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2015-20-07 BOMBARDIER, INC.: Amendment 39-18286. Docket No. FAA-2014-1046; Directorate Identifier 2014-NM-021-AD.
(a) EFFECTIVE DATE

    This AD becomes effective November 10, 2015.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to the  airplanes identified in paragraphs (c)(1)  and
    (c)(2) of this AD, certificated in any category.

(1) Bombardier, Inc.  Model CL-600-2C10 (Regional Jet Series  700,  701, &
    702) airplanes, serial number (S/N) 10002 and subsequent.

(2) Bombardier, Inc.  Model CL-600-2D15 (Regional Jet Series 705), and CL-
    600-2D24 (Regional Jet Series 900) airplanes S/N 15001 and subsequent.

(d) SUBJECT

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

(e) REASON

    This  AD was  prompted by  a  determination  that no  instructions for
    continued  airworthiness  exist  for  the  nose  landing  gear   (NLG)
    alternate extension actuator of  the NLG alternate release  system. We
    are issuing this  AD to prevent  failure of the  NLG alternate release
    system and, if the normal NLG extension system also fails, failure  of
    the NLG to extend, and consequent damage to the airplane and injury to
    occupants.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) MAINTENANCE OR INSPECTION PROGRAM REVISION

    Within  30  days after  the  effective date  of  this AD,  revise  the
    maintenance or inspection program,  as applicable, to incorporate  the
    information  specified  in  Task 320100-225,  Restoration  of  the NLG
    Manual Release Actuator, of Subject 1-32, Landing Gear, of Section  1,
    Systems and Powerplant Program, Volume 1 of Part 1, Maintenance Review
    Board  Report,  Revision  14,  dated   July  10,  2013,  of  the   CRJ
    700/900/1000 Maintenance Requirements  Manual, CSP-B-053. The  initial
    compliance time for the task is specified in paragraph (h) of this AD.

(h) INITIAL TASK COMPLIANCE TIME

    Before the accumulation of 20,000 total flight cycles, or within 5,500
    flight cycles after  the effective date  of this AD,  whichever occurs
    later: Perform the initial  restoration specified in Task  320100-225,
    Restoration  of  the NLG  Manual  Release Actuator,  of  Subject 1-32,
    Landing Gear, of Section 1,  Systems and Powerplant Program, Volume  1
    of Part 1,  Maintenance Review Board  Report, Revision 14,  dated July
    10, 2013,  of the  CRJ 700/900/1000  Maintenance Requirements  Manual,
    CSP-B-053.

(i) NO ALTERNATIVE ACTIONS AND INTERVALS

    After accomplishing the revision 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 (j)(1) of this AD.

(j) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager, New York Air-
    craft 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 ACO, send  it to
    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. The AMOC  approval letter
    must specifically reference this AD.

(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, Engine  and Propeller  Directorate, 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.

(k) RELATED INFORMATION

    Refer  to  MCAI  Canadian Airworthiness Directive CF-2013-24R1,  dated
    December 24, 2013, for related information.  This MCAI may be found in
    the AD docket on the Internet at http://www.regulations.gov/#!document
    Detail;D=FAA-2014-1046-0002.

(l) MATERIAL INCORPORATED BY REFERENCE

(1) The  Director  of  the  Federal Register approved the incorporation by
    reference (IBR) of the  service  information  listed in this paragraph
    under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this  service information as applicable to do the actions
    required by this AD, unless this AD specifies otherwise.

(i) Task  320100-225,  Restoration of the NLG Manual Release Actuator,  of
    Subject 1-32,  Landing Gear,  of  Section 1,  Systems  and  Powerplant
    Program, Volume 1 of Part 1, Maintenance Review Board Report, Revision
    14, dated July 10, 2013,  of the CRJ 700/900/1000 Maintenance Require-
    ments Manual, CSP-B-053.

(ii) Reserved.

(3) For service information identified in this AD,  Bombardier, Inc.,  400
    Cote-Vertu Road West, Dorval,  Quebec H4S 1Y9, Canada;  telephone 514-
    855-5000; fax 514-855-7401;  email thd.crj@aero.bombardier.com; Inter-
    net 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 September 27, 2015.  Michael Kaszycki,
Acting  Manager,  Transport Airplane  Directorate,  Aircraft Certification
Service.

FOR FURTHER INFORMATION CONTACT: Luke Walker, 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 516-228-7363; fax 516-794-5531.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-1046; Directorate Identifier 2014-NM-021-AD;
Amendment 39-18286; AD 2015-20-07]
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 CL-600-2C10 (Regional Jet Series 700, 701, &
702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional
Jet Series 900) airplanes. This AD was prompted by a determination that
no instructions for continued airworthiness exist for the nose landing
gear (NLG) alternate extension actuator of the NLG alternate release
system. This AD requires revising the maintenance or inspection
program, as applicable, to incorporate a new airworthiness limitation
task for the NLG alternate extension actuator. We are issuing this AD
to prevent failure of the NLG alternate release system and, if the
normal NLG extension system also fails, failure of the NLG to extend,
and consequent damage to the airplane and injury to occupants.

DATES: This AD becomes effective November 10, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 10,
2015.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-1046 or in person at the
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.
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. 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-2014-1046.

FOR FURTHER INFORMATION CONTACT: Luke Walker, 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 516-228-7363; 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 CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15
(Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900)
airplanes. The NPRM published in the Federal Register on January 23,
2015 (80 FR 3502).
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2013-24R1, dated December 24, 2013 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for certain Bombardier, Inc. Model CL-600-
2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet
Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes. The
MCAI states:

It was discovered that there are no instructions for continued
airworthiness for the Nose Landing Gear (NLG) alternate extension
actuator. Without an effective maintenance task to maintain the
aeroplane's inherent level of safety, there is a potential that a
dormant failure of the alternate release system of the NLG could
occur. Failure of the NLG alternate release system could prevent the
nose landing gear from extending in the case of a failure of the
normal NLG extension system.
This [Canadian] AD is to mandate the incorporation of a new
maintenance task to prevent failure of the NLG alternate release
system.
Revision 1 of this [Canadian] AD changes the phase-in time to be
based on the NLG manual release actuators instead of aeroplanes.

You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-1046-0002.

Comments

We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM (80
FR 3502, January 23, 2015) and the FAA's response to each comment.

Support for the NPRM (80 FR 3502, January 23, 2015)

Airline Pilots Association (ALPA) International agreed with the
intent of the NPRM (80 FR 3502, January 23, 2015).

Request To Revise Compliance Time

Envoy Airlines and Mesa Airlines asked that we revise the
compliance time language in paragraph (h) of the proposed AD (80 FR
3502, January 23, 2015) from ``whichever occurs first'' to ``whichever
occurs later.'' The compliance time, as written, could result in
airplanes being grounded. Envoy Airlines added that the compliance time
referred to in the TCCA AD is ``whichever occurs later.'' Mesa Airlines
noted that changing the compliance time would also allow for scheduling
and parts procurement.
We agree with the commenters' request for the reasons provided, and
due to the fact that this was an inadvertent error. We have revised the
compliance time in paragraph (h) of this AD as requested.

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 change described previously and minor editorial
changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (80 FR 3502, January 23, 2015) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (80 FR 3502, January 23, 2015).
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, Inc. has issued Task 320100-225, Restoration of the NLG
Manual Release Actuator, of Subject 1-32, Landing Gear, of Section 1,
Systems and Powerplant Program, Volume 1 of Part 1, Maintenance Review
Board Report, Revision 14, dated July 10, 2013, of the CRJ 700/900/1000
Maintenance Requirements Manual, CSP-B-053. This service information
describes an airworthiness limitation task for the NLG alternate
extension actuator. 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
of this AD.

Costs of Compliance

We estimate that this AD affects 416 airplanes of U.S. registry.
We also estimate that it takes about 1 work-hour per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts will cost about $0 per product.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $35,360, or $85 per product.
In addition, we estimate that any necessary follow-on actions take
about 1 work-hour and require parts costing $0, for a cost of $85 per
product. We have no way of determining the number of aircraft that
might need these actions.

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.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-1046; 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 Operations office (telephone 800-647-
5527) is in the ADDRESSES section.

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

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]

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