39--AIRWORTHINESS DIRECTIVES
0
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]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2011-04-09 Transport Category Airplanes: Amendment 39-16630. Docket
No. FAA-2011-0157; Directorate Identifier 2010-NM-261-AD.
Effective Date
(a) This AD becomes effective March 14, 2011, to all persons
except those persons to whom it was made immediately effective by AD
2011-04-09, issued on February 10, 2011, which contained the
requirements of this amendment.
Affected ADs
(b) None.
Applicability
(c) This AD applies to transport category airplanes, in
passenger-carrying operations, that are equipped with any chemical
oxygen generator installed in any lavatory, and are:
(1) Operating under 14 CFR part 121; or
(2) U.S.-registered and operating under 14 CFR part 129, with a
maximum passenger capacity of 20 or greater.
Subject
(d) Joint Aircraft System Component (JASC)/Air Transport
Association (ATA) of America Code 35, Oxygen.
Unsafe Condition
(e) This AD was prompted by reports that the current design of
chemical oxygen generators in the lavatories presents a hazard that
could jeopardize flight safety. We are issuing this AD to eliminate
this hazard.
Compliance
(f) Comply with this AD within the compliance times specified,
unless already done.
Oxygen Generator Deactivation
(g) Within 21 days after the effective date of this AD, do the
actions specified in paragraphs (g)(1) and (g)(2) of this AD.
(1) Activate all chemical oxygen generators in the lavatories
until the generator oxygen supply is expended. An operator may also
remove the oxygen generator(s), in accordance with existing
maintenance practice, in lieu of activating it.
(2) For each chemical oxygen generator, after the generator is
expended (or removed), remove or re-stow the oxygen masks and close
the mask dispenser door.
Note 1: Chemical oxygen generators are considered a hazardous
material and subject to specific requirements under Title 49 CFR for
shipping. Oxygen generators must be expended prior to disposal but
are considered a hazardous waste; therefore, disposal must be in
accordance with all Federal, State, and local regulations. Expended
oxygen generators are forbidden in air transportation as cargo. For
more information, contact 1-800-HMR-4922.
[[Page 12558]]
Note 2: Design approval holders are not expected to release
service instructions for this action.
Compliance with Federal Aviation Regulations
(h) Notwithstanding the requirements of Sections 25.1447,
121.329, 121.333, and 129.13 of the Federal Aviation Regulations (14
CFR 25.1447, 121.329, 121.333, and 129.13), operators complying with
this AD are authorized to operate affected airplanes until this
action is superseded by other rulemaking.
Parts Installation
(i) After the effective date of this AD, no person may install a
chemical oxygen generator in any lavatory on any affected airplane.
Special Flight Permit
(j) Special flight permits, as described in Section 21.197 and
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197
and 21.199), are not allowed.
Alternative Methods of Compliance (AMOCs)
(k)(1) The Manager, Transport Standards Staff, ANM-110, FAA, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. Send information to an individual
identified in either paragraph (k)(1)(i) or (k)(1)(ii) of this AD.
(i) Jeff Gardlin, Aerospace Engineer, Cabin Safety Branch, ANM-
115, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone (425) 227-2136; fax (425)
227-1149; e-mail [email protected].
(ii) Robert Hettman, Aerospace Engineer, Propulsion and
Mechanical Systems Branch, ANM-112, FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-2683; fax (425) 227-1149; e-mail
[email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector or, lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
Contact Information
(l) For technical information about this AD, contact:
(1) Jeff Gardlin, Aerospace Engineer, Cabin Safety Branch, ANM-
115, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone (425) 227-2136; fax (425)
227-1149; e-mail [email protected].
(2) Robert Hettman, Aerospace Engineer, Propulsion and
Mechanical Systems Branch, ANM-112, FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-2683; fax (425) 227-1149; e-mail
[email protected].
(m) For FAA Flight Standards information about this AD, contact
the manager at your local certificate management office (CMO) or
certificate management team (CMT).
Issued in Renton, Washington, on March 2, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-5292 Filed 3-7-11; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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