82_FR_27520 82 FR 27406 - Airworthiness Directives; Bombardier, Inc., Airplanes

82 FR 27406 - Airworthiness Directives; Bombardier, Inc., Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 114 (June 15, 2017)

Page Range27406-27408
FR Document2017-12169

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was prompted by a report that the equipment racks were not designed to support the actual weight of all the equipment and the secondary direct current power centers under all loading conditions. This AD requires modifying the equipment racks. We are issuing this AD to address the unsafe condition on these products.

Federal Register, Volume 82 Issue 114 (Thursday, June 15, 2017)
[Federal Register Volume 82, Number 114 (Thursday, June 15, 2017)]
[Rules and Regulations]
[Pages 27406-27408]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-12169]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-9387; Directorate Identifier 2016-NM-182-AD; 
Amendment 39-18926; AD 2017-12-11]
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 that the equipment racks were not designed to support the 
actual weight of all the equipment and the secondary direct current 
power centers under all loading conditions. This AD requires modifying 
the equipment racks. We are issuing this AD to address the unsafe 
condition on these products.

DATES: This AD is effective July 20, 2017.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of July 20, 
2017.

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 Airplane Directorate, 1601 Lind Avenue SW., Renton, 
WA. For information on the availability of this material at the FAA, 
call 425-227-1221. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9387.

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-2016-
9387; 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: Aziz Ahmed, Aerospace Engineer, 
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft 
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, 
NY 11590; telephone 516-228-7329; 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 March 23, 2017 (82 FR 14837). The NPRM was prompted by a recent 
design review of the equipment racks which revealed that the left-hand 
side (LHS) and right-hand side (RHS) equipment racks were not designed 
to support the actual weight of all the equipment and the secondary 
direct current power centers under all loading conditions. The NPRM 
proposed to require modifying the equipment racks. We are

[[Page 27407]]

issuing this AD to prevent structural failure of the LHS or RHS 
equipment racks in the event of a high energy emergency landing or 
runway excursion, which could result in blockage of the emergency exit 
for the flightcrew.
    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued Canadian Airworthiness Directive CF-
2016-26, dated September 14, 2016 (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:

    During a recent design review, a Bombardier equipment supplier 
discovered that the weight of the Secondary Direct Current (DC) 
Power Center was incorrectly reported to the structural partner(s) 
via their equipment interface drawing. Consequently, the left-hand 
side (LHS) and right-hand side (RHS) equipment racks were not 
designed to support the actual weight of all the equipment and the 
Secondary DC Power Centers under all loading conditions. In the 
event of a high energy emergency landing or runway excursion, the 
structural failure of the LHS or RHS equipment racks may result in 
the blockage of the emergency escape route for the pilot(s) and crew 
if this condition is not corrected.

    Required actions include modifying the equipment racks. 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-2016-
9387.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this AD as proposed, except for 
minor editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    We reviewed Bombardier Service Bulletin 100-25-39, dated October 
26, 2015; and Bombardier Service Bulletin 350-25-002, dated October 26, 
2015. This service information describes procedures for modifying the 
equipment racks. These documents are distinct since they apply to 
airplanes having different 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

    We estimate that this AD affects 161 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                         Cost per
            Action                  Labor cost         Parts cost        product        Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Modify equipment racks.......  Up to 10 work-hours           $1,755  Up to $2,605...  Up to $419,405.
                                x $85 per hour =
                                $850.
----------------------------------------------------------------------------------------------------------------

    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 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.

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):

2017-12-11 Bombardier, Inc.: Amendment 39-18926; Docket No. FAA-
2016-9387; Directorate Identifier 2016-NM-182-AD.

(a) Effective Date

    This AD is effective July 20, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Bombardier, Inc., Model BD-100-1A10 
airplanes, certificated in any category, serial numbers (S/Ns) 20003 
through 20532 inclusive.

[[Page 27408]]

(d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/
Furnishings.

(e) Reason

    This AD was prompted by a report that the left-hand side (LHS) 
and right-hand side (RHS) equipment racks were not designed to 
support the actual weight of all the equipment and the secondary 
direct current power centers under all loading conditions. We are 
issuing this AD to prevent structural failure of the LHS or RHS 
equipment racks in the event of a high energy emergency landing or 
runway excursion, which could result in blockage of the emergency 
exit for the flightcrew.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Modification of the Equipment Racks

    Within 90 months after the effective date of this AD, do the 
modification required by paragraph (g)(1) or (g)(2) of this AD, as 
applicable.
    (1) For airplanes having S/Ns 20003 through 20500 inclusive: 
Modify the equipment racks having part numbers (P/Ns) K1000070316-
003 (LHS) and K1000070316-004 (RHS), in accordance with the 
Accomplishment Instructions of Bombardier Service Bulletin 100-25-
39, dated October 26, 2015.
    (2) For airplanes having S/Ns 20501 through 20532 inclusive: 
Modify the equipment rack having P/N K1000070316-004 (RHS only), in 
accordance with the Accomplishment Instructions of Bombardier 
Service Bulletin 350-25-002, dated October 26, 2015.

(h) 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 New York ACO, send it to ATTN: Program Manager, 
Continuing Operational Safety, FAA, New York ACO, 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, 
ANE-170, 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 Airworthiness Directive CF-2016-26, dated September 
14, 2016, 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-2016-9387.
    (2) For more information about this AD, contact Aziz Ahmed, 
Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, 
FAA, New York Aircraft Certification Office (ACO), 1600 Stewart 
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7329; 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 100-25-39, dated October 26, 
2015.
    (ii) Bombardier Service Bulletin 350-25-002, dated October 26, 
2015.
    (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 
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 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 Renton, Washington, on June 5, 2017.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2017-12169 Filed 6-14-17; 8:45 am]
 BILLING CODE 4910-13-P



                                             27406              Federal Register / Vol. 82, No. 114 / Thursday, June 15, 2017 / Rules and Regulations

                                             Type Certificate nos. A9NM and A3EU,                    the event of an over-temperature                       of certain publications listed in this AD
                                             respectively, to incorporate the same                   condition, cell failure, or battery failure.           as of July 20, 2017.
                                             novel or unusual design feature, these                     9. Have a failure sensing and warning               ADDRESSES: For service information
                                             special conditions would apply to those                 system to alert the flightcrew if its                  identified in this final rule, contact
                                             models as well.                                         failure affects safe operation of the                  Bombardier, Inc., 400 Côte-Vertu Road
                                                                                                     airplane.                                              West, Dorval, Québec H4S 1Y9, Canada;
                                             Conclusion
                                                                                                        10. If its function is required for safe            telephone: 514–855–5000; fax: 514–
                                               This action affects only a certain                    operation of the airplane, have a                      855–7401; email: thd.crj@
                                             novel or unusual design feature on two                  monitoring and warning feature that                    aero.bombardier.com; Internet http://
                                             model series of airplanes. It is not a rule             alerts the flightcrew when its charge                  www.bombardier.com. You may view
                                             of general applicability and affects only               state falls below acceptable levels.                   this referenced service information at
                                             the applicant who applied to the FAA                                                                           the FAA, Transport Airplane
                                                                                                       Note 1: A battery system consists of the
                                             for approval of these features on the                   battery, battery charger, and any protective,          Directorate, 1601 Lind Avenue SW.,
                                             airplanes.                                              monitoring, and alerting circuitry or                  Renton, WA. For information on the
                                             List of Subjects in 14 CFR Part 25                      hardware inside or outside of the battery. It          availability of this material at the FAA,
                                                                                                     also includes vents (where necessary) and              call 425–227–1221. It is also available
                                               Aircraft, Aviation safety, Reporting                  packaging. For the purpose of these special            on the Internet at http://
                                             and recordkeeping requirements.                         conditions, a battery and battery system are
                                                                                                     referred to as a battery.
                                                                                                                                                            www.regulations.gov by searching for
                                               The authority citation for these                                                                             and locating Docket No. FAA–2016–
                                             special conditions is as follows:                                                                              9387.
                                                                                                        Note 2: These special conditions apply to
                                               Authority: 49 U.S.C. 106(g), 40113, 44701,            all rechargeable lithium-battery installations
                                             44702, 44704.                                           in lieu of § 25.1353(c)(1) through (c)(4) at
                                                                                                                                                            Examining the AD Docket
                                                                                                     Amendment 25–0 (Model 650) and                           You may examine the AD docket on
                                             The Special Conditions                                  Amendment 25–42 (Model 800A).                          the Internet at http://
                                                Accordingly, pursuant to the                                                                                www.regulations.gov by searching for
                                             authority delegated to me by the                          Issued in Renton, Washington, on June 9,
                                                                                                                                                            and locating Docket No. FAA–2016–
                                             Administrator, the following special                    2017.
                                                                                                                                                            9387; or in person at the Docket
                                             conditions are issued as part of the type               Michael Kaszycki,
                                                                                                                                                            Management Facility between 9 a.m.
                                             certification basis for Textron Model                   Assistant Manager, Transport Airplane                  and 5 p.m., Monday through Friday,
                                             650 and Beechcraft Model 800A                           Directorate, Aircraft Certification Service.
                                                                                                                                                            except Federal holidays. The AD docket
                                             airplanes as modified by Peregrine.                     [FR Doc. 2017–12381 Filed 6–14–17; 8:45 am]            contains this AD, the regulatory
                                                Each rechargeable lithium battery                    BILLING CODE 4910–13–P                                 evaluation, any comments received, and
                                             installation must:                                                                                             other information. The street address for
                                                1. Be designed so that safe cell                                                                            the Docket Office (telephone 800–647–
                                             temperatures and pressures are                          DEPARTMENT OF TRANSPORTATION                           5527) is Docket Management Facility,
                                             maintained under all foreseeable                                                                               U.S. Department of Transportation,
                                             operating conditions to prevent fire and                Federal Aviation Administration
                                                                                                                                                            Docket Operations, M–30, West
                                             explosion.                                                                                                     Building Ground Floor, Room W12–140,
                                                2. Be designed to prevent the                        14 CFR Part 39
                                                                                                                                                            1200 New Jersey Avenue SE.,
                                             occurrence of self-sustaining,                                                                                 Washington, DC 20590.
                                                                                                     [Docket No. FAA–2016–9387; Directorate
                                             uncontrolled increases in temperature                   Identifier 2016–NM–182–AD; Amendment                   FOR FURTHER INFORMATION CONTACT: Aziz
                                             or pressure.                                            39–18926; AD 2017–12–11]
                                                3. Not emit explosive or toxic gases in                                                                     Ahmed, Aerospace Engineer, Airframe
                                             normal operation, or as a result of its                                                                        and Mechanical Systems Branch, ANE–
                                                                                                     RIN 2120–AA64
                                             failure, that may accumulate in                                                                                171, FAA, New York Aircraft
                                             hazardous quantities within the                         Airworthiness Directives; Bombardier,                  Certification Office (ACO), 1600 Stewart
                                             airplane.                                               Inc., Airplanes                                        Avenue, Suite 410, Westbury, NY
                                                4. Meet the requirements of 14 CFR                                                                          11590; telephone 516–228–7329; fax
                                             25.863.                                                 AGENCY:  Federal Aviation                              516–794–5531.
                                                5. Not damage surrounding structure                  Administration (FAA), Department of                    SUPPLEMENTARY INFORMATION:
                                             or adjacent systems, equipment, or                      Transportation (DOT).
                                                                                                     ACTION: Final rule.
                                                                                                                                                            Discussion
                                             electrical wiring from corrosive fluids or
                                             gases that may escape in such a way as                                                                           We issued a notice of proposed
                                             to cause a major or more-severe failure                 SUMMARY:   We are adopting a new                       rulemaking (NPRM) to amend 14 CFR
                                             condition.                                              airworthiness directive (AD) for certain               part 39 by adding an AD that would
                                                6. Have provisions to prevent any                    Bombardier, Inc., Model BD–100–1A10                    apply to certain Bombardier, Inc., Model
                                             hazardous effect on airplane structure or               airplanes. This AD was prompted by a                   BD–100–1A10 airplanes. The NPRM
                                             systems caused by the maximum                           report that the equipment racks were                   published in the Federal Register on
                                             amount of heat the battery installation                 not designed to support the actual                     March 23, 2017 (82 FR 14837). The
                                             can generate due to any failure of it or                weight of all the equipment and the                    NPRM was prompted by a recent design
                                             its individual cells.                                   secondary direct current power centers                 review of the equipment racks which
                                                7. Be capable of automatically                       under all loading conditions. This AD                  revealed that the left-hand side (LHS)
pmangrum on DSK3GDR082PROD with RULES




                                             controlling the charge rate of each cell                requires modifying the equipment racks.                and right-hand side (RHS) equipment
                                             to prevent cell imbalance, back-                        We are issuing this AD to address the                  racks were not designed to support the
                                             charging, overcharging, overheating, and                unsafe condition on these products.                    actual weight of all the equipment and
                                             uncontrollable temperature and                          DATES: This AD is effective July 20,                   the secondary direct current power
                                             pressure.                                               2017.                                                  centers under all loading conditions.
                                                8. Have a means to be automatically                    The Director of the Federal Register                 The NPRM proposed to require
                                             disconnected from its charging source in                approved the incorporation by reference                modifying the equipment racks. We are


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                                                                Federal Register / Vol. 82, No. 114 / Thursday, June 15, 2017 / Rules and Regulations                                                 27407

                                             issuing this AD to prevent structural                   runway excursion, the structural failure of              • Do not add any additional burden
                                             failure of the LHS or RHS equipment                     the LHS or RHS equipment racks may result              upon the public than was already
                                             racks in the event of a high energy                     in the blockage of the emergency escape
                                                                                                                                                            proposed in the NPRM.
                                                                                                     route for the pilot(s) and crew if this
                                             emergency landing or runway                             condition is not corrected.
                                             excursion, which could result in                                                                               Related Service Information Under 1
                                             blockage of the emergency exit for the                    Required actions include modifying                   CFR Part 51
                                             flightcrew.                                             the equipment racks. You may examine
                                                                                                     the MCAI in the AD docket on the                         We reviewed Bombardier Service
                                                Transport Canada Civil Aviation
                                                                                                     Internet at http://www.regulations.gov                 Bulletin 100–25–39, dated October 26,
                                             (TCCA), which is the aviation authority
                                             for Canada, has issued Canadian                         by searching for and locating Docket No.               2015; and Bombardier Service Bulletin
                                             Airworthiness Directive CF–2016–26,                     FAA–2016–9387.                                         350–25–002, dated October 26, 2015.
                                             dated September 14, 2016 (referred to                                                                          This service information describes
                                                                                                     Comments
                                             after this as the Mandatory Continuing                                                                         procedures for modifying the equipment
                                             Airworthiness Information, or ‘‘the                       We gave the public the opportunity to                racks. These documents are distinct
                                             MCAI’’), to correct an unsafe condition                 participate in developing this AD. We                  since they apply to airplanes having
                                             for certain Bombardier, Inc., Model BD–                 received no comments on the NPRM or                    different serial numbers. This service
                                                                                                     on the determination of the cost to the                information is reasonably available
                                             100–1A10 airplanes. The MCAI states:
                                                                                                     public.                                                because the interested parties have
                                               During a recent design review, a
                                             Bombardier equipment supplier discovered                Conclusion                                             access to it through their normal course
                                             that the weight of the Secondary Direct                   We reviewed the relevant data and                    of business or by the means identified
                                             Current (DC) Power Center was incorrectly               determined that air safety and the                     in the ADDRESSES section.
                                             reported to the structural partner(s) via their
                                                                                                     public interest require adopting this AD               Costs of Compliance
                                             equipment interface drawing. Consequently,
                                             the left-hand side (LHS) and right-hand side            as proposed, except for minor editorial
                                             (RHS) equipment racks were not designed to              changes. We have determined that these                   We estimate that this AD affects 161
                                             support the actual weight of all the                    minor changes:                                         airplanes of U.S. registry.
                                             equipment and the Secondary DC Power                      • Are consistent with the intent that
                                                                                                                                                              We estimate the following costs to
                                             Centers under all loading conditions. In the            was proposed in the NPRM for
                                                                                                                                                            comply with this AD:
                                             event of a high energy emergency landing or             correcting the unsafe condition; and

                                                                                                                   ESTIMATED COSTS
                                                                                                                                                                                                Cost on
                                                       Action                                     Labor cost                             Parts cost          Cost per product                U.S. operators

                                             Modify equipment racks        Up to 10 work-hours × $85 per hour = $850 .......                    $1,755   Up to $2,605 .................   Up to $419,405.



                                                According to the manufacturer, some                  products identified in this rulemaking                 Adoption of the Amendment
                                             of the costs of this AD may be covered                  action.
                                             under warranty, thereby reducing the                                                                             Accordingly, under the authority
                                                                                                     Regulatory Findings                                    delegated to me by the Administrator,
                                             cost impact on affected individuals. We
                                             do not control warranty coverage for                      We determined that this AD will not                  the FAA amends 14 CFR part 39 as
                                             affected individuals. As a result, we                   have federalism implications under                     follows:
                                             have included all costs in our cost                     Executive Order 13132. This AD will
                                                                                                     not have a substantial direct effect on                PART 39—AIRWORTHINESS
                                             estimate.                                                                                                      DIRECTIVES
                                                                                                     the States, on the relationship between
                                             Authority for This Rulemaking                           the national government and the States,
                                                                                                     or on the distribution of power and                    ■ 1. The authority citation for part 39
                                                Title 49 of the United States Code                                                                          continues to read as follows:
                                             specifies the FAA’s authority to issue                  responsibilities among the various
                                                                                                     levels of government.                                      Authority: 49 U.S.C. 106(g), 40113, 44701.
                                             rules on aviation safety. Subtitle I,
                                             section 106, describes the authority of                   For the reasons discussed above, I
                                                                                                                                                            § 39.13    [Amended]
                                             the FAA Administrator. ‘‘Subtitle VII:                  certify that this AD:
                                                                                                       1. Is not a ‘‘significant regulatory                 ■ 2. The FAA amends § 39.13 by adding
                                             Aviation Programs,’’ describes in more
                                                                                                     action’’ under Executive Order 12866;                  the following new airworthiness
                                             detail the scope of the Agency’s
                                                                                                       2. Is not a ‘‘significant rule’’ under the           directive (AD):
                                             authority.
                                                                                                     DOT Regulatory Policies and Procedures
                                                We are issuing this rulemaking under                                                                        2017–12–11 Bombardier, Inc.: Amendment
                                                                                                     (44 FR 11034, February 26, 1979);                          39–18926; Docket No. FAA–2016–9387;
                                             the authority described in ‘‘Subtitle VII,                3. Will not affect intrastate aviation in                Directorate Identifier 2016–NM–182–AD.
                                             Part A, Subpart III, Section 44701:                     Alaska; and
                                             General requirements.’’ Under that                        4. Will not have a significant                       (a) Effective Date
                                             section, Congress charges the FAA with                  economic impact, positive or negative,                   This AD is effective July 20, 2017.
                                             promoting safe flight of civil aircraft in              on a substantial number of small entities
pmangrum on DSK3GDR082PROD with RULES




                                                                                                                                                            (b) Affected ADs
                                             air commerce by prescribing regulations                 under the criteria of the Regulatory
                                             for practices, methods, and procedures                                                                           None.
                                                                                                     Flexibility Act.
                                             the Administrator finds necessary for                                                                          (c) Applicability
                                             safety in air commerce. This regulation                 List of Subjects in 14 CFR Part 39
                                                                                                                                                               This AD applies to Bombardier, Inc.,
                                             is within the scope of that authority                     Air transportation, Aircraft, Aviation               Model BD–100–1A10 airplanes, certificated
                                             because it addresses an unsafe condition                safety, Incorporation by reference,                    in any category, serial numbers (S/Ns) 20003
                                             that is likely to exist or develop on                   Safety.                                                through 20532 inclusive.



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                                             27408              Federal Register / Vol. 82, No. 114 / Thursday, June 15, 2017 / Rules and Regulations

                                             (d) Subject                                             (i) Related Information                                DEPARTMENT OF TRANSPORTATION
                                               Air Transport Association (ATA) of                       (1) Refer to Mandatory Continuing
                                             America Code 25, Equipment/Furnishings.                 Airworthiness Information (MCAI) Canadian              Federal Aviation Administration
                                             (e) Reason                                              Airworthiness Directive CF–2016–26, dated
                                                                                                     September 14, 2016, for related information.           14 CFR Part 39
                                                This AD was prompted by a report that the
                                             left-hand side (LHS) and right-hand side                This MCAI may be found in the AD docket                [Docket No. FAA–2016–9571; Directorate
                                             (RHS) equipment racks were not designed to              on the Internet at http://www.regulations.gov          Identifier 2016–NM–139–AD; Amendment
                                             support the actual weight of all the                    by searching for and locating Docket No.               39–18925; AD 2017–12–10]
                                             equipment and the secondary direct current              FAA–2016–9387.
                                             power centers under all loading conditions.                                                                    RIN 2120–AA64
                                                                                                        (2) For more information about this AD,
                                             We are issuing this AD to prevent structural            contact Aziz Ahmed, Aerospace Engineer,
                                             failure of the LHS or RHS equipment racks                                                                      Airworthiness Directives; Airbus
                                                                                                     Airframe and Mechanical Systems Branch,
                                             in the event of a high energy emergency                                                                        Airplanes
                                                                                                     ANE–171, FAA, New York Aircraft
                                             landing or runway excursion, which could
                                             result in blockage of the emergency exit for            Certification Office (ACO), 1600 Stewart               AGENCY:  Federal Aviation
                                             the flightcrew.                                         Avenue, Suite 410, Westbury, NY 11590;                 Administration (FAA), Department of
                                                                                                     telephone 516–228–7329; fax 516–794–5531.              Transportation (DOT).
                                             (f) Compliance
                                                                                                     (j) Material Incorporated by Reference                 ACTION: Final rule.
                                                Comply with this AD within the
                                             compliance times specified, unless already                 (1) The Director of the Federal Register            SUMMARY:    We are adopting a new
                                             done.                                                   approved the incorporation by reference                airworthiness directive (AD) for certain
                                             (g) Modification of the Equipment Racks                 (IBR) of the service information listed in this        Airbus Model A321–111, –112, –131,
                                                                                                     paragraph under 5 U.S.C. 552(a) and 1 CFR              –211, –212, –213, –231, and –232
                                                Within 90 months after the effective date
                                             of this AD, do the modification required by             part 51.                                               airplanes. This AD was prompted by a
                                             paragraph (g)(1) or (g)(2) of this AD, as                  (2) You must use this service information           full scale fatigue test campaign on these
                                             applicable.                                             as applicable to do the actions required by            airplanes in the context of the extended
                                                (1) For airplanes having S/Ns 20003                  this AD, unless this AD specifies otherwise.           service goal. This AD requires
                                             through 20500 inclusive: Modify the                        (i) Bombardier Service Bulletin 100–25–39,
                                                                                                                                                            inspections of the affected frame
                                             equipment racks having part numbers (P/Ns)              dated October 26, 2015.
                                             K1000070316–003 (LHS) and K1000070316–                                                                         locations, and repair if necessary. We
                                                                                                        (ii) Bombardier Service Bulletin 350–25–
                                             004 (RHS), in accordance with the                                                                              are issuing this AD to address the unsafe
                                                                                                     002, dated October 26, 2015.
                                             Accomplishment Instructions of Bombardier                                                                      condition on these products.
                                                                                                        (3) For service information identified in
                                             Service Bulletin 100–25–39, dated October                                                                      DATES: This AD is effective July 20,
                                                                                                     this AD, contact Bombardier, Inc., 400 Côte-
                                             26, 2015.                                                                                                      2017.
                                                (2) For airplanes having S/Ns 20501                  Vertu Road West, Dorval, Québec H4S 1Y9,
                                                                                                     Canada; telephone: 514–855–5000; fax: 514–               The Director of the Federal Register
                                             through 20532 inclusive: Modify the
                                             equipment rack having P/N K1000070316–                  855–7401; email: thd.crj@                              approved the incorporation by reference
                                             004 (RHS only), in accordance with the                  aero.bombardier.com; Internet http://                  of certain publications listed in this AD
                                             Accomplishment Instructions of Bombardier               www.bombardier.com.                                    as of July 20, 2017.
                                             Service Bulletin 350–25–002, dated October                 (4) You may view this service information           ADDRESSES: For service information
                                             26, 2015.                                               at the FAA, Transport Airplane Directorate,            identified in this final rule, contact
                                             (h) Other FAA AD Provisions                             1601 Lind Avenue SW., Renton, WA. For                  Airbus, Airworthiness Office—EIAS, 1
                                                                                                     information on the availability of this                Rond Point Maurice Bellonte, 31707
                                               The following provisions also apply to this
                                             AD:                                                     material at the FAA, call 425–227–1221.                Blagnac Cedex, France; telephone +33 5
                                               (1) Alternative Methods of Compliance                    (5) You may view this service information           61 93 36 96; fax +33 5 61 93 44 51; email
                                             (AMOCs): The Manager, New York Aircraft                 that is incorporated by reference at the               account.airworth-eas@airbus.com;
                                             Certification Office (ACO), ANE–170, FAA,               National Archives and Records                          Internet http://www.airbus.com. You
                                             has the authority to approve AMOCs for this             Administration (NARA). For information on              may view this referenced service
                                             AD, if requested using the procedures found             the availability of this material at NARA, call        information at the FAA, Transport
                                             in 14 CFR 39.19. In accordance with 14 CFR              202–741–6030, or go to: http://
                                             39.19, send your request to your principal
                                                                                                                                                            Airplane Directorate, 1601 Lind Avenue
                                                                                                     www.archives.gov/federal-register/cfr/ibr-             SW., Renton, WA. For information on
                                             inspector or local Flight Standards District
                                                                                                     locations.html.                                        the availability of this material at the
                                             Office, as appropriate. If sending information
                                             directly to the New York ACO, send it to                  Issued in Renton, Washington, on June 5,             FAA, call 425–227–1221. It is also
                                             ATTN: Program Manager, Continuing                       2017.                                                  available on the Internet at http://
                                             Operational Safety, FAA, New York ACO,                  Michael Kaszycki,                                      www.regulations.gov by searching for
                                             1600 Stewart Avenue, Suite 410, Westbury,                                                                      and locating Docket No. FAA–2016–
                                             NY 11590; telephone 516–228–7300; fax                   Acting Manager, Transport Airplane
                                                                                                     Directorate, Aircraft Certification Service.           9571.
                                             516–794–5531. Before using any approved
                                             AMOC, notify your appropriate principal                 [FR Doc. 2017–12169 Filed 6–14–17; 8:45 am]            Examining the AD Docket
                                             inspector, or lacking a principal inspector,
                                             the manager of the local flight standards
                                                                                                     BILLING CODE 4910–13–P                                   You may examine the AD docket on
                                             district office/certificate holding district                                                                   the Internet at http://
                                             office.                                                                                                        www.regulations.gov by searching for
                                               (2) Contacting the Manufacturer: For any                                                                     and locating Docket No. FAA–2016–
                                             requirement in this AD to obtain corrective                                                                    9571; or in person at the Docket
pmangrum on DSK3GDR082PROD with RULES




                                             actions from a manufacturer, the action must                                                                   Management Facility between 9 a.m.
                                             be accomplished using a method approved                                                                        and 5 p.m., Monday through Friday,
                                             by the Manager, New York ACO, ANE–170,
                                             FAA; or Transport Canada Civil Aviation
                                                                                                                                                            except Federal holidays. The AD docket
                                             (TCCA); or Bombardier, Inc.’s TCCA Design                                                                      contains this AD, the regulatory
                                             Approval Organization (DAO). If approved by                                                                    evaluation, any comments received, and
                                             the DAO, the approval must include the                                                                         other information. The street address for
                                             DAO-authorized signature.                                                                                      the Docket Office (telephone 800–647–


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Document Created: 2017-06-15 01:03:47
Document Modified: 2017-06-15 01:03:47
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionRules and Regulations
ActionFinal rule.
DatesThis AD is effective July 20, 2017.
ContactAziz Ahmed, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7329; fax 516-794-5531.
FR Citation82 FR 27406 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

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