AD 2012-17-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | Jetstream Model 4101 | Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes |
Unsafe Condition
The fire extinguisher bottle part number BA20509AM-4, when mounted horizontally in the toilet vanity unit, may not fully discharge extinguishant in the event of a fire, potentially leading to fire propagation in the toilet waste bin, damage to the airplane, and injury to occupants.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect to determine if fire extinguisher bottle part number BA20509AM-4 is installed. If installed, reposition the fire extinguisher bottle to a vertical orientation in accordance with BAE SYSTEMS (Operations) Limited Service Bulletin J41-26-008, Revision 2, dated September 20, 2011.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 2 months after the effective date of the AD, with repositioning completed before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BAE SYSTEMS (Operations) Limited Model 4101 airplanes, all serial numbers.
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 all BAE SYSTEMS (Operations) Limited Model 4101 airplanes. This AD was prompted by reports that the fire extinguisher in the toilet vanity unit needs to be mounted vertically rather than horizontally. This AD requires inspecting to determine if a certain fire extinguisher bottle is installed, and repositioning the affected fire extinguisher bottle to the vertical position. We are issuing this AD to detect and correct the orientation of the fire extinguisher bottle in the toilet vanity unit to the vertical position, which if not corrected, could result in a toilet waste bin fire spreading, and consequent damage to the airplane and injury to its occupants.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to BAE SYSTEMS (Operations) Limited Model 4101
airplanes, certificated in any category, all serial numbers.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 77, Number 173 (Thursday, September 6, 2012)]
[Rules and Regulations]
[Pages 54803-54804]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2012-21288]
[[Page 54803]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0489; Directorate Identifier 2011-NM-229-AD;
Amendment 39-17174; AD 2012-17-11]
RIN 2120-AA64
Airworthiness Directives; BAE SYSTEMS (Operations) Limited
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 all BAE
SYSTEMS (Operations) Limited Model 4101 airplanes. This AD was prompted
by reports that the fire extinguisher in the toilet vanity unit needs
to be mounted vertically rather than horizontally. This AD requires
inspecting to determine if a certain fire extinguisher bottle is
installed, and repositioning the affected fire extinguisher bottle to
the vertical position. We are issuing this AD to detect and correct the
orientation of the fire extinguisher bottle in the toilet vanity unit
to the vertical position, which if not corrected, could result in a
toilet waste bin fire spreading, and consequent damage to the airplane
and injury to its occupants.
DATES: This AD becomes effective October 11, 2012.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 11,
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 20590.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: (425) 227-1175;
fax: (425) 227-1149.
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 May 21, 2012 (77 FR
29914). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
The Jetstream 4100 is equipped with a fire extinguisher that, if
a fire is detected, discharges into the waste bin located within the
toilet vanity unit.
On the majority of aeroplanes, the furnishing vendor's original
design installs the fire extinguisher bottle part number (P/N)
BA20509AM-4 in a horizontal position within the vanity unit. BAE
Systems have subsequently been informed by the fire extinguisher
manufacturer that the fire extinguisher bottle should be mounted
vertically, as its operation cannot be guaranteed when mounted
horizontally. In the event of a fire in the waste bin the
extinguishant may not fully discharge from the fire extinguisher
bottle.
This condition, if not corrected, could result in a toilet waste
bin fire propagation and consequent damage to the aeroplane and/or
injury to its occupants.
For the reasons described above, this [European Aviation Safety
Agency (EASA)] AD requires [an inspection to determine if a certain
fire extinguisher is installed and] the repositioning of the fire
extinguisher bottle from a horizontal orientation to a vertical
orientation.
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 received no comments on the NPRM (77 FR 29914, May 21,
2012) or on the determination of the cost to the public.
Conclusion
We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed--except for
minor editorial changes. We have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (77 FR 29914, May 21, 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 29914, May 21, 2012).
Costs of Compliance
We estimate that this AD will affect 4 products of U.S. registry.
We also estimate that it will take about 8 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 $170 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 $3,400, or 850 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 29914, May 21, 2012),
the regulatory evaluation, any
[[Page 54804]]
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.
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:
2012-17-11 BAE SYSTEMS (Operations) Limited: Amendment 39-17174.
Docket No. FAA-2012-0489; Directorate Identifier 2011-NM-229-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective October 11,
2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to BAE SYSTEMS (Operations) Limited Model 4101
airplanes, certificated in any category, all serial numbers.
(d) Subject
Air Transport Association (ATA) of America Code 26, Fire
Protection.
(e) Reason
This AD was prompted by reports that the fire extinguisher of
the toilet vanity unit needs to be mounted vertically, rather than
horizontally. We are issuing this AD to detect and correct the
orientation of the fire extinguisher bottle in the toilet vanity
unit to the vertical position, which if not corrected, could result
in a toilet waste bin fire spreading, and consequent damage to the
airplane and injury to its occupants.
(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 2 months after the effective date of this AD, determine
from the table specified in paragraph 2.A.(1) of BAE SYSTEMS
(Operations) Limited Service Bulletin J41-26-008, Revision 2, dated
September 20, 2011, if fire extinguisher bottle part number (P/N)
BA20509AM-4 is fitted to the airplane. If a fire extinguisher bottle
P/N BA20509AM-4 is fitted, before further flight, reposition the
fire extinguisher bottle, in accordance with the Accomplishment
Instructions of BAE SYSTEMS (Operations) Limited Service Bulletin
J41-26-008, Revision 2, dated September 20, 2011.
(h) Credit for Previous Actions
This paragraph provides credit for the actions required by
paragraph (g) of this AD, if those actions were performed before the
effective date of this AD using BAE SYSTEMS (Operations) Limited
Service Bulletin J41-26-008, dated October 5, 2010; or BAE SYSTEMS
(Operations) Limited Service Bulletin J41-26-008, Revision 1, dated
April 12, 2011.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, 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 International Branch, send it to ATTN: Todd
Thompson, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone: (425) 227-1175; fax: (425) 227-1149.
Information may be emailed to: <a href="/cdn-cgi/l/email-protection#774e5a36393a5a4646415a363a38345a25322622322423243711161659101801"><span class="__cf_email__" data-cfemail="40796d010e0d6d7171766d010d0f036d1205111505131413002621216e272f36">[email protected]</span></a>.
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 European Aviation Safety Agency (EASA)
Airworthiness Directive 2011-0194, dated October 6, 2011; and BAE
SYSTEMS (Operations) Limited Service Bulletin J41-26-008, Revision
2, dated September 20, 2011; for related information.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) BAE SYSTEMS (Operations) Limited Service Bulletin J41-26-
008, Revision 2, dated September 20, 2011.
(ii) Reserved.
(3) For service information identified in this AD, contact BAE
SYSTEMS (Operations) Limited, Customer Information Department,
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United
Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email
<a href="/cdn-cgi/l/email-protection#96c4d7e6e3f4fafff5f7e2fff9f8e5d6f4f7f3e5efe5e2f3fbe5b8f5f9fb"><span class="__cf_email__" data-cfemail="faa8bb8a8f989693999b8e93959489ba989b9f8983898e9f9789d4999597">[email protected]</span></a>; Internet <a href="http://www.baesystems.com/Businesses/RegionalAircraft/index.htm">http://www.baesystems.com/Businesses/RegionalAircraft/index.htm</a>.
(4) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA.
For information on the availability of this material at the FAA,
call 425-227-1221.
(5) 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 August 22, 2012.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-21288 Filed 9-5-12; 8:45 am]
BILLING CODE 4910-13-P
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