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2015-04-01 SHORT BROTHERS & HARLAND LTD:
( c o r r e c t i o n )

Amendment 39-18103; Docket No. FAA-2014-1001; Directorate Identifier 2014-CE-034-AD.

TDATA NOTE: The FAA is correcting  the  amendment  number  in  the  Agency
            Identification Numbers in the preamble section. It should read
            "Amendment 39-18103" instead of "Amendment 39-18003".

(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective March 30, 2015.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies  to  Short Brothers & Harland Ltd. Model SC-7 Series 3
    airplanes, all serial numbers, certificated in any category.

(d) SUBJECT

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

(e) REASON

    This AD was prompted by mandatory continuing airworthiness information
    (MCAI)  originated  by an  aviation  authority of  another  country to
    identify and correct an unsafe  condition on an aviation product.  The
    MCAI describes the  unsafe condition as  fatigue cracking which  could
    lead to  structural failure  of the  nose landing  gear (NLG).  We are
    issuing this proposed AD to detect and correct fatigue cracking which,
    if not detected and corrected, could lead to structural failure of the
    NLG, possibly  resulting in  loss of  control of  the airplane  during
    take-off or landing.

(f) ACTIONS AND COMPLIANCE

    Unless already done, comply with  this AD within the compliance  times
    specified in paragraphs (f)(1) through (f)(5) of this AD.

(1) Within 30 days  after  March 30, 2015 (the effective date of this AD),
    accomplish a visual inspection of  the NLG sliding tube following  the
    instructions of paragraph 3.A of SAFRAN Messier-Buggatti-Dowty Service
    Bulletin No. 32-17M, dated November 1, 2014.

Note  1 to  paragraphs (f)(1),  (f)(2), (f)(4),  and  (f)(5)  of this  AD:
Instructions provided  by SAFRAN  Messier-Buggatti-Dowty Service  Bulletin
No.  32-17M,  dated  November 1, 2014,  are  referenced in  Shorts Service
Bulletin Number 32-74, dated November 1, 2014.

(2) Within 90 days  after  March 30, 2015 (the effective date of this AD),
    do a fluorescent  penetrant inspection of  the sliding tube  following
    the  instructions  of  paragraph 3.B  of SAFRAN Messier-Buggatti-Dowty
    Service Bulletin No. 32-17M, dated November 1, 2014.

(3) If any crack is detected during the inspection required  by  paragraph
    (f)(1)  or  (f)(2)  of  this AD,  before  further  flight,  obtain FAA
    -approved  repair  instructions approved  specifically  for compliance
    with this AD by reporting the findings to Short Brothers & Harland Ltd
    and incorporating those instructions. You can find contact information
    for Short Brothers & Harland Ltd. in paragraph (h) of this AD.

(4) Within 30 days after  any inspection required by paragraphs (f)(1) and
    (f)(2)  of  this  AD or  within  30  days after  March  30,  2015 (the
    effective  date  of  this  AD),  whichever  occurs  later,  report the
    inspection results to Short Brothers & Harland Ltd. by completing  the
    Inspection Results  Proforma following  the instructions  of paragraph
    3.C.(2) of SAFRAN Messier-Buggatti-Dowty Service Bulletin No.  32-17M,
    dated November  1, 2014.  You can  find contact  information for Short
    Brothers & Harland Ltd. in paragraph (h) of this AD.

(5) From March 30, 2015 (the effective date of this AD), you may install a
    sliding  tube  on  an  NLG provided  that,  before  next  flight after
    installation,  the  NLG  sliding   tube  passes  the  inspections   in
    paragraphs (f)(1) and (f)(2) of this AD following the instructions  of
    paragraph 3 of  SAFRAN  Messier-Buggatti-Dowty Service Bulletin No. 32
    -17M, dated November 1, 2014.

(g) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative  Methods  of  Compliance  (AMOCs):  The Manager, Standards
    Office,  FAA,  has the authority to approve AMOCs for this AD,  if re-
    quested using the procedures found in 14 CFR 39.19.  Send  information
    to  ATTN:  Doug  Rudolph,  Aerospace  Engineer,  FAA,  Small  Airplane
    Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106;  tele-
    phone: (816) 329-4059;  fax: (816) 329-4090;  email: doug.rudolph@faa.
    gov.  Before using any approved AMOC on any airplane to which the AMOC
    applies,  notify your appropriate  principal inspector (PI) in the FAA
    Flight Standards District Office (FSDO), or lacking a PI,  your  local
    FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective
    actions from a manufacturer or other source, use these actions if they
    are FAA-approved.  Corrective actions  are considered  FAA-approved if
    they are approved by the State of Design Authority (or their delegated
    agent). You are required to assure the product is airworthy before  it
    is returned to service.

(3) Reporting  Requirements:  For any reporting requirement in this AD, a
    federal  agency  may not  conduct  or sponsor,  and  a person  is  not
    required to respond to, nor shall a person be subject to a penalty for
    failure to  comply with  a collection  of information  subject to  the
    requirements of the Paperwork Reduction Act unless that collection  of
    information  displays  a current  valid  OMB Control  Number.  The OMB
    Control Number  for this  information collection  is 2120-0056. Public
    reporting  for  this  collection of  information  is  estimated to  be
    approximately 5 minutes per response, including the time for reviewing
    instructions, completing and reviewing the collection of  information.
    All  responses  to  this  collection  of  information  are  mandatory.
    Comments concerning the  accuracy of this  burden and suggestions  for
    reducing the burden should be directed to the FAA at: 800 Independence
    Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance
    Officer, AES-200.

(h) RELATED INFORMATION

    Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2014-0246,
    dated  November 12, 2014;  and  Shorts Service Bulletin  Number 32-74,
    dated November 1, 2014, for related information. The MCAI can be found
    in  the  AD  docket  on the Internet at: http://www.regulations.gov/#!
    documentDetail;D=FAA-2014-1001-0002. For Short Brothers & Harland Ltd.
    service information identified in this AD contact Airworthiness, Short
    Brothers PLC,  P.O. Box 241,  Airport Road,  Belfast, BT3 9DZ Northern
    Ireland, United Kingdom; phone: +44-2890-462469,  fax: 44-2890-733647,
    email: michael.mulholland@aero.bombardier.com, internet: None.

(i) 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 the AD specifies otherwise.

(i) SAFRAN  Messier-Buggatti-Dowty  Service  Bulletin  No.  32-17M,  dated
    November 1, 2014.

(ii) Reserved.

(3) For  SAFRAN  Messier-Buggatti-Dowty  service information identified in
    this AD contact Messier-Dowty Limited, Cheltenham Road, Gloucester GL2
    9QH, ENGLAND; phone: +44(0)1452 712424; fax: +44(0)1452 713821; email:
    americacsc@safranmbd.com, Internet: http://www.safranmbd.com.

(4) You  may  view  this  service  information  at the FAA, Small Airplane
    Directorate, 901 Locust, Kansas City, Missouri 64106.  For information
    on the availability of this material at the FAA,  call (816) 329-4148.
    In  addition,  you can access this service information on the Internet
    at http://www.regulations.gov by searching for and locating Docket No.
    FAA-2014-1001.

(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 Kansas City, Missouri, on February 6, 2015. Robert Busto, Acting
Manager, Small Airplane Directorate, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Doug Rudolph,  Aerospace  Engineer,  FAA,
Small Airplane Directorate,  901 Locust,  Room 301,  Kansas City, Missouri
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email: doug.rudolph
@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-1001; Directorate Identifier 2014-CE-034-AD;
Amendment 39-18103; AD 2015-04-01]
RIN 2120-AA64

Airworthiness Directives; Short Brothers & Harland Ltd. Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for Short
Brothers & Harland Ltd. Model SC-7 Series 3 airplanes. This AD results
from mandatory continuing airworthiness information (MCAI) issued by an
aviation authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as fatigue cracking, which could lead to structural failure
of the nose landing gear (NLG). We are issuing this AD to require
actions to address the unsafe condition on these products.

DATES: This AD is effective March 30, 2015.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of March 30,
2015.

ADDRESSES: You may examine the AD docket on the Internet at http://
www.regulations.gov by searching for and locating Docket No. FAA-2014-
1001; or in person at Document 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 service information identified in this AD, contact Short
Brothers & Harland Ltd. service information identified in this proposed
AD, contact Airworthiness, Short Brothers PLC, P.O. Box 241, Airport
Road, Belfast, BT3 9DZ Northern Ireland, United Kingdom; phone: +44-
2890-462469, fax: 44-2890-733647, email:
michael.mulholland@aero.bombardier.com, internet: None; and for SAFRAN
Messier-Buggatti-Dowty service information contact Messier-Dowty
Limited, Cheltenham Road, Gloucester GL2 9QH, ENGLAND; phone:
+44(0)1452 712424; fax: +44(0)1452 713821; email:
americacsc@safranmbd.com, Internet: http://www.safranmbd.com. You may
view this referenced service information at the FAA, Small Airplane
Directorate, 901 Locust, Kansas City, Missouri 64106. For information
on the availability of this material at the FAA, call (816) 329-4148.
You can also find this service information on the Internet at http://www.
regulations.gov by searching for and locating Docket No. FAA-2014-
1001. It is also available on the Internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2014-1001.

FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email:
doug.rudolph@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to adding an AD that would apply to Short Brothers & Harland
Ltd Model SC-7 Series 3 airplane. The NPRM was published in the Federal
Register on December 8, 2014 (79 FR 72562). The NPRM proposed to
correct an unsafe condition for the specified products and was based on
mandatory continuing airworthiness information (MCAI) originated by an
aviation authority of another country. The MCAI states:

A fracture of the nose landing gear (NLG) sliding tube was
reported. The subsequent investigation determined fatigue cracking
as possible cause of the failure.
This condition, if not detected and corrected, could lead to
structural failure of the NLG, possibly resulting in loss of control
of the aeroplane during take-off or landing.
To address this unsafe condition, the Messier-Dowty Ltd, the NLG
manufacturer, issued Service Bulletin (SB) 32-17M to provide
inspection instructions. Consequently Short Brothers PLC issued SB
32-74 which references Messier-Dowty Ltd SB 32-17M.
For the reasons described above, this AD requires one-time
visual and fluorescent penetrant inspections and, depending on
findings, accomplishment of applicable corrective action(s).

The MCAI requires you report the findings to Short Brothers PLC to
obtain FAA-approved repair instructions and accomplish the repair
accordingly. The MCAI can be found in the AD docket on the Internet at:
http://www.regulations.gov/#!documentDetail;D=FAA-2014-1001-0002.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 72562, December 8,
2014) 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 the 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 (79 FR 72562, December 8, 2014) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 72562, December 8, 2014).

Relative Service Information Under 1 CFR Part 51

We reviewed Short Brothers & Harland Ltd. Shorts Service Bulletin
Number 32-74, dated November 1, 2014; and SAFRAN Messier-Buggatti-Dowty
Service Bulletin No. 32-17M, dated November 1, 2014. The Shorts Service
Bulletin Number 32-74, dated November 1, 2014, and SAFRAN Messier-
Buggatti-Dowty Service Bulletin No. 32-17M, dated November 1, 2014,
describe procedures for a visual inspection and a fluorescent penetrant
inspection (FPI) for cracking of the NLG
Sliding Tube. This service information is reasonably available; see
ADDRESSES for ways to access this service information.

Costs of Compliance

We estimate that this AD will affect 24 products of U.S. registry.
We also estimate that it would take about 5 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour.
Based on these figures, we estimate the cost of the AD on U.S.
operators to be $10,200, or $425 per product.
In addition, we estimate that any necessary follow-on actions would
take about 16 work-hours and require parts costing $25,000, for a cost
of $26,360 per product. We have no way of determining the number of
products that may need these actions.

Paperwork Reduction Act

A federal agency may not conduct or sponsor, and a person is not
required to respond to, nor shall a person be subject to penalty for
failure to comply with a collection of information subject to the
requirements of the Paperwork Reduction Act unless that collection of
information displays a current valid OMB control number. The control
number for the collection of information required by this AD is 2120-
0056. The paperwork cost associated with this AD has been detailed in
the Costs of Compliance section of this document and includes time for
reviewing instructions, as well as completing and reviewing the
collection of information. Therefore, all reporting associated with
this AD is mandatory. Comments concerning the accuracy of this burden
and suggestions for reducing the burden should be directed to the FAA
at 800 Independence Ave. SW., Washington, DC 20591. ATTN: Information
Collection Clearance Officer, AES-200.

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 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 by searching for and locating Docket No. FAA-2014-
1001; 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 the NPRM, the regulatory evaluation, any comments received,
and other information. The street address for the Docket Office
(telephone (800) 647-5527) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

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 AD: