Document ID: FAA-2018-0710-0004
Agency: faa
Document Type: Rule
Title: Airworthiness Directives: Bombardier, Inc., Airplanes
Posted Date: 2019-03-11T04:00Z

[Federal Register Volume 84, Number 47 (Monday, March 11, 2019)]
[Rules and Regulations]
[Pages 8591-8598]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-03255]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0710; Product Identifier 2018-NM-079-AD; Amendment 
39-19574; AD 2019-03-22]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This AD 
was prompted by in-service findings that a cotter pin at the main 
fitting joint of the nose landing gear (NLG) retraction actuator to the 
NLG strut showed evidence of shearing after an NLG retraction-extension 
cycling. This AD requires revision of the existing maintenance or 
inspection program, as applicable, a general visual inspection for 
damage of a certain cotter pin present on certain configurations of the 
NLG strut assembly and for the

[[Page 8592]]

modification number shown on the identification plate for the NLG 
strut, and modification of the NLG retraction actuator hardware on any 
damaged NLG strut assembly. We are issuing this AD to address the 
unsafe condition on these products.

DATES: This AD is effective April 15, 2019.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of April 15, 
2019.

ADDRESSES: For service information identified in this final rule, 
contact Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, 
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; email thd.crj@aero.bombardier.com; internet http://www.bombardier.com. You may view this service information at the FAA, 
Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 206-
231-3195. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0710.

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-2018-
0710; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, the regulatory evaluation, any comments received, and 
other information. The address for Docket Operations (phone: 800-647-
5527) is U.S. Department of Transportation, Docket Operations, M-30, 
West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, 
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Darren Gassetto, Aerospace Engineer, 
Mechanical Systems and Admin Services Section, FAA, New York ACO 
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 
516-228-7323; fax 516-794-5531; email 9-avs-nyaco-cos@faa.gov.

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-700-1A10 and BD-700-1A11 airplanes. The NPRM published in the 
Federal Register on August 16, 2018 (83 FR 40703). The NPRM was 
prompted by in-service findings that a cotter pin at the main fitting 
joint of the NLG retraction actuator to the NLG strut showed evidence 
of shearing after an NLG retraction-extension cycling. The NPRM 
proposed to require revision of the existing maintenance or inspection 
program, as applicable, a general visual inspection for damage of a 
certain cotter pin present on certain configurations of the NLG strut 
assembly and for the modification number shown on the identification 
plate for the NLG strut, and modification of the NLG retraction 
actuator hardware on any damaged NLG strut assembly.
    We are issuing this AD to address shearing of the cotter pin at the 
main fitting joint of the NLG retraction actuator to the NLG strut, 
which could lead to a loss of hardware and result in an actuator 
disconnect and the NLG failing to retract or extend, or in an undamped 
freefall, which could adversely affect the airplane's continued safe 
flight and landing.
    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued Canadian AD CF-2018-05, dated January 
23, 2018 (referred to after this as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for certain Bombardier, Inc., Model BD-700-1A10 and BD-700-
1A11 airplanes. The MCAI states:

    There have been in-service findings whereby the cotter pin at 
the retraction actuator to nose landing gear (NLG) strut main 
fitting was observed to be damaged after a NLG retraction-extension 
cycling. This condition could lead to a loss of hardware and result 
in an actuator disconnect resulting in a failure to retract or 
extend, or in an undamped freefall of the NLG [which could adversely 
affect the airplane's continued safe flight and landing].
    This [Canadian] AD mandates a revision to the approved 
maintenance schedule. This [Canadian] AD also mandates a visual 
inspection of the cotter pin for certain configurations of NLG strut 
assembly, and if found damaged, the incorporation of a modification 
which introduces a new castellated nut, spacer, end plate and sleeve 
to the NLG retraction actuator to main fitting joint.

    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-2018-
0710.

Comments

    We gave the public the opportunity to participate in developing 
this final rule. The following presents the comments received on the 
NPRM and the FAA's response to each comment.

Request To Clarify Effectivity of Inspection and Modification 
Requirements

    NetJets stated that they were not able to find paragraph 1.A, 
``Effectivity,'' in the proposed AD, which was referenced in paragraph 
(h)(2) of the proposed AD.
    We infer from the commenter's statement that they request the 
language in paragraph (h)(2) of the proposed AD be revised to clarify 
the reference to paragraph 1.A, ``Effectivity.'' We agree to clarify. 
Paragraph (h)(2) of the proposed AD directs operators to the applicable 
Bombardier service information specified in figure 2 to paragraph (h) 
of this AD. Each Bombardier service information referenced in figure 2 
to paragraph (h) of this AD contains paragraph 1.A, ``Effectivity,'' 
which operators must use to determine the applicability of the actions 
required in paragraph (h)(1) to their specific airplane configuration. 
Paragraph 1.A, ``Effectivity,'' can be found in Paragraph 1, ``Planning 
Information,'' in the applicable Bombardier service information. We 
have not changed the AD in this regard.

Request To Refer to New Service Information

    NetJets observed that the service information specified in figure 1 
to paragraph (g) of the proposed AD is out of date and requested that 
we update those references to the latest revision. Netjets noted that 
at least one of the service bulletins has been revised since the NPRM 
was released.
    We agree with the request to refer to the latest service 
information, which adds a note to clarify the level at which time 
tracking of non-serialized parts should be done, and increases the 
interval at which certain inspections must be conducted. We have 
determined that the revised actions have no effect on airplanes on 
which the earlier actions were completed. Each service bulletin in 
figure 1 to paragraph (g) of the AD has been revised since the NPRM was 
released, and we have revised the preamble and figure 1 to paragraph 
(g) of this AD accordingly. We have coordinated this with TCCA.
    Because the revised service information does not include any 
additional actions, we have revised paragraph (j) of this AD to provide 
credit for specified actions performed before the effective date of 
this AD in accordance with Airworthiness Limitation (AWL) Task 32-33-
01-111, ``Restoration of the Nose Landing Gear Shock-Strut Assembly to 
Retraction-Actuator Main-Fitting Joint,'' of Bombardier Global 5000 
Time Limits/

[[Page 8593]]

Maintenance Checks, Publication No. BD-700 TLMC, Revision 19, dated 
November 13, 2017; Bombardier Global 5000 Featuring Global Vision 
Flight Deck--Time Limits/Maintenance Checks, Publication No. GL 5000 
GVFD, Revision 9, dated November 13, 2017; Bombardier Global 6000 Time 
Limits/Maintenance Checks, Publication No. GL 6000 TLMC, Revision 9, 
dated November 13, 2017; Bombardier Global Express Time Limits/
Maintenance Checks, Publication No. BD-700 TLMC, Revision 28, dated 
November 13, 2017; or Bombardier Global Express XRS Time Limits/
Maintenance Checks, Publication No. BD-700 XRS TLMC, Revision 15, dated 
November 13, 2017; as applicable.

Conclusion

    We reviewed the relevant data, considered the comments received, 
and determined that air safety and the public interest require adopting 
this final rule with the changes described previously and minor 
editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.
    We also determined that these changes will not increase the 
economic burden on any operator or increase the scope of this final 
rule.

Related Service Information Under 1 CFR Part 51

    Bombardier has issued the following service information, which 
describes procedures for a general visual inspection for damage of the 
cotter pin retaining the bolt that secures the main fitting joint of 
the NLG retraction actuator to the NLG strut and for the modification 
number shown on the identification plate for the NLG strut, and 
modification of the NLG retraction actuator hardware that secures the 
NLG retraction actuator to the NLG strut. These documents are distinct 
since they apply to different airplane models in different 
configurations.
     Bombardier Service Bulletin 700-1A11-32-022, Revision 2, 
dated November 6, 2017.
     Bombardier Service Bulletin 700-32-035, Revision 2, dated 
November 6, 2017.
     Bombardier Service Bulletin 700-32-5011, Revision 2, dated 
November 6, 2017.
     Bombardier Service Bulletin 700-32-6011, Revision 2, dated 
November 6, 2017.
    Bombardier has issued AWL Task 32-33-01-111, ``Restoration of the 
Nose Landing Gear Shock-Strut Assembly to Retraction-Actuator Main-
Fitting Joint,'' of the following service information, which identifies 
airworthiness limitation tasks for restoration of the main fitting 
joint of the NLG retraction actuator to the NLG strut. These documents 
are distinct since they apply to different airplane models in different 
configurations.
     Bombardier Global 5000 Time Limits/Maintenance Checks, 
Publication No. BD-700 TLMC, Revision 20, dated May 3, 2018, for 
Bombardier Model BD-700-1A11 airplanes.
     Bombardier Global 5000 Featuring Global Vision Flight Deck 
Time Limits/Maintenance Checks, Publication No. GL 5000 GVFD TLMC, 
Revision 10, dated May 3, 2018, for Bombardier Model BD-700-1A11 
airplanes.
     Bombardier Global 6000 Time Limits/Maintenance Checks, 
Publication No. GL 6000 TLMC, Revision 10, dated May 3, 2018, for 
Bombardier Model BD-700-1A10 airplanes.
     Bombardier Global Express Time Limits/Maintenance Checks, 
Publication No. BD-700 TLMC, Revision 29, dated May 3, 2018, for 
Bombardier Model BD-700-1A10 airplanes.
     Bombardier Global Express XRS Time Limits/Maintenance 
Checks, Publication No. BD-700 XRS TLMC, Revision 16, dated May 3, 
2018, for Bombardier Model BD-700-1A10 airplanes.
    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 60 airplanes of U.S. registry. We 
estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
4 work-hours x $85 per hour = $340...........................              $0             $340          $20,400
----------------------------------------------------------------------------------------------------------------

    We have determined that revising the existing maintenance or 
inspection program takes an average of 90 work-hours per operator, 
although we recognize that this number may vary from operator to 
operator. In the past, we have estimated that this action takes 1 work-
hour per airplane. Since operators incorporate maintenance or 
inspection program changes for their affected fleet(s), we have 
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, we estimate the total cost per operator 
to be $7,650 (90 work-hours x $85 per work-hour).
    We estimate the following costs to do the necessary on-condition 
action that would be required based on the results of any required 
actions. We have no way of determining the number of aircraft that 
might need this on-condition action:

                                     Estimated Costs of On-Condition Action
----------------------------------------------------------------------------------------------------------------
                                                                                                     Cost per
                                  Labor cost                                       Parts cost        product
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85..............................................         $10,847          $10,932
----------------------------------------------------------------------------------------------------------------

    According to the manufacturer, some or all 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 known costs in our cost 
estimate.

[[Page 8594]]

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. Subtitle VII: Aviation Programs, 
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in 
Subtitle VII, Part A, Subpart III, Section 44701: ``General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes and 
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

    This AD will not have federalism implications under Executive Order 
13132. This AD will not have a substantial direct effect on the States, 
on the relationship between the national government and the States, or 
on the distribution of power and responsibilities among the various 
levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13   [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2019-03-22 Bombardier, Inc.: Amendment 39-19574; Docket No. FAA-
2018-0710; Product Identifier 2018-NM-079-AD.

(a) Effective Date

    This AD is effective April 15, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Bombardier, Inc., Model BD-700-1A10 and BD-
700-1A11 airplanes, certificated in any category, serial numbers 
9002 through 9638 inclusive and 9998.

(d) Subject

    Air Transport Association (ATA) of America Code 32, Landing 
gear.

(e) Reason

    This AD was prompted by in-service findings that a cotter pin at 
the main fitting joint of the nose landing gear (NLG) retraction 
actuator to the NLG strut showed evidence of shearing after an NLG 
retraction-extension cycling. We are issuing this AD to address this 
condition, which could lead to a loss of hardware and result in an 
actuator disconnect and the NLG failing to retract or extend, or in 
an undamped freefall, which could adversely affect the airplane's 
continued safe flight and landing.

(f) Compliance

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

(g) Maintenance or Inspection Program Revision

    Within 30 days after the effective date of this AD: Revise the 
existing maintenance or inspection program, as applicable, to 
incorporate the information specified in Airworthiness Limitation 
(AWL) Task 32-33-01-111, ``Restoration of the Nose Landing Gear 
Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint,'' as 
specified in the applicable time limits/maintenance checks (TLMC) 
manual identified in figure 1 to paragraph (g) of this AD, as 
applicable. The initial compliance time for doing the task is at the 
time specified in the applicable TLMC manual listed in figure 1 to 
paragraph (g) of this AD, or within 30 days after the effective date 
of this AD, whichever occurs later.

[[Page 8595]]

[GRAPHIC] [TIFF OMITTED] TR11MR19.000

(h) Inspection and Modification

    (1) Except for airplanes identified in paragraph (h)(2) of this 
AD: Within 6 months from the effective date of this AD, perform a 
general visual inspection for damage of the cotter pin retaining the 
bolt that secures the NLG retraction actuator to the NLG strut, and 
a general visual inspection of the modification number shown on the 
identification plate for the NLG strut, and, if applicable, mark the 
correct modification number on the identification plate of the NLG 
strut, in accordance with the applicable Bombardier service 
information as shown in figure 2 to paragraph (h) of this AD. If 
damage to the cotter pin is present: Before further flight, perform 
the modification of the NLG retraction actuator hardware in 
accordance with the Accomplishment Instructions of the applicable 
Bombardier service information as shown in figure 2 to paragraph (h) 
of this AD.
    (2) The actions specified in paragraph (h)(1) of this AD are not 
required for airplanes that do not have the NLG configuration 
specified in Paragraph 1.A, ``Effectivity'' of the applicable 
Bombardier service information as shown in figure 2 to paragraph (h) 
of this AD.

[[Page 8596]]

[GRAPHIC] [TIFF OMITTED] TR11MR19.001

(i) No Alternative Actions or Intervals

    After the maintenance or inspection program has been revised as 
required by paragraph (g) of this AD, no alternative actions (e.g., 
inspections) or intervals, may be used unless the actions or 
intervals are approved as an alternative method of compliance (AMOC) 
in accordance with the procedures specified in paragraph (l)(1) of 
this AD.

(j) Credit for Previous Actions

    (1) This paragraph provides credit for actions required by 
paragraph (g) of this AD, if those actions were performed before the 
effective date of this AD using AWL Task 32-33-01-111, ``Restoration 
of the Nose Landing Gear Shock-Strut Assembly to Retraction-Actuator 
Main-Fitting Joint,'' of the applicable service information 
specified in figure 3 to paragraph (j)(1) of this AD.

[[Page 8597]]

[GRAPHIC] [TIFF OMITTED] TR11MR19.002

    (2) This paragraph provides credit for actions required by 
paragraph (h)(1) of this AD, if those actions were performed before 
the effective date of this AD using the service information 
specified in paragraphs (j)(2)(i) through (j)(2)(xiii) of this AD, 
provided that it can be confirmed that at least 25 NLG extension-
retraction cycles had been completed on the NLG at the time of 
completion of the Instructions of the applicable service information 
specified in paragraphs (j)(2)(i) through (j)(2)(xiii) of this AD; 
and provided neither the NLG nor the NLG retraction actuator has 
been replaced or modified since the completion of the Instructions 
of the applicable service information specified in paragraphs 
(j)(2)(i) through (j)(2)(xiii) of this AD.
    (i) Task 32-33-01-111of Bombardier Global 5000 Time Limits/
Maintenance Checks, Revision 19, dated November 13, 2017.
    (ii) Task 32-33-01-111of Bombardier Global 5000 Featuring Global 
Vision Flight Deck--Time Limits/Maintenance Checks, Publication No. 
GL 5000 GVFD TLMC, Revision 9, dated November 13, 2017.
    (iii) Task 32-33-01-111of Bombardier Global 6000 Time Limits/
Maintenance Checks, Publication No. GL 6000 TLMC, Revision 9, dated 
November 13, 2017.
    (iv) Task 32-33-01-111of Bombardier Global Express Time Limits/
Maintenance

[[Page 8598]]

Checks, Publication No. BD-700 TLMC, Revision 28, dated November 13, 
2017.
    (v) Task 32-33-01-111of Bombardier Global Express XRS Time 
Limits/Maintenance Checks, Publication No. BD-XRS TLMC, Revision 15, 
dated November 13, 2017.
    (vi) Bombardier Service Bulletin 700-1A11-32-022, dated May 13, 
2015.
    (vii) Bombardier Service Bulletin 700-1A11-32-022, Revision 1, 
dated August 26, 2015.
    (viii) Bombardier Service Bulletin 700-32-035, dated May 13, 
2015.
    (ix) Bombardier Service Bulletin 700-32-035, Revision 1, dated 
August 26, 2015.
    (x) Bombardier Service Bulletin 700-32-5011, dated May 13, 2015.
    (xi) Bombardier Service Bulletin 700-32-5011, Revision 1, dated 
August 26, 2015.
    (xii) Bombardier Service Bulletin 700-32-6011, dated May 13, 
2015.
    (xiii) Bombardier Service Bulletin 700-32-6011, Revision 1, 
dated August 26, 2015.

(k) Service Information Prohibition

    As of the effective date of this AD, no person may incorporate 
Liebherr-Aerospace Service Bulletin 1285A-32-07 at any revision 
level on the NLG strut assemblies of any Bombardier, Inc., Model BD-
700-1A10 or BD-700-1A11 airplane.

(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 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.

(m) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) Canadian AD CF-2018-05, dated January 23, 2018, 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-2018-0710.
    (2) For more information about this AD, contact Darren Gassetto, 
Aerospace Engineer, Mechanical Systems and Admin Services Section, 
FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, 
NY 11590; telephone 516-228-7323; fax 516-794-5531; email 9-avs-nyaco-cos@faa.gov.
    (3) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (n)(3) and (n)(4) of this AD.

(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 700-1A11-32-022, Revision 2, 
dated November 6, 2017.
    (ii) Bombardier Service Bulletin 700-32-035, Revision 2, dated 
November 6, 2017.
    (iii) Bombardier Service Bulletin 700-32-5011, Revision 2, dated 
November 6, 2017.
    (iv) Bombardier Service Bulletin 700-32-6011, Revision 2, dated 
November 6, 2017.
    (v) Task 32-33-01-111, ``Restoration of the Nose Landing Gear 
Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint,'' of 
Bombardier Global 5000 Time Limits/Maintenance Checks, Publication 
No. BD-700 TLMC, Revision 20, dated May 3, 2018.
    (vi) Task 32-33-01-111, ``Restoration of the Nose Landing Gear 
Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint,'' of 
Bombardier Global 5000 Featuring Global Vision Flight Deck Time 
Limits/Maintenance Checks, Publication No. GL 5000 GVFD TLMC, 
Revision 10, dated May 3, 2018.
    (vii) Task 32-33-01-111, ``Restoration of the Nose Landing Gear 
Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint,'' of 
Bombardier Global 6000 Time Limits/Maintenance Checks, Publication 
No. GL 6000 TLMC, Revision 10, dated May 3, 2018.
    (viii) Task 32-33-01-111, ``Restoration of the Nose Landing Gear 
Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint,'' of 
Bombardier Global Express Time Limits/Maintenance Checks, 
Publication No. BD-700 TLMC, Revision 29, dated May 3, 2018.
    (ix) Task 32-33-01-111, ``Restoration of the Nose Landing Gear 
Shock-Strut Assembly to Retraction-Actuator Main-Fitting Joint,'' of 
Bombardier Global Express XRS Time Limits/Maintenance Checks, 
Publication No. BD-700 XRS TLMC, Revision 16, dated May 3, 2018.
    (3) For service information identified in this AD, contact 
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, 
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; email thd.crj@aero.bombardier.com; 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 February 14, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2019-03255 Filed 3-8-19; 8:45 am]
BILLING CODE 4910-13-P