Airworthiness Directives; British Aerospace (Operations) Limited Airplanes, 23897-23900 [2014-09540]
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Federal Register / Vol. 79, No. 82 / Tuesday, April 29, 2014 / Rules and Regulations
53A2473, Revision 4, dated December 1,
2011, specifies to contact Boeing for repair
instructions, the repair instructions must be
approved in accordance with the procedures
specified in paragraph (q) of this AD. All
provisions of AD 2010–14–07 that are not
specifically referenced in this paragraph
remain fully applicable and must be
complied with.
(2) Accomplishing the inspections, repairs,
and interim modification in accordance with
Boeing Alert Service Bulletin 747–53A2427,
Revision 7, dated July 19, 2013, is an
acceptable terminating action for the
corresponding inspections, repairs and
interim modification at the BS 2598 bulkhead
required by paragraphs (i), (j), (o), (s), (t), (u),
and (v) of AD 2010–14–07, Amendment 39–
16352 (75 FR 38001, July 1, 2010). Where
Boeing Alert Service Bulletin 747–53A2427,
Revision 7, dated July 19, 2013, specifies to
contact Boeing for repair data, the repair data
must be approved in accordance with the
procedures specified in paragraph (q) of this
AD. All provisions of AD 2010–14–07 that
are not specifically referenced in this
paragraph remain fully applicable and must
be complied with.
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(p) Credit for Previous Actions
This paragraph provides credit for the
actions required by paragraphs (g), (h), (i),
and (n)(2) of this AD, if those actions were
performed before the effective date of this AD
using Boeing Alert Service Bulletin 747–
53A2427, Revision 6, dated July 14, 2011,
provided that the additional actions added in
Boeing Alert Service Bulletin 747–53A2427,
Revision 7, dated July 19, 2013, are done
within the applicable compliance times
specified in paragraphs (g), (h), and (i) of this
AD. Boeing Alert Service Bulletin 747–
53A2427, Revision 6, dated July 14, 2011, is
not incorporated by reference in this AD.
(q) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Seattle Aircraft
Certification Office (ACO), 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 ACO, send it to the
attention of the person identified in
paragraph (r)(1) of this AD. Information may
be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov.
(2) 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.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair
required by this AD if it is approved by the
Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has
been authorized by the Manager, Seattle
ACO, to make those findings. For a repair
method to be approved, the repair must meet
the certification basis of the airplane, and the
approval must specifically refer to this AD.
(4) Related portions or applicable
paragraphs of AMOCs approved previously
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in accordance with AD 2010–14–07,
Amendment 39–16352 (75 FR 38001, July 1,
2010), are approved as AMOCs for the
corresponding provisions of paragraphs (g),
(h), (i), (j), (k), and (l) of this AD. All new
actions specified in paragraphs (g), (h), (i), (j),
(k), and (l) of this AD that are not identified
in a previously approved AMOC must still be
done.
(1) For more information about this AD,
contact Nathan Weigand, Aerospace
Engineer, Airframe Branch, ANM–120S,
FAA, Seattle ACO, 1601 Lind Avenue SW.,
Renton, WA 98057–3356; phone: 425–917–
6428; fax: 425–917–6590; email:
nathan.p.weigand@faa.gov.
(2) Service information identified in this
AD that is not incorporated by reference in
this AD may be viewed at the addresses
specified in paragraphs (s)(3) and (s)(4) of
this AD.
(s) 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) Boeing Alert Service Bulletin 747–
53A2427, Revision 7, dated July 19, 2013.
(ii) Boeing Service Bulletin 747–53A2473,
Revision 4, dated December 1, 2011.
(iii) Boeing Alert Service Bulletin 747–
53A2837, dated July 13, 2012.
(3) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Data & Services
Management, P.O. Box 3707, MC 2H–65,
Seattle, WA 98124–2207; telephone 206–
544–5000, extension 1; fax 206–766–5680;
Internet https://www.myboeingfleet.com.
(4) You may view this service information
at 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: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Renton, Washington, on March
17, 2014.
Dionne Palermo,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2014–07339 Filed 4–28–14; 8:45 am]
BILLING CODE 4910–13–P
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0020; Directorate
Identifier 2013–CE–039–AD; Amendment
39–17821; AD 2014–07–07]
RIN 2120–AA64
(r) Related Information
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Airworthiness Directives; British
Aerospace (Operations) Limited
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are superseding an
airworthiness directive (AD) 87–02–04
for British Aerospace (Operations)
Limited Model HP.137 Jetstream MK.1,
Jetstream Series 200, and Jetstream
Series 3101 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 cracking of the forward
main landing gear yoke pintle resulting
from corrosion pits leading to stress
corrosion. We are issuing this AD to
require actions to address the unsafe
condition on these products.
DATES: This AD is effective June 3, 2014.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of June 3, 2014.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2014–
0020; 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 20590.
For service information identified in
this AD, contact BAE Systems
(Operations) Ltd, Customer Information
Department, Prestwick International
Airport, Ayrshire, KA9 2RW, Scotland,
United Kingdom; phone: +44 1292
675207, fax: +44 1292 675704; email:
RApublications@baesystems.com;
Internet: https://
www.jetstreamcentral.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.
SUMMARY:
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FOR FURTHER INFORMATION CONTACT
Taylor Martin, Aerospace Engineer,
FAA, Small Airplane Directorate, 901
Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329–
4138; fax: (816) 329–4090; email:
taylor.martin@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
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We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to add an AD that would apply
to British Aerospace (Operations)
Limited Model HP 137 Jetstream MK1,
Jetstream Series 200, and Jetstream
Series 3101 airplanes. The NPRM was
published in the Federal Register on
January 15, 2014 (79 FR 2593), and
proposed to supersede AD 87–02–04,
Amendment 39–5497 (51 FR 47211,
December 31, 1986).
The NPRM (79 FR 2593, January 15,
2014) 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 that:
Prompted by occurrences of the main
landing gear (MLG) yoke pintle housing
cracking, the United Kingdom Civil Aviation
Authority (UK CAA) issued AD G–003–01–86
to require repetitive inspections to identify
any crack in the yoke pintle housing on MLG
fitted to Jetstream 3100 aeroplanes in
accordance with BAE Systems (Operations)
Ltd Service Bulletin (SB) 32–A–JA851226,
and depending on findings, corrective action.
After that AD was issued, an occurrence of
Jetstream 3100 MLG failure was reported
after landing. The subsequent investigation
revealed stress corrosion cracking of the MLG
yoke pintle housing as a root cause of the
MLG failure. Furthermore, the investigation
report recommended a review of the
effectiveness of UK CAA AD G–003–01–86 in
identifying cracks in the yoke pintle housing
on MLG fitted to Jetstream 3100 aeroplanes.
Degradation of the surface protection by
abrasion can occur when the forward face of
the yoke pintle rotates against the pintle
bearing, which introduces corrosion pits and,
consequently, stress corrosion cracking.
This condition, if not detected and
corrected, could lead to structural failure of
the MLG, possibly resulting in loss of control
of the aeroplane during take-off or landing
runs.
To provide protection of the affected area
of the MLG assembly spigot housing, BAE
Systems (Operations) Ltd issued SB 32–
JM7862 to provide instructions for
installation of a protective washer, fitted at
the forward spigot on both, left hand (LH)
and right hand (RH), MLG. Consequently,
BAE Systems (Operations) Ltd issued SB 32–
A–JA851226 at Revision 5 to provide
additional accomplishment instructions for
Non-destructive testing inspection (NDT) of
MLG equipped with the protective washer
installed in accordance with BAE Systems
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(Operations) Ltd SB 32–JM7862 and to
introduce reference to MLG manufacturer
APPH Ltd SB 32–19 at Revision 4, providing
instructions for re-protection of the yoke
pintle.
For the reasons described above, this AD
retains the requirements of AD G–003–01–86,
which is superseded, and requires
implementation of revised inspection
requirements, and depending on findings,
corrective action. This AD introduces an
optional modification, which constitutes
terminating action for the inspections
required by this AD.
The MCAI can be found in the AD
docket on the Internet at: https://
www.regulations.gov/
#!documentDetail;D=FAA-2014-00200002.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM 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 2593,
January 15, 2014) for correcting the
unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Costs of Compliance
We estimate that this AD will affect
44 products of U.S. registry. We also
estimate that it would take about 14
work-hours per product to comply with
the inspection requirements of this AD.
The average labor rate is $85 per workhour.
Based on these figures, we estimate
the cost of this AD on U.S. operators to
be $52,360, or $1,190 per product.
In addition, we estimate that any
necessary follow-on actions would take
about 10 work-hours and require parts
costing $5,000, for a cost of $5,850 per
product for repairs. We have no way of
determining the number of products
that may 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.
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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 https://
www.regulations.gov by searching for
and locating Docket No. FAA–2014–
0020; 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:
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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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing Amendment 39–5497 (51 FR
47211, December 31, 1986) and adding
the following new AD:
■
2014–07–07 British Aerospace (Operations)
Limited: Amendment 39–17821; Docket
No. FAA–2014–0020; Directorate
Identifier 2013–CE–039–AD.
(a) Effective Date
This airworthiness directive (AD) becomes
effective June 3, 2014.
(b) Affected ADs
This AD supersedes AD 87–02–04,
Amendment 39–5497 (51 FR 47211,
December 31, 1986.
(c) Applicability
This AD applies to British Aerospace
(Operations) Limited Model HP.137 Jetstream
Mk.1, Jetstream Series 200, and Jetstream
Series 3101 airplanes, all serial numbers,
certificated in any category.
(d) Subject
Air Transport Association of America
(ATA) Code 32: Landing Gear.
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(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 cracking of
the forward main landing gear (MLG) yoke
pintle that resulted from corrosion pits
leading to stress corrosion. We are issuing
this AD to prevent failure of the MLG, which
could result in loss of control of the airplane
during take-off or landing.
(f) Actions and Compliance
Unless already done, do the following
actions specified in paragraphs (f)(1) through
(f)(11) of this AD:
(1) For airplanes that were affected by AD
87–02–04, Amendment 39–5497 (51 FR
47211, December 31, 1986): At the next 1,200
MLG flight cycle repetitive inspection that
would have been required by AD 87–02–04
or within the next 12 months after the last
1,200 MLG flight cycle repetitive inspection
that would have been required by AD 87–02–
04, whichever occurs first, and repetitively
thereafter at intervals not to exceed 1,200
MLG flight cycles or 12 months, whichever
occurs first, do a nondestructive testing
(NDT) inspection of each MLG assembly
cylinder attachment spigot housing following
the Accomplishment Instructions in APPH
Ltd. Service Bulletin No. 32–19, Revision 4,
dated April 3, 2013, and British Aerospace
Jetstream Series 3100 & 3200 Service Bulletin
32–A–JA851226, Revision 5, dated April 30,
2013.
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(2) For airplanes that were not affected by
AD 87–02–04, Amendment 39–5497 (51 FR
47211, December 31, 1986): Within the next
300 MLG flight cycles after June 3, 2014 (the
effective date of this AD) or within the next
3 months after June 3, 2014 (the effective date
of this AD) or at the next overhaul of the
MLG after June 3, 2014 (the effective date of
this AD), whichever occurs first, and
repetitively thereafter at intervals not to
exceed 1,200 MLG flight cycles or 12 months,
whichever occurs first, do a NDT inspection
of each MLG assembly cylinder attachment
spigot housing following the
Accomplishment Instructions in APPH Ltd.
Service Bulletin No. 32–19, Revision 4, dated
April 3, 2013, and British Aerospace
Jetstream Series 3100 & 3200 Service Bulletin
32–A–JA851226, Revision 5, dated April 30,
2013.
(3) For all airplanes: Within 300 landings
after a heavy or abnormal landing, conduct
a NDT inspection of each MLG assembly
cylinder attachment spigot following
Accomplishment Instructions in APPH Ltd.
Service Bulletin No. 32–19, Revision 4, dated
April 3, 2013, and British Aerospace
Jetstream Series 3100 & 3200 Service Bulletin
32–A–JA851226, Revision 5, dated April 30,
2013.
(4) For all airplanes: If any crack is found
during any inspection required in paragraphs
(f)(1), (f)(2), or (f)(3) of this AD, before further
flight, take all necessary corrective actions
following the Accomplishment Instructions
in APPH Ltd. Service Bulletin No. 32–19,
Revision 4, dated April 3, 2013, and British
Aerospace Jetstream Series 3100 & 3200
Service Bulletin 32–A–JA851226, Revision 5,
dated April 30, 2013.
(5) For all airplanes: Within 300 MLG
flight cycles or 3 months, whichever occurs
first after each NDT inspection required in
paragraph (f)(1) or (f)(2) of this AD, as
applicable, and repetitively thereafter at
intervals not to exceed 300 MLG flight cycles
or 3 months, whichever occurs first, do a
visual inspection of each MLG following the
Accomplishment Instructions in APPH Ltd.
Service Bulletin No. 32–19, Revision 4, dated
April 3, 2013, and British Aerospace
Jetstream Series 3100 & 3200 Service Bulletin
32–A–JA851226, Revision 5, dated April 30,
2013.
(6) For all airplanes: If any discrepancy is
found during any visual inspection required
in paragraph (f)(5) of this AD, before further
flight, take all necessary corrective actions
following the Accomplishment Instructions
in APPH Ltd. Service Bulletin No. 32–19,
Revision 4, dated April 3, 2013, and British
Aerospace Jetstream Series 3100 & 3200
Service Bulletin 32–A–JA851226, Revision 5,
dated April 30, 2013.
(7) For all airplanes with a MLG
incorporating a microswitch hole: Within the
next 10,600 MLG flight cycles since new and
repetitively thereafter at intervals not to
exceed 1,200 MLG flight cycles, do a NDT
inspection of each MLG microswitch hole
following the Accomplishment Instructions
in APPH Ltd. Service Bulletin No. 32–40,
Revision 1, dated February 2003, and Part C,
paragraph (2)(b) of British Aerospace
Jetstream Series 3100 & 3200 Service Bulletin
32–A–JA851226, Revision 5, dated April 30,
2013.
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23899
(8) For all airplanes: If any crack is found
during any NDT inspection required in
paragraph (f)(7) of this AD, before further
flight, take all necessary corrective actions
following the Accomplishment Instructions
in APPH Ltd. Service Bulletin No. 32–40,
Revision 1, dated February 2003, and British
Aerospace Jetstream Series 3100 & 3200
Service Bulletin 32–A–JA851226, Revision 5,
dated April 30, 2013.
(9) For all airplanes: Doing all necessary
corrective actions required in paragraphs
(f)(4), (f)(6), and (f)(8) of this AD does not
constitute terminating action for the
inspections required by this AD.
(10) For all airplanes: Modification of each
MLG cylinder following Jetstream Service
Bulletin 32–JA880340, original issue, dated
January 6, 1989, constitutes terminating
action for the inspections required by this AD
for that MLG.
(11) For all airplanes: The compliance
times in paragraphs (f)(2), (f)(3), (f)(5), and
(f)(7) of this AD are presented in flight cycles
(landings). If the total flight cycles have not
been kept, multiply the total number of
airplane hours time-in-service (TIS) by 0.75
to calculate the cycles. For the purposes of
this AD:
(i) 100 hours TIS × .75 = 75 cycles; and
(ii) 1,000 hours TIS × .75 = 750 cycles.
(g) Credit for Actions Done in Accordance
With Previous Service Information
This AD allows credit for the initial
inspection required in paragraph (f)(7) of this
AD if done before June 3, 2014 (the effective
date of this AD) following APPH Ltd. Service
Bulletin 32–40, at Initial Issue dated June 21,
1989.
(h) 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: Taylor Martin, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4138; fax: (816) 329–
4090; email: taylor.martin@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
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the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
(i) Related Information
Refer to MCAI European Aviation Safety
Agency (EASA) AD No.: 2013–0208, dated
September 10, 2013, for related information.
The MCAI can be found in the AD docket on
the Internet at: https://www.regulations.gov/
#!documentDetail;D=FAA-2014-0020-0002.
For availability information about APPH Ltd.
Service Bulletin 32–40, at Initial Issue dated
June 21, 1989, which is not incorporated by
reference, use the contact information in
paragraphs (j)(4) and (j)(5).
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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.
Federal Aviation Administration
(j) 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) APPH Ltd. Service Bulletin No. 32–19,
Revision 4, dated April 3, 2013.
(ii) APPH Ltd. Service Bulletin No. 32–40,
Revision 1, dated February 2003.
(iii) British Aerospace Jetstream Series
3100 & 3200 Service Bulletin 32–A–
JA851226, Revision 5, dated April 30, 2013.
(iv) Jetstream Service Bulletin 32–
JA880340, original issue, dated January 6,
1989.
(3) For British Aerospace (Operations)
Limited and Jetstream service information
identified in this AD, contact BAE Systems
(Operations) Ltd, Customer Information
Department, Prestwick International Airport,
Ayrshire, KA9 2RW, Scotland, United
Kingdom; phone: +44 1292 675207, fax: +44
1292 675704; email: RApublications@
baesystems.com; Internet: https://
www.jetstreamcentral.com.
(4) For APPH Ltd. service information
identified in this AD, contact APPH Ltd.
Engineering Division, Unit 1, Pembroke
Court, Chancellor Road, Manor Park,
Runcorn, Cheshire, WA7 1TG, England;
phone: +44 01928 532600; fax: +44 01928
579626; Internet: https://apph.com/contactus/customer-support/.
(5) You may view this service information
at 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.
(6) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
AGENCY:
VerDate Mar<15>2010
15:55 Apr 28, 2014
Jkt 232001
Issued in Kansas City, Missouri, on April
4, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2014–09540 Filed 4–28–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
[Docket No. FAA–2014–0233; Directorate
Identifier 2014–NM–053–AD; Amendment
39–17825; AD 2014–08–01]
RIN 2120–AA64
Airworthiness Directives; Airbus
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
We are superseding
Airworthiness Directive (AD) 2014–03–
08 for all Airbus Model A318, A319,
A320, and A321 series airplanes. AD
2014–03–08 required an inspection to
determine the part number of the
interconnecting struts installed on the
wings, identifying the part number and
the serial number of the associated
target and proximity sensor if
applicable, and replacing or reidentifying the flap interconnecting
strut if applicable. This new AD corrects
a typographical error that affects the
definition of a serviceable
interconnecting strut. This AD was
prompted by a report that an
investigation showed that when a
certain combination of a target/
proximity sensor serial number is
installed on a flap interconnecting strut,
a ‘‘target FAR’’ signal cannot be detected
when it reaches the mechanical end
stop of the interconnecting strut. We are
issuing this AD to detect and correct a
latent failure of the flap down drive
disconnection due to an already-failed
interconnecting strut sensor, which
could result in asymmetric flap panel
movement and consequent loss of
control of the airplane.
DATES: This AD becomes effective May
14, 2014.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
SUMMARY:
PO 00000
Frm 00014
Fmt 4700
Sfmt 4700
as of March 26, 2014 (79 FR 9398,
February 19, 2014).
We must receive comments on this
AD by June 13, 2014.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC, between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For service information identified in
this AD, contact Airbus, Airworthiness
Office—EAS, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France;
telephone +33 5 61 93 36 96; fax +33 5
61 93 44 51; email account.airwortheas@airbus.com; Internet https://
www.airbus.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.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2014–
0233; or in person at the Docket
Operations office 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. Comments will be available in
the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT:
Sanjay Ralhan, Aerospace Engineer,
International Branch, ANM 116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA
98057–3356; telephone (425) 227–1405;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Discussion
On January 22, 2014, we issued AD
2014–03–08, Amendment 39–17745 (79
FR 9398, February 19, 2014). AD 2014–
03–08 applied to all Airbus Model
A318, A319, A320, and A321 series
E:\FR\FM\29APR1.SGM
29APR1
]]>Agencies
[Federal Register Volume 79, Number 82 (Tuesday, April 29, 2014)]
[Rules and Regulations]
[Pages 23897-23900]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-09540]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0020; Directorate Identifier 2013-CE-039-AD;
Amendment 39-17821; AD 2014-07-07]
RIN 2120-AA64
Airworthiness Directives; British Aerospace (Operations) Limited
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are superseding an airworthiness directive (AD) 87-02-04
for British Aerospace (Operations) Limited Model HP.137 Jetstream MK.1,
Jetstream Series 200, and Jetstream Series 3101 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 cracking of the forward main landing gear yoke
pintle resulting from corrosion pits leading to stress corrosion. We
are issuing this AD to require actions to address the unsafe condition
on these products.
DATES: This AD is effective June 3, 2014.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of June 3, 2014.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0020; 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 20590.
For service information identified in this AD, contact BAE Systems
(Operations) Ltd, Customer Information Department, Prestwick
International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom;
phone: +44 1292 675207, fax: +44 1292 675704; email:
RApublications@baesystems.com; Internet: https://www.jetstreamcentral.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.
[[Page 23898]]
FOR FURTHER INFORMATION CONTACT Taylor Martin, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4138; fax: (816) 329-4090; email:
taylor.martin@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to add an AD that would apply to British Aerospace (Operations)
Limited Model HP 137 Jetstream MK1, Jetstream Series 200, and Jetstream
Series 3101 airplanes. The NPRM was published in the Federal Register
on January 15, 2014 (79 FR 2593), and proposed to supersede AD 87-02-
04, Amendment 39-5497 (51 FR 47211, December 31, 1986).
The NPRM (79 FR 2593, January 15, 2014) 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 that:
Prompted by occurrences of the main landing gear (MLG) yoke
pintle housing cracking, the United Kingdom Civil Aviation Authority
(UK CAA) issued AD G-003-01-86 to require repetitive inspections to
identify any crack in the yoke pintle housing on MLG fitted to
Jetstream 3100 aeroplanes in accordance with BAE Systems
(Operations) Ltd Service Bulletin (SB) 32-A-JA851226, and depending
on findings, corrective action. After that AD was issued, an
occurrence of Jetstream 3100 MLG failure was reported after landing.
The subsequent investigation revealed stress corrosion cracking of
the MLG yoke pintle housing as a root cause of the MLG failure.
Furthermore, the investigation report recommended a review of the
effectiveness of UK CAA AD G-003-01-86 in identifying cracks in the
yoke pintle housing on MLG fitted to Jetstream 3100 aeroplanes.
Degradation of the surface protection by abrasion can occur when
the forward face of the yoke pintle rotates against the pintle
bearing, which introduces corrosion pits and, consequently, stress
corrosion cracking.
This condition, if not detected and corrected, could lead to
structural failure of the MLG, possibly resulting in loss of control
of the aeroplane during take-off or landing runs.
To provide protection of the affected area of the MLG assembly
spigot housing, BAE Systems (Operations) Ltd issued SB 32-JM7862 to
provide instructions for installation of a protective washer, fitted
at the forward spigot on both, left hand (LH) and right hand (RH),
MLG. Consequently, BAE Systems (Operations) Ltd issued SB 32-A-
JA851226 at Revision 5 to provide additional accomplishment
instructions for Non-destructive testing inspection (NDT) of MLG
equipped with the protective washer installed in accordance with BAE
Systems (Operations) Ltd SB 32-JM7862 and to introduce reference to
MLG manufacturer APPH Ltd SB 32-19 at Revision 4, providing
instructions for re-protection of the yoke pintle.
For the reasons described above, this AD retains the
requirements of AD G-003-01-86, which is superseded, and requires
implementation of revised inspection requirements, and depending on
findings, corrective action. This AD introduces an optional
modification, which constitutes terminating action for the
inspections required by this AD.
The MCAI can be found in the AD docket on the Internet at: https://www.regulations.gov/#!documentDetail;D=FAA-2014-0020-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM 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 2593, January 15, 2014) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Costs of Compliance
We estimate that this AD will affect 44 products of U.S. registry.
We also estimate that it would take about 14 work-hours per product to
comply with the inspection requirements of this AD. The average labor
rate is $85 per work-hour.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $52,360, or $1,190 per product.
In addition, we estimate that any necessary follow-on actions would
take about 10 work-hours and require parts costing $5,000, for a cost
of $5,850 per product for repairs. We have no way of determining the
number of products that may 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 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 https://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0020; 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:
[[Page 23899]]
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 removing Amendment 39-5497 (51 FR
47211, December 31, 1986) and adding the following new AD:
2014-07-07 British Aerospace (Operations) Limited: Amendment 39-
17821; Docket No. FAA-2014-0020; Directorate Identifier 2013-CE-039-
AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective June 3,
2014.
(b) Affected ADs
This AD supersedes AD 87-02-04, Amendment 39-5497 (51 FR 47211,
December 31, 1986.
(c) Applicability
This AD applies to British Aerospace (Operations) Limited Model
HP.137 Jetstream Mk.1, Jetstream Series 200, and Jetstream Series
3101 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 cracking of the
forward main landing gear (MLG) yoke pintle that resulted from
corrosion pits leading to stress corrosion. We are issuing this AD
to prevent failure of the MLG, which could result in loss of control
of the airplane during take-off or landing.
(f) Actions and Compliance
Unless already done, do the following actions specified in
paragraphs (f)(1) through (f)(11) of this AD:
(1) For airplanes that were affected by AD 87-02-04, Amendment
39-5497 (51 FR 47211, December 31, 1986): At the next 1,200 MLG
flight cycle repetitive inspection that would have been required by
AD 87-02-04 or within the next 12 months after the last 1,200 MLG
flight cycle repetitive inspection that would have been required by
AD 87-02-04, whichever occurs first, and repetitively thereafter at
intervals not to exceed 1,200 MLG flight cycles or 12 months,
whichever occurs first, do a nondestructive testing (NDT) inspection
of each MLG assembly cylinder attachment spigot housing following
the Accomplishment Instructions in APPH Ltd. Service Bulletin No.
32-19, Revision 4, dated April 3, 2013, and British Aerospace
Jetstream Series 3100 & 3200 Service Bulletin 32-A-JA851226,
Revision 5, dated April 30, 2013.
(2) For airplanes that were not affected by AD 87-02-04,
Amendment 39-5497 (51 FR 47211, December 31, 1986): Within the next
300 MLG flight cycles after June 3, 2014 (the effective date of this
AD) or within the next 3 months after June 3, 2014 (the effective
date of this AD) or at the next overhaul of the MLG after June 3,
2014 (the effective date of this AD), whichever occurs first, and
repetitively thereafter at intervals not to exceed 1,200 MLG flight
cycles or 12 months, whichever occurs first, do a NDT inspection of
each MLG assembly cylinder attachment spigot housing following the
Accomplishment Instructions in APPH Ltd. Service Bulletin No. 32-19,
Revision 4, dated April 3, 2013, and British Aerospace Jetstream
Series 3100 & 3200 Service Bulletin 32-A-JA851226, Revision 5, dated
April 30, 2013.
(3) For all airplanes: Within 300 landings after a heavy or
abnormal landing, conduct a NDT inspection of each MLG assembly
cylinder attachment spigot following Accomplishment Instructions in
APPH Ltd. Service Bulletin No. 32-19, Revision 4, dated April 3,
2013, and British Aerospace Jetstream Series 3100 & 3200 Service
Bulletin 32-A-JA851226, Revision 5, dated April 30, 2013.
(4) For all airplanes: If any crack is found during any
inspection required in paragraphs (f)(1), (f)(2), or (f)(3) of this
AD, before further flight, take all necessary corrective actions
following the Accomplishment Instructions in APPH Ltd. Service
Bulletin No. 32-19, Revision 4, dated April 3, 2013, and British
Aerospace Jetstream Series 3100 & 3200 Service Bulletin 32-A-
JA851226, Revision 5, dated April 30, 2013.
(5) For all airplanes: Within 300 MLG flight cycles or 3 months,
whichever occurs first after each NDT inspection required in
paragraph (f)(1) or (f)(2) of this AD, as applicable, and
repetitively thereafter at intervals not to exceed 300 MLG flight
cycles or 3 months, whichever occurs first, do a visual inspection
of each MLG following the Accomplishment Instructions in APPH Ltd.
Service Bulletin No. 32-19, Revision 4, dated April 3, 2013, and
British Aerospace Jetstream Series 3100 & 3200 Service Bulletin 32-
A-JA851226, Revision 5, dated April 30, 2013.
(6) For all airplanes: If any discrepancy is found during any
visual inspection required in paragraph (f)(5) of this AD, before
further flight, take all necessary corrective actions following the
Accomplishment Instructions in APPH Ltd. Service Bulletin No. 32-19,
Revision 4, dated April 3, 2013, and British Aerospace Jetstream
Series 3100 & 3200 Service Bulletin 32-A-JA851226, Revision 5, dated
April 30, 2013.
(7) For all airplanes with a MLG incorporating a microswitch
hole: Within the next 10,600 MLG flight cycles since new and
repetitively thereafter at intervals not to exceed 1,200 MLG flight
cycles, do a NDT inspection of each MLG microswitch hole following
the Accomplishment Instructions in APPH Ltd. Service Bulletin No.
32-40, Revision 1, dated February 2003, and Part C, paragraph (2)(b)
of British Aerospace Jetstream Series 3100 & 3200 Service Bulletin
32-A-JA851226, Revision 5, dated April 30, 2013.
(8) For all airplanes: If any crack is found during any NDT
inspection required in paragraph (f)(7) of this AD, before further
flight, take all necessary corrective actions following the
Accomplishment Instructions in APPH Ltd. Service Bulletin No. 32-40,
Revision 1, dated February 2003, and British Aerospace Jetstream
Series 3100 & 3200 Service Bulletin 32-A-JA851226, Revision 5, dated
April 30, 2013.
(9) For all airplanes: Doing all necessary corrective actions
required in paragraphs (f)(4), (f)(6), and (f)(8) of this AD does
not constitute terminating action for the inspections required by
this AD.
(10) For all airplanes: Modification of each MLG cylinder
following Jetstream Service Bulletin 32-JA880340, original issue,
dated January 6, 1989, constitutes terminating action for the
inspections required by this AD for that MLG.
(11) For all airplanes: The compliance times in paragraphs
(f)(2), (f)(3), (f)(5), and (f)(7) of this AD are presented in
flight cycles (landings). If the total flight cycles have not been
kept, multiply the total number of airplane hours time-in-service
(TIS) by 0.75 to calculate the cycles. For the purposes of this AD:
(i) 100 hours TIS x .75 = 75 cycles; and
(ii) 1,000 hours TIS x .75 = 750 cycles.
(g) Credit for Actions Done in Accordance With Previous Service
Information
This AD allows credit for the initial inspection required in
paragraph (f)(7) of this AD if done before June 3, 2014 (the
effective date of this AD) following APPH Ltd. Service Bulletin 32-
40, at Initial Issue dated June 21, 1989.
(h) 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: Taylor Martin, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4138; fax: (816) 329-4090; email:
taylor.martin@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
[[Page 23900]]
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.
(i) Related Information
Refer to MCAI European Aviation Safety Agency (EASA) AD No.:
2013-0208, dated September 10, 2013, for related information. The
MCAI can be found in the AD docket on the Internet at: https://www.regulations.gov/#!documentDetail;D=FAA-2014-0020-0002. For
availability information about APPH Ltd. Service Bulletin 32-40, at
Initial Issue dated June 21, 1989, which is not incorporated by
reference, use the contact information in paragraphs (j)(4) and
(j)(5).
(j) 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) APPH Ltd. Service Bulletin No. 32-19, Revision 4, dated
April 3, 2013.
(ii) APPH Ltd. Service Bulletin No. 32-40, Revision 1, dated
February 2003.
(iii) British Aerospace Jetstream Series 3100 & 3200 Service
Bulletin 32-A-JA851226, Revision 5, dated April 30, 2013.
(iv) Jetstream Service Bulletin 32-JA880340, original issue,
dated January 6, 1989.
(3) For British Aerospace (Operations) Limited and Jetstream
service information identified in this AD, contact BAE Systems
(Operations) Ltd, Customer Information Department, Prestwick
International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom;
phone: +44 1292 675207, fax: +44 1292 675704; email:
RApublications@baesystems.com; Internet: https://www.jetstreamcentral.com.
(4) For APPH Ltd. service information identified in this AD,
contact APPH Ltd. Engineering Division, Unit 1, Pembroke Court,
Chancellor Road, Manor Park, Runcorn, Cheshire, WA7 1TG, England;
phone: +44 01928 532600; fax: +44 01928 579626; Internet: https://apph.com/contact-us/customer-support/.
(5) You may view this service information at 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.
(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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on April 4, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2014-09540 Filed 4-28-14; 8:45 am]
BILLING CODE 4910-13-P
