AD 2018-25-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; C Series Aircraft Limited Partnership (CSALP) (Type Certificate Previously Held by Bombardier, Inc.) Airplanes |
| aircraft | Bombardier | Various | Airworthiness Directives; C Series Aircraft Limited Partnership (CSALP) (Type Certificate Previously Held by Bombardier, Inc.) Airplanes |
Unsafe Condition
Dislodged cargo compartment blow-out panels create openings in the forward and aft cargo compartments. In the event of a cargo compartment fire, these unintended openings in the forward and aft cargo compartments would provide a path for smoke, fire, and Halon to enter the adjacent equipment bays, flight deck, and passenger cabin, which could delay smoke detection in the forward and aft cargo compartments and result in the forward and aft cargo compartments not being able to maintain Halon concentration required for fire suppression.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitive inspections for any dislodged blow-out panel in the forward and aft cargo compartments, reporting of the inspection findings, and reinstallation if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
C Series Aircraft Limited Partnership (CSALP) Model BD-500-1A10 and BD-500-1A11 airplanes.
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 C Series Aircraft Limited Partnership (CSALP) Model BD-500-1A10 and BD- 500-1A11 airplanes. This AD was prompted by reports of dislodged cargo compartment blowout panels. This AD requires repetitive inspections for any dislodged blow-out panel in the forward and aft cargo compartments, reporting of the inspection findings, and reinstallation if necessary. We are issuing this AD to address the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to C Series Aircraft Limited Partnership (CSALP)
(Type Certificate Previously Held by Bombardier, Inc.) airplanes,
certificated in any category, identified in paragraphs (c)(1) and
(c)(2) of this AD.
(1) Model BD-500-1A10 airplanes, serial numbers 50001 and
subsequent, equipped with blow-out panel part number D762213-503,
D762216-505, or D762209-503.
(2) Model BD-500-1A11 airplanes, serial numbers 55001 and
subsequent, equipped with blow-out panel part number D762213-503,
D762216-505, or D762209-503.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 83, Number 236 (Monday, December 10, 2018)]
[Rules and Regulations]
[Pages 63397-63399]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2018-26473]
[[Page 63397]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-0799; Product Identifier 2018-NM-117-AD; Amendment
39-19515; AD 2018-25-04]
RIN 2120-AA64
Airworthiness Directives; C Series Aircraft Limited Partnership
(CSALP) (Type Certificate Previously Held by Bombardier, Inc.)
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
C Series Aircraft Limited Partnership (CSALP) Model BD-500-1A10 and BD-
500-1A11 airplanes. This AD was prompted by reports of dislodged cargo
compartment blowout panels. This AD requires repetitive inspections for
any dislodged blow-out panel in the forward and aft cargo compartments,
reporting of the inspection findings, and reinstallation if necessary.
We are issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective January 14, 2019.
The Director of the Federal Register approved the incorporation by
reference of certain publication listed in this AD as of January 14,
2019.
ADDRESSES: For service information identified in this final rule,
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#582c303c763b2a3218393d2a37763a37353a392a3c313d2a763b3735"><span class="__cf_email__" data-cfemail="13677b773d706179537276617c3d717c7e717261777a76613d707c7e">[email protected]</span></a>; internet <a href="http://www.bombardier.com">http://www.bombardier.com</a>. You may view this service information at the FAA,
Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call 206-
231-3195. It is also available on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2018-
0799.
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> by searching for and locating Docket No. FAA-2018-
0799; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations (phone: 800-647-
5527) is 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: Darren Gassetto, Aerospace Engineer,
Mechanical Systems and Admin Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone
516-228-7323; fax 516 794 5531; email <a href="/cdn-cgi/l/email-protection#30091d5146431d5e4951535f1d535f43705651511e575f46"><span class="__cf_email__" data-cfemail="61584c0017124c0f1800020e4c020e12210700004f060e17">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain C Series Aircraft
Limited Partnership (CSALP) Model BD-500-1A10 and BD-500-1A11
airplanes. The NPRM published in the Federal Register on September 19,
2018 (83 FR 47315). The NPRM was prompted by reports of dislodged cargo
compartment blowout panels. The NPRM proposed to require repetitive
inspections for any dislodged blow-out panel in the forward and aft
cargo compartments, reporting of the inspection findings, and
reinstallation if necessary.
We are issuing this AD to address dislodged cargo compartment blow-
out panels, which could result in openings in the forward and aft cargo
compartments. In the event of a cargo compartment fire, these
unintended openings in the forward and aft cargo compartments would
provide a path for smoke, fire, and Halon to enter the adjacent
equipment bays, flight deck, and passenger cabin, which could delay
smoke detection in the forward and aft cargo compartments and result in
the forward and aft cargo compartments not being able to maintain the
Halon concentration required for fire suppression. The cargo
compartment fire may become uncontrollable if this condition is not
addressed, which could result in the loss of controllability of the
airplane.
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2018-15, dated June 6,
2018 (referred to after this as the Mandatory Continuing Airworthiness
Information, or ``the MCAI''), to correct an unsafe condition for
certain C Series Aircraft Limited Partnership (CSALP) Model BD-500-1A10
and BD-500-1A11 airplanes. The MCAI states:
Multiple events of dislodged cargo compartment blow-out panels
have been reported in-service. It was determined that these events
were caused by baggage impacting the cargo panel cage, or the cargo
compartment liner below the cargo panel cage, during baggage loading
and unloading on the ground, or during flight due to shifting
luggage.
Dislodged cargo compartment blow-out panels create openings in
the forward and aft cargo compartments. In the event of a cargo
compartment fire, these unintended openings in the forward and aft
cargo compartments would provide a path for smoke, fire, and Halon
to enter the adjacent equipment bays, flight deck, and passenger
cabin, which could delay smoke detection in the forward and aft
cargo compartments and result in the forward and aft cargo
compartments not being able to maintain Halon concentration required
for fire suppression. The cargo compartment fire may become
uncontrollable if this condition is not corrected.
This [TCCA] AD mandates repetitive [detailed] inspections of the
affected forward and aft cargo compartment blow-out panels, and
reporting of inspection findings where dislodged blow-out panels
have been found [and re-installation of dislodged blow-out panels].
You may examine the MCAI in the AD docket on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA 2018
0799.
Comments
We gave the public the opportunity to participate in developing
this final rule. We received no comments on the NPRM or on the
determination of the cost to the public.
Change to Product Name
The type certificate holder for Model BD-500-1A10 and BD-500-1A11
airplanes has changed from ``Bombardier, Inc.,'' to ``C Series Aircraft
Limited Partnership (CSALP).'' We have revised this AD accordingly.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting this final rule with the change
described previously and minor editorial changes. We have determined
that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this final
rule.
[[Page 63398]]
Related Service Information Under 1 CFR Part 51
Bombardier has issued C Series Data Module BD500-A-J50-10-01-01AAA-
310B-A, ``Forward and aft cargo compartment blow-out panels--Visual
check,'' Issue 002, dated May 16, 2018. This service information
describes procedures for an inspection for any dislodged blow-out panel
in the forward and aft cargo compartments.
Bombardier has issued C Series Data Module BD500-A-J50-10-01-00AAA-
521A-A, ``Decompression panels dislodging--Return to basic
configuration,'' Issue 002, dated May 16, 2018. This service
information describes procedures for re-installation of dislodged
forward and aft cargo compartment blow-out panels.
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Costs of Compliance
We estimate that this affects 21 airplanes of U.S. registry. We
estimate the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85............................. $0 $85 $1,785
----------------------------------------------------------------------------------------------------------------
We estimate the following costs to do any necessary on-condition
action that would be required based on the results of any required
actions. We have no way of determining the number of aircraft that
might need this on-condition action:
Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
Cost per
Labor cost Parts cost product
------------------------------------------------------------------------
2 work-hours x $85 per hour = $170.............. $0 $170
------------------------------------------------------------------------
We estimate that it would take about 1 work-hour per product to
comply with the on-condition reporting requirement in this AD. The
average labor rate is $85 per hour. Based on these figures, we estimate
the cost of reporting the inspection results on U.S. operators to be
$85 per product.
Paperwork Reduction Act
A federal agency may not conduct or sponsor, and a person is not
required to respond to, nor shall a person be subject to penalty for
failure to comply with a collection of information subject to the
requirements of the Paperwork Reduction Act unless that collection of
information displays a current valid OMB control number. The control
number for the collection of information required by this AD is 2120-
0056. The paperwork cost associated with this AD has been detailed in
the Costs of Compliance section of this document and includes time for
reviewing instructions, as well as completing and reviewing the
collection of information. Therefore, all reporting associated with
this AD is mandatory. Comments concerning the accuracy of this burden
and suggestions for reducing the burden should be directed to the FAA
at 800 Independence Ave. SW, Washington, DC 20591, ATTN: Information
Collection Clearance Officer, AES-200.
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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes and
associated appliances to the Director of the System Oversight Division.
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 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.
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):
2018-25-04 C Series Aircraft Limited Partnership (CSALP) (Type
Certificate Previously Held by Bombardier, Inc.): Amendment 39-
19515; Docket No. FAA-2018-0799; Product Identifier 2018-NM-117-AD.
[[Page 63399]]
(a) Effective Date
This AD is effective January 14, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to C Series Aircraft Limited Partnership (CSALP)
(Type Certificate Previously Held by Bombardier, Inc.) airplanes,
certificated in any category, identified in paragraphs (c)(1) and
(c)(2) of this AD.
(1) Model BD-500-1A10 airplanes, serial numbers 50001 and
subsequent, equipped with blow-out panel part number D762213-503,
D762216-505, or D762209-503.
(2) Model BD-500-1A11 airplanes, serial numbers 55001 and
subsequent, equipped with blow-out panel part number D762213-503,
D762216-505, or D762209-503.
(d) Subject
Air Transport Association (ATA) of America Code 50, Cargo and
accessory compartment.
(e) Reason
This AD was prompted by reports of dislodged cargo compartment
blow-out panels. We are issuing this AD to address this condition,
which could result in openings in the forward and aft cargo
compartments. In the event of a cargo compartment fire, these
unintended openings in the forward and aft cargo compartments would
provide a path for smoke, fire, and Halon to enter the adjacent
equipment bays, flight deck, and passenger cabin, which could delay
smoke detection in the forward and aft cargo compartments and result
in the forward and aft cargo compartments not being able to maintain
the Halon concentration required for fire suppression. The cargo
compartment fire may become uncontrollable if this condition is not
addressed, which could result in the loss of controllability of the
airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Repetitive Inspections of the Forward and Aft Cargo Compartment
Blow-Out Panels and Re-Installation
Within 7 days or 50 flight cycles, whichever occurs first, after
the effective date of this AD, do a detailed inspection for any
dislodged blow-out panel in the forward and aft cargo compartments,
in accordance with C Series (Bombardier) Data Module BD500-A-J50-10-
01-01AAA-310B-A, ``Forward and aft cargo compartment blow-out
panels--Visual check,'' Issue 002, dated May 16, 2018. Re-install
all dislodged forward and aft cargo compartment blow-out panels
before further flight, in accordance with C Series (Bombardier) Data
Module BD500-A-J50-10-01-00AAA-521A-A, ``Decompression panels
dislodging--Return to basic configuration,'' Issue 002, dated May
16, 2018. Thereafter, at intervals not to exceed 100 flight cycles,
repeat the detailed inspection for any dislodged blow-out panel in
the forward and aft cargo compartments.
(h) Reporting
If any blow-out panel in the forward or aft cargo compartments
is found dislodged during any inspection required by paragraph (g)
of this AD, at the applicable time specified in paragraph (h)(1) or
(h)(2) of this AD, report findings to the Bombardier customer
response center (CRC) via email: <a href="/cdn-cgi/l/email-protection#98fbeafbc7fbebfdeaf1fdebd8f9fdeaf7b6faf7f5faf9eafcf1fdeab6fbf7f5"><span class="__cf_email__" data-cfemail="accfdecff3cfdfc9dec5c9dfeccdc9dec382cec3c1cecddec8c5c9de82cfc3c1">[email protected]</span></a>.
Reportable findings include the airplane serial number on which any
dislodged blow-out panel was found, the date of inspection, and the
part number and location of each dislodged blow-out panel.
(1) If the inspection was done on or after the effective date of
this AD: Submit the report within 30 days after the inspection.
(2) If the inspection was done before the effective date of this
AD: Submit the report within 30 days after the effective date of
this AD.
(i) Paperwork Reduction Act Burden Statement
A federal agency may not conduct or sponsor, and a person is not
required to respond to, nor shall a person be subject to a penalty
for failure to comply with a collection of information subject to
the requirements of the Paperwork Reduction Act unless that
collection of information displays a current valid OMB Control
Number. The OMB Control Number for this information collection is
2120-0056. Public reporting for this collection of information is
estimated to be approximately 1 hour per response, including the
time for reviewing instructions, completing and reviewing the
collection of information. All responses to this collection of
information are mandatory. Comments concerning the accuracy of this
burden and suggestions for reducing the burden should be directed to
the FAA at: 800 Independence Ave. SW, Washington, DC 20591, Attn:
Information Collection Clearance Officer, AES-200.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO Branch, 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 manager of the certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 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.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or Transport Canada Civil Aviation (TCCA); or C Series
Aircraft Limited Partnership's (CSALP's) TCCA Design Approval
Organization (DAO). If approved by the DAO, the approval must
include the DAO-authorized signature.
(k) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian AD CF-2018-15, dated June 6, 2018, for related
information. This MCAI may be found in the AD docket on the internet
at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket
No. FAA-2018-0799.
(2) For more information about this AD, contact Darren Gassetto,
Aerospace Engineer, Mechanical Systems and Admin Services Section,
FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516-228-7323; fax 516 794 5531; email <a href="/cdn-cgi/l/email-protection#4f76622e393c6221362e2c20622c203c0f292e2e61282039"><span class="__cf_email__" data-cfemail="7f46521e090c5211061e1c10521c100c3f191e1e51181009">[email protected]</span></a>.
(l) 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 this AD specifies otherwise.
(i) C Series (Bombardier) Data Module BD500-A-J50-10-01-00AAA-
521A-A, ``Decompression panels dislodging--Return to basic
configuration,'' Issue 002, dated May 16, 2018.
(ii) C Series (Bombardier) Data Module BD500-A-J50-10-01-01AAA-
310B-A, ``Forward and aft cargo compartment blow-out panels--Visual
check,'' Issue 002, dated May 16, 2018.
(3) 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#5b2f333f753829311b3a3e293475393436393a293f323e2975383436"><span class="__cf_email__" data-cfemail="e89c808cc68b9a82a8898d9a87c68a87858a899a8c818d9ac68b8785">[email protected]</span></a>; internet <a href="http://www.bombardier.com">http://www.bombardier.com</a>.
(4) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Des Moines, Washington, on November 23, 2018.
John P. Piccola,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-26473 Filed 12-7-18; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.