AD 2012-13-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-600-2B19 (Regional Jet Series 100) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B19 (Regional Jet Series 440) | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Damage to the third crew person oxygen line and oxygen escaping from it, which could feed a fire in the vicinity of an electrical panel.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the flexible oxygen hose of the third crew person oxygen line with a new hose and change its routing. Modify the entrance compartment assembly in accordance with Bombardier Service Bulletin 601R-35-017, Revision A.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 4,000 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes equipped with entrance compartment assemblies having part numbers that begin with A281001, A282001, A283001, A284001, 4591001, 4592001, 4593001, or 4594001.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD was prompted by a report of a ground fire which was fed by oxygen escaping from a damaged third crew person oxygen line and had started in the vicinity of an electrical panel. This AD requires replacing and changing the routing of the flexible oxygen hose of the third crew person oxygen line and modifying the entrance compartment assembly. We are issuing this AD to prevent the possibility of damage to the third crew person oxygen line and of an oxygen-fed fire in the airplane.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Bombardier, Inc. Model CL-600-2B19 (Regional
Jet Series 100 & 440) airplanes; certificated in any category;
equipped with entrance compartment assembly having part numbers that
begin with A281001, A282001, A283001, A284001, 4591001, 4592001,
4593001, or 4594001.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 77, Number 125 (Thursday, June 28, 2012)]
[Rules and Regulations]
[Pages 38468-38470]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2012-15602]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0034; Directorate Identifier 2011-NM-153-AD;
Amendment 39-17105; AD 2012-13-03]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440)
airplanes. This AD was prompted by a report of a ground fire which was
fed by oxygen escaping from a damaged third crew person oxygen line and
had started in the vicinity of an electrical panel. This AD requires
replacing and changing the routing of the flexible oxygen hose of the
third crew person oxygen line and modifying the entrance compartment
assembly. We are issuing this AD to prevent the possibility of damage
to the third crew person oxygen line and of an oxygen-fed fire in the
airplane.
DATES: This AD becomes effective August 2, 2012.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 2,
2012.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New
York 11590; telephone (516) 228-7318; fax (516) 794-5531.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on January 23, 2012 (77
FR 3184). That NPRM proposed to correct
[[Page 38469]]
an unsafe condition for the specified products. The MCAI states:
An operator has reported a ground fire in the CL-600-2B19
aeroplane. The fire burnt an 18 inch hole through the left upper
fuselage skin panel in the cockpit area. The fire started in the
vicinity of the Junction Box 1 (JB1) electrical panel, and was fed
by oxygen escaping from a damaged third crewman oxygen line.
This [Transport Canada Civil Aviation (TCCA)] Airworthiness
Directive (AD) was issued to prevent the possibility of damage to
the third crewman oxygen line and an oxygen fed fire in the
aeroplane.
You may obtain further information by examining the MCAI in the AD
docket.
Comments
We gave the public the opportunity to participate in developing
this AD. We have considered the comments received.
Support for the NPRM (77 FR 3184, January 23, 2012)
Air Line Pilots Association, International (ALPA) stated that the
proposed actions will enhance safety and that it supports the intent of
the NPRM (77 FR 3184, January 23, 2012).
Request To Shorten the Compliance Time and Add an Inspection
The ALPA requested that an initial inspection of the oxygen hose be
performed within 500 flight hours after the effective date of the AD
and immediate replacement of any damaged hoses. The commenter also
requested that the compliance time for the replacement specified in the
NPRM (77 FR 3184, January 23, 2012) of ``within 4,000 flight hours
after the effective date of the AD.'' be reduced to ``within 2000
flight hours after the effective date of this AD.''
We do not agree to add an inspection to the requirements of this
AD. We have determined that accomplishing the replacement required by
paragraph (g) of this AD addresses the identified unsafe condition. We
have not changed the AD in this regard.
We, also, do not agree with the request for a shorter compliance
time. In developing the compliance time, we determined that the
compliance time of 4,000 flight hours after the effective date of the
AD is appropriate considering the safety implications, the average
utilization rate of the affected fleet, the practical aspects of an
orderly inspection of the fleet during regular maintenance periods, and
the availability of required replacement parts. In addition, the
proposed compliance time corresponds with the compliance time of the
parallel AD issued by TCCA. Operators may request approval of an
alternative method of compliance (AMOC) under the provisions of
paragraph (i)(1) of this AD. We have not changed the AD in this regard.
Request To Revise Wording
Air Wisconsin requested that the wording in paragraph (h) of the
NPRM (77 FR 3184, January 23, 2012) be changed from ``modify'' to
``discard'' as Bombardier Service Bulletin 601R-35-017, Revision A,
dated June 9, 2011, states in various places to discard the hose.
We partially agree. The wording in paragraph (h) of the NPRM (77 FR
3184, January 23, 2012) incorrectly implied that both the entrance
compartment assembly and the flexible oxygen hose could be modified. We
have changed paragraphs (g) and (h) of this AD to clarify that the
entrance compartment assembly is ``modified'' and that the flexible
oxygen hose is ``replaced with a new flexible oxygen hose.''
Conclusion
We reviewed the available data, including the comments received,
and determined that air safety and the public interest require adopting
the AD with the changes described previously--except for minor
editorial changes. We have determined that these changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (77 FR 3184, January 23, 2012) for correcting the unsafe
condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (77 FR 3184, January 23, 2012).
Costs of Compliance
We estimate that this AD will affect 588 products of U.S. registry.
We also estimate that it will take about 13 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts will cost about $108 per product.
Where the service information lists required parts costs that are
covered under warranty, we have assumed that there will be no charge
for these parts. As we do not control warranty coverage for affected
parties, some parties may incur costs higher than estimated here. Based
on these figures, we estimate the cost of this AD to the U.S. operators
to be $713,244, or $1,213 per product.
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 determined that 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 the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. 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 AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a>; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM (77 FR 3184, January 23,
2012), the regulatory evaluation, any comments received, and other
information. The street address for the Docket Operations office
(telephone (800) 647-5527) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
[[Page 38470]]
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 AD:
2012-13-03 Bombardier, Inc.: Amendment 39-17105. Docket No. FAA-
2012-0034; Directorate Identifier 2011-NM-153-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective August 2,
2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model CL-600-2B19 (Regional
Jet Series 100 & 440) airplanes; certificated in any category;
equipped with entrance compartment assembly having part numbers that
begin with A281001, A282001, A283001, A284001, 4591001, 4592001,
4593001, or 4594001.
(d) Subject
Air Transport Association (ATA) of America Code 35: Oxygen.
(e) Reason
This AD was prompted by a report of a ground fire which was fed
by oxygen escaping from a damaged third crew person oxygen line and
had started in the vicinity of an electrical panel. We are issuing
this AD to prevent the possibility of damage to the third crew
person oxygen line and of an oxygen-fed fire in the airplane.
(f) Compliance
You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.
(g) Actions
Within 4,000 flight hours after the effective date of this AD,
change the routing and replace the flexible oxygen hose of the third
crew person oxygen line with a new flexible oxygen hose and modify
the entrance compartment assembly, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 601R-35-
017, Revision A, dated June 9, 2011.
(h) Parts Installation
As of the effective date of this AD, no person may install an
entrance compartment assembly having a part number that begins with
A281001, A282001, A283001, A284001, 4591001, 4592001, 4593001, or
4594001, or a flexible oxygen hose having a part number 38027-0260,
on any airplane, unless that entrance compartment assembly has been
modified and the flexible oxygen hose has been replaced with a new
flexible oxygen hose, in accordance with the Accomplishment
Instructions of Bombardier Service Bulletin 601R-35-017, Revision A,
dated June 9, 2011.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office (ACO), ANE-170, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the ACO, send it to ATTN: Program Manager, Continuing
Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite
410, Westbury, New York 11590; telephone 516-228-7300; fax 516-794-
5531. 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. The AMOC approval letter must specifically
reference this AD.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(j) Related Information
Refer to MCAI Canadian Airworthiness Directive CF-2011-23, dated
July 14, 2011; and Bombardier Service Bulletin 601R-35-017, Revision
A, dated June 9, 2011; for related information.
(k) Material Incorporated by Reference
(1) You must use the following service information to do the
actions required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference (IBR) of the following service information under 5 U.S.C.
552(a) and 1 CFR part 51:
(i) Bombardier Service Bulletin 601R-35-017, Revision A, dated
June 9, 2011.
(2) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; email <a href="/cdn-cgi/l/email-protection#a1d5c9c58fc2d3cbe1c0c4d3ce8fc3ceccc3c0d3c5c8c4d38fc2cecc"><span class="__cf_email__" data-cfemail="ea9e828ec4899880aa8b8f9885c4888587888b988e838f98c4898587">[email protected]</span></a>; Internet <a href="http://www.bombardier.com">http://www.bombardier.com</a>.
(3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton,
Washington. For information on the availability of this material at
the FAA, call 425-227-1221.
(4) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at an NARA facility, call 202-741-6030, or go to <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.
Issued in Renton, Washington, on June 19, 2012.
John P. Piccola,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-15602 Filed 6-27-12; 8:45 am]
BILLING CODE 4910-13-P
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