80 FR 14299 - Airworthiness Directives; Short Brothers & Harland Ltd. Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 80, Issue 53 (March 19, 2015)

Page Range		14299-14301
FR Document		2015-06235

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Short Brothers & Harland Ltd. Model SC-7 Series 3 airplanes. The amendment number in the Agency Identification Numbers in the preamble section of the AD is incorrect. Although no other part of the preamble or regulatory information has been corrected, we are publishing the entire rule in the Federal Register.

Federal Register, Volume 80 Issue 53 (Thursday, March 19, 2015)

[Federal Register Volume 80, Number 53 (Thursday, March 19, 2015)]
[Rules and Regulations]
[Pages 14299-14301]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2015-06235]


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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), DOT.

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting an airworthiness directive (AD) that 
published in the Federal Register. That AD applies to all Short 
Brothers & Harland Ltd. Model SC-7 Series 3 airplanes. The amendment 
number in the Agency Identification Numbers in the preamble section of 
the AD is incorrect. Although no other part of the preamble or 
regulatory information has been corrected, we are publishing the entire 
rule in the Federal Register.

DATES: This final rule is effective March 30, 2015.

ADDRESSES: You may examine the AD docket on the Internet at http://

[[Page 14300]]

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: 
[email protected], 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: 
[email protected], 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. 
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: 
[email protected].

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2015-04-01, 
Amendment 39-18003 (80 FR 9382, February 23, 2015), currently requires 
a visual inspection of the NLG sliding tube and a fluorescent penetrant 
inspection of the sliding tube. If any crack is detected during either 
inspection, before further flight, obtain FAA-approved repair 
instructions approved specifically for compliance with this AD by 
reporting the findings, and incorporating those instructions for Short 
Brothers & Harland Ltd. Model SC-7 Series 3 airplanes, all serial 
numbers, certificated in any category.
    As published, the amendment number in the Agency Identification 
Numbers in the preamble section of the AD is incorrect. It has been 
corrected in this document.
    Although no other part of the preamble or regulatory information 
has been corrected, we are publishing the entire rule in the Federal 
Register.
    The effective date of this AD remains March 30, 2015.

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 AD:

2015-04-01 Short Brothers & Harland Ltd: Amendment 39-18103; Docket 
No. FAA-2014-1001; Directorate Identifier 2014-CE-034-AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective on 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 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 requested 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; telephone: (816) 329-4059; fax: (816) 329-4090; email: 
[email protected]. 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

[[Page 14301]]

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: 
[email protected], 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: [email protected], 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.
    (6) 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 March 11, 2015.
Robert Busto,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-06235 Filed 3-18-15; 8:45 am]
BILLING CODE 4910-13-P

Federal Register / Vol. 80, No. 53 / Thursday, March 19, 2015 / Rules and Regulations 14299

We are issuing this rulemaking under (a) Applicability (h) Additional Information
the authority described in Subtitle VII, This AD applies to the following (1) AgustaWestland S.p.A. Bollettino
Part A, Subpart III, Section 44701, helicopters, certificated in any category: Tecnico (BT) No. 109S–49, BT No. 109SP–
‘‘General requirements.’’ Under that (1) Agusta S.p.A. (Agusta) Model A109S 052, and BT No. 119–50, all Revision A, and
section, Congress charges the FAA with and AW109SP helicopters, with a main rotor all dated December 3, 2013, which are not
promoting safe flight of civil aircraft in lag damper assembly (lag damper), part incorporated by reference, contain additional
number (P/N) 109–0112–39–103 or 109– information about the subject of this AD. For
air commerce by prescribing regulations service information identified in this AD,
for practices, methods, and procedures 0112–39–105, installed on rod end assembly,
P/N M004–01H007–041 with a serial number contact AgustaWestland, Product Support
the Administrator finds necessary for Engineering, Via del Gregge, 100, 21015
(S/N) 1 through 202; or rod end assembly, P/
safety in air commerce. This regulation N M004–01H007–045 with a S/N 1RW Lonate Pozzolo (VA) Italy, ATTN: Maurizio
is within the scope of that authority through 202RW or 4964 through 5011. D’Angelo; telephone 39–0331–664757; fax
because it addresses an unsafe condition (2) Agusta Model A119 and AW119 MKII 39–0331–664680; or at http://
that is likely to exist or develop on www.agustawestland.com/technical-
helicopters, with a lag damper, P/N 109–
products identified in this rulemaking bulletins. You may review a copy of the
0112–05–105 or 109–0112–05–107, installed
service information at the FAA, Office of the
action. on rod end assembly, P/N 109–0112–11–101
Regional Counsel, Southwest Region, 2601
with a S/N 1 through 78; or rod end Meacham Blvd., Room 663, Fort Worth,
Regulatory Findings assembly, P/N 109–0112–11–105 with a S/N Texas 76137.
We have determined that this AD will 1RW through 78RW; or rod end assembly, P/ (2) The subject of this AD is addressed in
not have federalism implications under N M004–01H007–045 with a S/N 1RW the European Aviation Safety Agency (EASA)
Executive Order 13132. This AD will through 202RW or 4964 through 5011. AD No. 2013–0290, dated December 9, 2013.
not have a substantial direct effect on (b) Unsafe Condition You may view the EASA AD on the Internet
the States, on the relationship between at http://www.regulations.gov in Docket No.
This AD defines the unsafe condition as a FAA–2014–0579.
the national government and the States, crack in a rod end assembly, which could
or on the distribution of power and result in fracture of the rod end assembly, (i) Subject
responsibilities among the various damage to the main rotor, and subsequent Joint Aircraft Service Component (JASC)
levels of government. loss of control of the helicopter. Code: 6200, Main Rotor System.
For the reasons discussed above, I (c) Affected ADs Issued in Fort Worth, Texas, on March 4,
certify that this AD: 2015.
This AD supersedes AD 2014–04–14,
(1) Is not a ‘‘significant regulatory Bruce E. Cain,
amendment 39–17773 (79 FR 11699, March
action’’ under Executive Order 12866, 3, 2014). Acting Directorate Manager, Rotorcraft
(2) Is not a ‘‘significant rule’’ under Directorate, Aircraft Certification Service.
DOT Regulatory Policies and Procedures (d) Effective Date
[FR Doc. 2015–05715 Filed 3–18–15; 8:45 am]
(44 FR 11034, February 26, 1979), This AD becomes effective April 23, 2015.
BILLING CODE 4910–13–P
(3) Will not affect intrastate aviation (e) Compliance
in Alaska, and
You are responsible for performing each
(4) Will not have a significant DEPARTMENT OF TRANSPORTATION
action required by this AD within the
economic impact, positive or negative, specified compliance time unless it has
on a substantial number of small entities already been accomplished prior to that time. Federal Aviation Administration
under the criteria of the Regulatory
Flexibility Act. (f) Required Actions 14 CFR Part 39
(1) Within 25 hours time-in-service or the
List of Subjects in 14 CFR Part 39 next time maintenance of the helicopter [Docket No. FAA–2014–1001; Directorate
involves removing the rod end assembly, Identifier 2014–CE–034–AD; Amendment
Air transportation, Aircraft, Aviation 39–18103; AD 2015–04–01]
safety, Incorporation by reference, whichever occurs first, remove the rod end
Safety. assembly from service. RIN 2120–AA64
(2) Do not install a rod end assembly, P/
Adoption of the Amendment N M004–01H007–041 with a S/N 1 through Airworthiness Directives; Short
202; P/N M004–01H007–045 with a S/N 1RW Brothers & Harland Ltd. Airplanes
Accordingly, under the authority through 202RW or 4964 through 5011; P/N
delegated to me by the Administrator, 109–0112–11–101 with a S/N 1 through 78; AGENCY: Federal Aviation
the FAA amends 14 CFR part 39 as or P/N 109–0112–11–105 with a S/N 1RW Administration (FAA), DOT.
follows: through 78RW, on any helicopter. ACTION: Final rule; correction.
PART 39—AIRWORTHINESS (g) Alternative Methods of Compliance
(AMOCs) SUMMARY: The FAA is correcting an
DIRECTIVES airworthiness directive (AD) that
(1) The Manager, Safety Management
published in the Federal Register. That
■ 1. The authority citation for part 39 Group, FAA, may approve AMOCs for this
AD. Send your proposal to: Robert Grant,
AD applies to all Short Brothers &
continues to read as follows: Harland Ltd. Model SC–7 Series 3
Aviation Safety Engineer, Safety Management
Authority: 49 U.S.C. 106(g), 40113, 44701. Group, FAA, 2601 Meacham Blvd., Fort airplanes. The amendment number in
Worth, Texas 76137; telephone (817) 222– the Agency Identification Numbers in
§ 39.13 [Amended] 5110; email robert.grant@faa.gov. the preamble section of the AD is
■ 2. The FAA amends § 39.13 by (2) For operations conducted under a 14 incorrect. Although no other part of the
CFR part 119 operating certificate or under preamble or regulatory information has
Rmajette on DSK2VPTVN1PROD with RULES

removing Airworthiness Directive (AD)
2014–04–14, Amendment 39–17773 (79 14 CFR part 91, subpart K, we suggest that been corrected, we are publishing the
you notify your principal inspector, or entire rule in the Federal Register.
FR 11699, March 3, 2014), and adding lacking a principal inspector, the manager of
the following new AD: DATES: This final rule is effective March
the local flight standards district office or
2015–05–05 Agusta S.p.A.: Amendment 39– certificate holding district office, before 30, 2015.
18115; Docket No. FAA–2014–0579; operating any aircraft complying with this ADDRESSES: You may examine the AD
Directorate Identifier 2014–SW–020–AD. AD through an AMOC. docket on the Internet at http://

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14300 Federal Register / Vol. 80, No. 53 / Thursday, March 19, 2015 / Rules and Regulations

www.regulations.gov by searching for been corrected, we are publishing the paragraph 3.B of SAFRAN Messier-Buggatti-
and locating Docket No. FAA–2014– entire rule in the Federal Register. Dowty Service Bulletin No. 32–17M, dated
1001; or in person at Document The effective date of this AD remains November 1, 2014.
(3) If any crack is detected during the
Management Facility, U.S. Department March 30, 2015.
inspection required by paragraph (f)(1) or
of Transportation, Docket Operations, (f)(2) of this AD, before further flight, obtain
M–30, West Building Ground Floor, PART 39—AIRWORTHINESS FAA-approved repair instructions approved
Room W12–140, 1200 New Jersey DIRECTIVES specifically for compliance with this AD by
Avenue SE., Washington, DC 20590. reporting the findings to Short Brothers &
■ 1. The authority citation for part 39 Harland Ltd. and incorporating those
For service information identified in
continues to read as follows: instructions. You can find contact
this AD, contact Short Brothers &
Authority: 49 U.S.C. 106(g), 40113, 44701. information for Short Brothers & Harland Ltd.
Harland Ltd. service information
in paragraph (h) of this AD.
identified in this proposed AD, contact § 39.13 [Amended] (4) Within 30 days after any inspection
Airworthiness, Short Brothers PLC, P.O. required by paragraphs (f)(1) and (f)(2) of this
Box 241, Airport Road, Belfast, BT3 9DZ ■ 2. The FAA amends § 39.13 by adding AD or within 30 days after March 30, 2015
Northern Ireland, United Kingdom; the following new AD: (the effective date of this AD), whichever
phone: +44–2890–462469, fax: 44– 2015–04–01 Short Brothers & Harland Ltd: occurs later, report the inspection results to
2890–733647, email: Amendment 39–18103; Docket No. Short Brothers & Harland Ltd. by completing
michael.mulholland@ FAA–2014–1001; Directorate Identifier the Inspection Results Proforma following
aero.bombardier.com, internet: None; 2014–CE–034–AD. the instructions of paragraph 3.C.(2) of
SAFRAN Messier-Buggatti-Dowty Service
and for SAFRAN Messier-Buggatti- (a) Effective Date Bulletin No. 32–17M, dated November 1,
Dowty service information contact This airworthiness directive (AD) becomes 2014. You can find contact information for
Messier-Dowty Limited, Cheltenham effective on March 30, 2015. Short Brothers & Harland Ltd. in paragraph
Road, Gloucester GL2 9QH, ENGLAND; (h) of this AD.
phone: +44(0)1452 712424; fax: (b) Affected ADs (5) From March 30, 2015 (the effective date
+44(0)1452 713821; email: americacsc@ None. of this AD), you may install a sliding tube on
safranmbd.com, Internet: http:// an NLG provided that, before next flight after
(c) Applicability
www.safranmbd.com. You may view installation, the NLG sliding tube passes the
This AD applies to Short Brothers & inspections in paragraphs (f)(1) and (f)(2) of
this referenced service information at Harland Ltd. Model SC–7 Series 3 airplanes, this AD following the instructions of
the FAA, Small Airplane Directorate, all serial numbers, certificated in any paragraph 3 of SAFRAN Messier-Buggatti-
901 Locust, Kansas City, Missouri category. Dowty Service Bulletin No. 32–17M, dated
64106. For information on the November 1, 2014.
(d) Subject
availability of this material at the FAA,
call (816) 329–4148. It is also available Air Transport Association of America (g) Other FAA AD Provisions
on the Internet at http:// (ATA) Code 32: Landing Gear. The following provisions also apply to this
www.regulations.gov by searching for (e) Reason AD:
and locating Docket No. FAA–2014– (1) Alternative Methods of Compliance
This AD was prompted by mandatory (AMOCs): The Manager, Standards Office,
1001. continuing airworthiness information (MCAI) FAA, has the authority to approve AMOCs
originated by an aviation authority of another for this AD, if requested using the procedures
FOR FURTHER INFORMATION CONTACT:
country to identify and correct an unsafe found in 14 CFR 39.19. Send information to
Doug Rudolph, Aerospace Engineer, condition on an aviation product. The MCAI
FAA, Small Airplane Directorate, 901 ATTN: Doug Rudolph, Aerospace Engineer,
describes the unsafe condition as fatigue FAA, Small Airplane Directorate, 901 Locust,
Locust, Room 301, Kansas City, cracking which could lead to structural Room 301, Kansas City, Missouri 64106;
Missouri 64106; telephone: (816) 329– failure of the nose landing gear (NLG). We are telephone: (816) 329–4059; fax: (816) 329–
4059; fax: (816) 329–4090; email: issuing this AD to detect and correct fatigue 4090; email: doug.rudolph@faa.gov. Before
doug.rudolph@faa.gov. cracking which, if not detected and using any approved AMOC on any airplane
corrected, could lead to structural failure of to which the AMOC applies, notify your
SUPPLEMENTARY INFORMATION: the NLG, possibly resulting in loss of control
Airworthiness Directive 2015–04–01, appropriate principal inspector (PI) in the
of the airplane during take-off or landing. FAA Flight Standards District Office (FSDO),
Amendment 39–18003 (80 FR 9382, or lacking a PI, your local FSDO.
February 23, 2015), currently requires a (f) Actions and Compliance
(2) Airworthy Product: For any
visual inspection of the NLG sliding Unless already done, comply with this AD requirement in this AD to obtain corrective
tube and a fluorescent penetrant within the compliance times specified in actions from a manufacturer or other source,
inspection of the sliding tube. If any paragraphs (f)(1) through (f)(5) of this AD. use these actions if they are FAA-approved.
(1) Within 30 days after March 30, 2015
crack is detected during either (the effective date of this AD), accomplish a
Corrective actions are considered FAA-
inspection, before further flight, obtain approved if they are approved by the State
visual inspection of the NLG sliding tube of Design Authority (or their delegated
FAA-approved repair instructions following the instructions of paragraph 3.A of
approved specifically for compliance agent). You are required to assure the product
SAFRAN Messier-Buggatti-Dowty Service is airworthy before it is returned to service.
with this AD by reporting the findings, Bulletin No. 32–17M, dated November 1, (3) Reporting Requirements: For any
and incorporating those instructions for 2014. reporting requirement in this AD, a federal
Short Brothers & Harland Ltd. Model Note 1 to paragraphs (f)(1), (f)(2), (f)(4), agency may not conduct or sponsor, and a
SC–7 Series 3 airplanes, all serial and (f)(5) of this AD: Instructions provided person is not required to respond to, nor
numbers, certificated in any category. by SAFRAN Messier-Buggatti-Dowty Service shall a person be subject to a penalty for
Bulletin No. 32–17M, dated November 1, failure to comply with a collection of
Rmajette on DSK2VPTVN1PROD with RULES

As published, the amendment number
2014, are referenced in Shorts Service information subject to the requirements of
in the Agency Identification Numbers in Bulletin Number 32–74, dated November 1,
the preamble section of the AD is the Paperwork Reduction Act unless that
2014. collection of information displays a current
incorrect. It has been corrected in this (2) Within 90 days after March 30, 2015 valid OMB Control Number. The OMB
document. (the effective date of this AD), do a Control Number for this information
Although no other part of the fluorescent penetrant inspection of the collection is 2120–0056. Public reporting for
preamble or regulatory information has sliding tube following the instructions of this collection of information is estimated to

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Document Created: 2018-02-21 09:42:21
Document Modified: 2018-02-21 09:42:21

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Rules and Regulations
Action		Final rule; correction.
Dates		This final rule is effective March 30, 2015.
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: [email protected]
FR Citation		80 FR 14299
RIN Number		2120-AA64

80 FR 14299 - Airworthiness Directives; Short Brothers & Harland Ltd. Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 80, Issue 53 (March 19, 2015)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration