AD 2021-03-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | BD-700-1A10 | Airworthiness Directives; Bombardier, Inc., Airplanes |
Unsafe Condition
smoke and signs of an overheating condition from the emergency light battery (ELB) due to excessive corrosion surrounding the internal lead acid batteries, which caused an electrical short circuit that led to the smoke and overheating condition.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
an inspection to determine the last replacement date of the ELB, and replacement if necessary, and the incorporation of a new maintenance task into the existing maintenance or inspection program.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 48 months after the last replacement date or manufacturing date of the ELB is found to be 4 years or older.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier, Inc., Model BD-700-1A10 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10 airplanes. This AD was prompted by a report of smoke and signs of an overheating condition from the emergency light battery (ELB) due to excessive corrosion surrounding the internal lead acid batteries, which caused an electrical short circuit that led to the smoke and overheating condition. This AD requires an inspection to determine the last replacement date of the ELB, and replacement if necessary. This AD also requires the incorporation of a new maintenance task into the existing maintenance or inspection program. The FAA is 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 Bombardier, Inc., Model BD-700-1A10
airplanes, certificated in any category, serial numbers 9002, 9003,
9011, 9016, 9020, 9022 through 9025 inclusive, 9029, 9031, 9032,
9036, 9039 through 9044 inclusive, 9046 through 9058 inclusive, 9060
through 9065 inclusive, 9067 through 9081 inclusive, 9083 through
9106 inclusive, 9108 through 9122 inclusive, 9124 through 9126
inclusive, 9128, 9129, 9133, 9134, 9136 through 9139 inclusive, 9141
through 9148 inclusive, 9150, 9151, 9153, 9159, 9162, 9163, 9165,
and 9169.
Document Text
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[Federal Register Volume 86, Number 34 (Tuesday, February 23, 2021)]
[Rules and Regulations]
[Pages 10747-10750]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2021-03574]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0843; Product Identifier 2020-NM-073-AD; Amendment
39-21420; AD 2021-03-17]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD-700-1A10 airplanes. This AD was
prompted by a report of smoke and signs of an overheating condition
from the emergency light battery (ELB) due to excessive corrosion
surrounding the internal lead acid batteries, which caused an
electrical short circuit that led to the smoke and overheating
condition. This AD requires an inspection to determine the last
replacement date of the ELB, and replacement if necessary. This AD also
requires the incorporation of a new maintenance task into the existing
maintenance or inspection program. The FAA is issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective March 30, 2021.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 30,
2021.
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#c5a4a6ebbcb0a985a4a0b7aaeba7aaa8a7a4b7a1aca0b7eba6aaa8"><span class="__cf_email__" data-cfemail="a5c4c68bdcd0c9e5c4c0d7ca8bc7cac8c7c4d7c1ccc0d78bc6cac8">[email protected]</span></a>; internet <a href="https://www.bombardier.com">https://www.bombardier.com</a>. You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety 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="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating
Docket No. FAA-2020-0843.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2020-
0843; 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, any comments received, and other information. The
address for Docket Operations 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: Thomas Niczky, Aerospace Engineer,
Avionics and Electrical Systems Section, FAA, New York ACO Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7347;
fax 516-794-5531; email <a href="/cdn-cgi/l/email-protection#8db4a0ecfbfea0e3f4eceee2a0eee2fecdebececa3eae2fb"><span class="__cf_email__" data-cfemail="c5fce8a4b3b6e8abbca4a6aae8a6aab685a3a4a4eba2aab3">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Discussion
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2020-07, dated March
17, 2020 (also referred to as the Mandatory Continuing Airworthiness
Information, or the MCAI), to correct an unsafe condition for certain
Bombardier, Inc., Model BD-700-1A10 airplanes. You may examine the MCAI
in the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by
searching for and locating Docket No. FAA-2020-0843.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Bombardier,
Inc., Model BD-700-1A10 airplanes. The NPRM published in the Federal
Register on September 17, 2020 (85 FR 58010). The NPRM was prompted by
a report of smoke and signs of an overheating condition from the ELB
due to excessive corrosion surrounding the internal lead acid
batteries, which caused an electrical short circuit that led to the
smoke and overheating condition. The NPRM proposed to require an
inspection to determine the last replacement date of the ELB, and
replacement if necessary. The NPRM also proposed to require the
incorporation of a new maintenance task into the existing maintenance
or inspection program. The FAA is issuing this AD to address smoke and
an overheating condition of the ELB due to corrosion, which could cause
fire onboard the airplane. See the MCAI for additional background
information.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comment received
on the NPRM and the FAA's response to that comment.
[[Page 10748]]
Request To Update Bombardier Email Address
Bombardier requested that the FAA revise the NPRM to update the
email address for obtaining the specified service information from
``<a href="/cdn-cgi/l/email-protection#72061a165c110018321317001d5c101d1f101300161b17005c111d1f"><span class="__cf_email__" data-cfemail="d1a5b9b5ffb2a3bb91b0b4a3beffb3bebcb3b0a3b5b8b4a3ffb2bebc">[email protected]</span></a>'' to ``<a href="/cdn-cgi/l/email-protection#4322206d3a362f032226312c6d212c2e212231272a26316d202c2e"><span class="__cf_email__" data-cfemail="3e5f5d10474b527e5f5b4c51105c51535c5f4c5a575b4c105d5153">[email protected]</span></a>.''
The FAA agrees with the request and has revised this final rule
accordingly.
Clarifications of Compliance Times
The FAA has revised paragraph (g) of this AD to clarify when
replacement is required. This clarification explains that replacement
is required if, during the inspection required by paragraph (g) of this
AD, any last replacement date or manufacturing date is found to be 4
years or older.
The FAA has also revised paragraph (h)(2) of this AD to clarify
that the compliance time of within 48 months is related to the
applicable date specified in paragraph (h)(2)(i) or (ii) of this AD.
The proposed AD inadvertently stated that the compliance time was
``[w]ithin 48 months after the applicable compliance time specified in
paragraph (h)(2)(i) or (ii) of this AD,'' but paragraphs (h)(2)(i) and
(ii) of this AD specify dates, not compliance times.
Conclusion
The FAA reviewed the relevant data, considered the comment
received, and determined that air safety and the public interest
require adopting this final rule with the changes described previously
and minor editorial changes. The FAA has 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.
The FAA also determined that this change will not increase the
economic burden on any operator or increase the scope of this final
rule.
Related Service Information Under 1 CFR Part 51
Bombardier has issued Service Bulletin 700-33-024, dated May 13,
2019. This service information describes procedures for an inspection
to determine the last battery replacement date of the ELB, and
replacement if necessary.
Bombardier also issued the following service information.
<bullet> Global Express BD-700 Supplemental Time Limits/Maintenance
Checks (STLMC) Temporary Revision (TR) 05-19091701, dated September 17,
2019.
<bullet> Global Express BD-700 STLMC TR 05-19091704, dated
September 17, 2019.
<bullet> Global Express XRS BD-700 STLMC TR 05-19091705, dated
September 17, 2019.
These documents describe an amendment to the aircraft maintenance
schedule to include STLMC Chapter 5 task number 33-51-54-603,
``Restoration of the Emergency Lighting Batteries (XL245-B Emergency
Battery System),'' and are distinct since they apply to different
airplane serial numbers.
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
The FAA estimates that this AD affects 69 airplanes of U.S.
registry. The FAA estimates 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
----------------------------------------------------------------------------------------------------------------
3 work-hours x $85 per hour = $255........................... $11,308 $11,563 $797,847
----------------------------------------------------------------------------------------------------------------
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the FAA recognizes that this number may vary from operator to
operator. Since operators incorporate maintenance or inspection program
changes for their affected fleet(s), the FAA has determined that a per-
operator estimate is more accurate than a per-airplane estimate.
Therefore, the FAA estimates the total cost per operator to be $7,650
(90 work-hours x $85 per work-hour).
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.
The FAA is 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) Will not affect intrastate aviation in Alaska, 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.
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:
[[Page 10749]]
2021-03-17 Bombardier, Inc.: Amendment 39-21420; Docket No. FAA-
2020-0843; Product Identifier 2020-NM-073-AD.
(a) Effective Date
This airworthiness directive (AD) is effective March 30, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-700-1A10
airplanes, certificated in any category, serial numbers 9002, 9003,
9011, 9016, 9020, 9022 through 9025 inclusive, 9029, 9031, 9032,
9036, 9039 through 9044 inclusive, 9046 through 9058 inclusive, 9060
through 9065 inclusive, 9067 through 9081 inclusive, 9083 through
9106 inclusive, 9108 through 9122 inclusive, 9124 through 9126
inclusive, 9128, 9129, 9133, 9134, 9136 through 9139 inclusive, 9141
through 9148 inclusive, 9150, 9151, 9153, 9159, 9162, 9163, 9165,
and 9169.
(d) Subject
Air Transport Association (ATA) of America Code 33, Lights.
(e) Reason
This AD was prompted by a report of smoke and signs of an
overheating condition from the emergency light battery (ELB) due to
excessive corrosion surrounding the internal lead acid batteries,
which caused an electrical short circuit that led to the smoke and
overheating condition. The FAA is issuing this AD to address such
conditions, which could cause fire onboard the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection and Corrective Action
Within 15 months after the effective date of this AD, inspect
the ELB to determine the last replacement date or the manufacturing
date, as applicable; if during this inspection, any date is found to
be 4 years or older, replace the ELB before further flight. Do the
actions in accordance with the Accomplishment Instructions of
Bombardier Service Bulletin 700-33-024, dated May 13, 2019. For
airplanes on which the restoration task specified in paragraph (h)
of this AD was done before the effective date of this AD, the
requirements of paragraph (g) of this AD are not required.
(h) Maintenance or Inspection Program Revision
Within 60 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
include the information specified in Bombardier BD-700 Supplemental
Time Limits/Maintenance Checks (STLMC) Chapter 5 task number 33-51-
54-603, ``Restoration of the Emergency Lighting Batteries (XL245-B
Emergency Battery System),'' in the Bombardier BD-700 STLMC, as
specified in the applicable temporary revision identified in figure
1 to paragraph (h) of this AD. The initial compliance time for doing
task 33-51-54-603 is at the applicable time specified in paragraph
(h)(1) or (2) of this AD. Repeat task 33-51-54-603 thereafter at the
interval specified within that task.
(1) If both ELBs were replaced at the time of compliance with
paragraph (g) of this AD: Within 48 months after the ELB
replacement.
(2) If neither ELB, or only one ELB, was replaced at the time of
compliance with paragraph (g) of this AD: Within 48 months after the
applicable date specified in paragraph (h)(2)(i) or (ii) of this AD.
(i) For each ELB, use the battery replacement date, if it is
indicated.
(ii) For each ELB, use the date of manufacture, if it does not
have a battery replacement date indicated.
[GRAPHIC] [TIFF OMITTED] TR23FE21.015
(i) Misidentified Restoration Task
The following temporary revisions misidentified the required
restoration task as task ``33-51-54-602.''
(1) Bombardier Global Express XRS BD-700 STLMC Temporary
Revision 05-19032701, dated March 27, 2019.
(2) Bombardier Global Express BD-700 STLMC Temporary Revision
05-19040301, dated April 3, 2019.
(3) Bombardier Global Express BD-700 STLMC Temporary Revision
05-19040401, dated April 4, 2019.
(j) Compliance With Restoration Task for Airplanes On Which the
Misidentified Task Was Accomplished
For airplanes on which the restoration task specified as task
``33-51-54-602'' in the applicable temporary revision identified in
[[Page 10750]]
paragraph (i) of this AD was done before the effective date of this
AD:
(1) The actions specified in paragraph (g) of this AD are not
required.
(2) The initial accomplishment of the task specified in
paragraphs (h)(1) and (2) of this AD is not required.
(3) Task 33-51-54-603 must be done within 48 months after task
``33-51-54-602'' was accomplished, and thereafter at the intervals
specified in task 33-51-54-603.
(k) No Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (h) of this AD, no alternative
actions (e.g., inspections) and intervals may be used unless the
actions and intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (l)(1) of this AD.
(l) 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 instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or Transport Canada Civil Aviation (TCCA); or
Bombardier's TCCA Design Approval Organization (DAO). If approved by
the DAO, the approval must include the DAO-authorized signature.
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian AD CF-2020-07, dated March 17, 2020, for related
information. This MCAI may be found in the AD docket on the internet
at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket
No. FAA-2020-0843.
(2) For more information about this AD, contact Thomas Niczky,
Aerospace Engineer, Avionics and Electrical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7347; fax 516-794-5531; email <a href="/cdn-cgi/l/email-protection#172e3a7661643a796e7674783a7478645771767639707861"><span class="__cf_email__" data-cfemail="8bb2a6eafdf8a6e5f2eae8e4a6e8e4f8cbedeaeaa5ece4fd">[email protected]</span></a>.
(n) 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) Bombardier Service Bulletin 700-33-024, dated May 13, 2019.
(ii) Bombardier Global Express BD-700 Supplemental Time Limits/
Maintenance Checks (STLMC) Temporary Revision (TR) 05-19091701,
dated September 17, 2019.
(iii) Bombardier Global Express BD-700 STLMC TR 05-19091704,
dated September 17, 2019.
(iv) Bombardier Global Express XRS BD-700 STLMC TR 05-19091705,
dated September 17, 2019.
(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#8beae8a5f2fee7cbeaeef9e4a5e9e4e6e9eaf9efe2eef9a5e8e4e6"><span class="__cf_email__" data-cfemail="1f7e7c31666a735f7e7a6d70317d70727d7e6d7b767a6d317c7072">[email protected]</span></a>; internet <a href="https://www.bombardier.com">https://www.bombardier.com</a>.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety 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, email <a href="/cdn-cgi/l/email-protection#56303332243331783a3331373a163837243778313920"><span class="__cf_email__" data-cfemail="513734352334367f3d3436303d113f3023307f363e27">[email protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on January 29, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021-03574 Filed 2-22-21; 8:45 am]
BILLING CODE 4910-13-P
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Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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