Published 2018-06-20 · Federal Register document 2018-13125
Airworthiness Directives; Bombardier, Inc., Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was prompted by a report indicating that certain lanyards for the passenger oxygen masks located in the airplane's entry area are too long. This AD requires replacement of certain oxygen mask lanyards with shorter lanyards. We are issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:58.123663+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2018-258c65fa72d503e0
- Source row
- results[174]
- Raw source SHA-256
- 258c65fa72d503e0b0dfb928a28beb1793ddc7dd9218bce0413e53dfe11d78fb
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2018-13-04
- Effective date printed in this edition
- 2018-07-25
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective July 25, 2018.
Exact source excerpt. Text positions 11714–11775, end exclusive, in the original decoded publication. SHA-256: 607028b29b1e17ef3ecdd5561ba1702b8bbc1db220ebbe0c21571a0c0bc14eb7
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 11775–11804, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-100-1A10
airplanes, certificated in any category, serial numbers 20003
through 20424 inclusive and 20426 through 20500 inclusive.
Exact source excerpt. Text positions 11804–12006, end exclusive, in the original decoded publication. SHA-256: 140ae02f0047765b5a6ff1fbd416905cee19f890c0c5e79cfdf9401589e7742d
Subject
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
Exact source excerpt. Text positions 12006–12084, end exclusive, in the original decoded publication. SHA-256: beebdc11ca55a698e6bba23e8dc2d9b64bbafa16f2e35342201f0a7331ad0a62
Reason
(e) Reason
This AD was prompted by a report indicating that certain
lanyards for the passenger oxygen masks located in the airplane's
entry area are too long. The length of the oxygen mask lanyard might
cause the safety pin tethered to the opposite end of the lanyard to
remain engaged in the oxygen flow mechanism when the mask is pulled
to the passenger's face. We are issuing this AD to detect and
correct lanyards that are too long, which might result in
difficulties starting the flow of oxygen in an emergency.
Exact source excerpt. Text positions 12084–12614, end exclusive, in the original decoded publication. SHA-256: 96f6630f5d5a0c790923e49d5ecb2a7706a4d8d3463d4e02bc45c9cfe6fbfc4e
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 12614–12716, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Lanyard Replacement
(g) Lanyard Replacement
Within 36 months after the effective date of this AD: For any
entry area passenger oxygen mask dispensing unit (POMDU) having part
number (P/N) 833-830-01, replace the lanyards in the POMDU with new
lanyards having P/N 289-165-10, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 100-35-
08, dated April 11, 2017.
Exact source excerpt. Text positions 12716–13097, end exclusive, in the original decoded publication. SHA-256: aa610345b485d53391e9659cacbd95b3e3ca76be7592ad60fa3f02e97557bb9d
Other FAA AD Provisions
(h) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO
[[Page 28538]]
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
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
Exact source excerpt. Text positions 13097–14417, end exclusive, in the original decoded publication. SHA-256: 14a678b14c3e9d71f6bc732a4d366d34b301c4ade46fa20fe34377724c161ba0
Related Information
(i) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian AD CF-2017-22, dated June 23, 2017, for related
information. This MCAI may be found in the AD docket on the internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2017-1247.
(2) For more information about this AD, contact Cesar Gomez,
Aerospace Engineer, Airframe and Mechanical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone: 516-228-7318; fax: 516-794-5531.
Exact source excerpt. Text positions 14417–14981, end exclusive, in the original decoded publication. SHA-256: c6d2494d1a894ab550aecc0d72e440c4694a7944ae0dbc559bcfa72719a8bb75
Material Incorporated by Reference
(j) 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 100-35-08, dated April 11, 2017.
(ii) Reserved.
(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: [email protected]; internet: http://www.bombardier.com.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 14981–16204, end exclusive, in the original decoded publication. SHA-256: c1e57a7373970c504d1cbedee6cc2fb86eac2b8c530e6a6d6ba0b5f8e3952f4c
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 2018-13-04 · 0 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: b3f169ffd518ec872627aeee16e5672d67de742596dacbd45c6faf5bcc152649. Source manifest: 61d7f3a9cbbeb1d41b63878b5a9714da7cca17ec8bf51488c0fb813b10d4a64c.
Official source · 2018-06-20
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 83, Number 119 (Wednesday, June 20, 2018)]
[Rules and Regulations]
[Pages 28536-28538]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-13125]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-1247; Product Identifier 2017-NM-085-AD; Amendment
39-19316; AD 2018-13-04]
RIN 2120-AA64
Airworthiness Directives; 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
Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was prompted by
a report indicating that certain lanyards for the passenger oxygen
masks located in the airplane's entry area are too long. This AD
requires replacement of certain oxygen mask lanyards with shorter
lanyards. We are issuing this AD to address the unsafe condition on
these products.
DATES: This AD is effective July 25, 2018.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 25,
2018.
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: [email protected]; internet: http://www.bombardier.com. You may view this referenced 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 http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1247.
Examining the AD Docket
You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1247; 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 Docket Management Facility, 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: Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Section, FAA, New York ACO Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY 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 by adding an AD that would apply to certain Bombardier, Inc.,
Model BD-100-1A10 airplanes. The NPRM published in the Federal Register
on January 17, 2018 (83 FR 2373) (``the NPRM''). The NPRM was prompted
by a report indicating that certain lanyards for the passenger oxygen
masks located in the airplane's entry area are too long. The NPRM
proposed to require replacement of certain oxygen mask lanyards with
shorter lanyards. We are issuing this AD to detect and correct lanyards
that are too long, which might result in difficulties starting the flow
of oxygen in an emergency.
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2017-22, dated June 23,
2017 (referred to after this as the Mandatory Continuing Airworthiness
Information, or ``the MCAI''), to correct an unsafe condition for
certain Bombardier, Inc., Model BD-100-1A10 airplanes. The MCAI states:
Bombardier, Inc., has discovered that the entry area passenger
oxygen mask lanyards are too long. Upon deployment during an
emergency, this may result in difficulties to start the oxygen flow
for tall individuals. This [Canadian] AD mandates the replacement of
the existing entry area passenger oxygen mask lanyards with shorter
ones for proper operation.
You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1247.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM and
the FAA's response to each comment.
Request To Match Compliance Time in the Service Information
Bombardier noted that the compliance time in paragraph (g) of the
proposed AD was ``Within 36 months after the effective date of this
AD,'' whereas Bombardier Service Bulletin 100-35-08, dated April 11,
2017, includes a compliance time of within ``36 months from this
Service Bulletin release date (Basic Issue)''. We infer that the
commenter is requesting that the compliance time in paragraph (g) of
the proposed AD be changed to match what is in the service information.
We do not agree with the commenter's request. In developing an
appropriate compliance time for this AD, we considered the degree of
urgency associated with addressing the unsafe condition and the
manufacturer's recommendation for an appropriate compliance time, as
well as the time required for the rulemaking process. In consideration
of these factors, we find that the compliance time, as proposed,
represents an appropriate interval in which to replace the affected
oxygen mask lanyards, while still maintaining an adequate level of
safety. Operators are always permitted to accomplish the requirements
of an AD at a time earlier than the specified compliance time. We have
not changed this AD regarding this issue.
Request To Correct Typographical Error
Bombardier requested that a part number in paragraph (g) of the
proposed AD be corrected. Paragraph (g) of the proposed AD specified
the replacement of lanyards having a certain part number with new
lanyards having part number P/N 289-65-10. The correct part number for
the new lanyards is P/N 289-165-10.
We agree with the commenter's request and have revised paragraph
(g) of this AD to include the correct part number for the new lanyards,
P/N 289-165-10, which is specified in Bombardier Service Bulletin 100-
35-08, dated April 11, 2017.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD with the changes 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 correcting the unsafe condition; and
[[Page 28537]]
<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 AD.
Related Service Information Under 1 CFR Part 51
Bombardier has issued Service Bulletin 100-35-08, dated April 11,
2017. This service information describes procedures for replacing the
lanyards in the passenger oxygen masks located in the passenger entry
area. 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 AD affects 187 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............................. (\1\) $85 $15,895
----------------------------------------------------------------------------------------------------------------
\1\ We have received no definitive data that will enable us to provide cost estimates for the required parts.
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all available costs in our
cost estimate.
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 to
the Director of the System Oversight Division.
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.
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):
2018-13-04 Bombardier, Inc. Amendment 39-19316; Docket No. FAA-2017-
1247; Product Identifier 2017-NM-085-AD.
(a) Effective Date
This AD is effective July 25, 2018.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-100-1A10
airplanes, certificated in any category, serial numbers 20003
through 20424 inclusive and 20426 through 20500 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Reason
This AD was prompted by a report indicating that certain
lanyards for the passenger oxygen masks located in the airplane's
entry area are too long. The length of the oxygen mask lanyard might
cause the safety pin tethered to the opposite end of the lanyard to
remain engaged in the oxygen flow mechanism when the mask is pulled
to the passenger's face. We are issuing this AD to detect and
correct lanyards that are too long, which might result in
difficulties starting the flow of oxygen in an emergency.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Lanyard Replacement
Within 36 months after the effective date of this AD: For any
entry area passenger oxygen mask dispensing unit (POMDU) having part
number (P/N) 833-830-01, replace the lanyards in the POMDU with new
lanyards having P/N 289-165-10, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 100-35-
08, dated April 11, 2017.
(h) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO
[[Page 28538]]
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
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(i) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian AD CF-2017-22, dated June 23, 2017, for related
information. This MCAI may be found in the AD docket on the internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2017-1247.
(2) For more information about this AD, contact Cesar Gomez,
Aerospace Engineer, Airframe and Mechanical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone: 516-228-7318; fax: 516-794-5531.
(j) 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 100-35-08, dated April 11, 2017.
(ii) Reserved.
(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: [email protected]; internet: http://www.bombardier.com.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Des Moines, Washington, on June 8, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-13125 Filed 6-19-18; 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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