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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.
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