Airworthiness Directives; 328 Support Services GmbH (Type Certificate Previously Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Airplanes, 12370-12373 [2014-02995]
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Federal Register / Vol. 79, No. 43 / Wednesday, March 5, 2014 / Rules and Regulations
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 adding
the following new airworthiness
directive (AD):
■
2014–03–06 The Boeing Company:
Amendment 39–17743; Docket No.
FAA–2013–0866; Directorate Identifier
2013–NM–131–AD.
(a) Effective Date
This AD is effective April 9, 2014.
(b) Affected ADs
None.
(c) Applicability
(1) This AD applies to all The Boeing
Company Model 737–100, –200, –200C,
–300, –400, and –500 series airplanes,
certificated in any category.
(2) Installation of Supplemental Type
Certificate (STC) ST01219SE (https://
rgl.faa.gov/Regulatory_and_Guidance_
Library/rgstc.nsf/0/
2C6E3DBDDD36F91C862576A4005D64E2?
OpenDocument&Highlight=st01219se) does
not affect the ability to accomplish the
actions required by this AD. Therefore, for
airplanes on which STC ST01219SE is
installed, a ‘‘change in product’’ alternative
method of compliance (AMOC) approval
request is not necessary to comply with the
requirements of 14 CFR 39.17.
(d) Subject
Air Transport Association (ATA) of
America Code 57, Wings.
(e) Unsafe Condition
This AD was prompted by reports of cracks
found in the aft support fitting for the main
landing gear (MLG) beam, and the rear spar
upper chord and rear spar web. We are
issuing this AD to detect and correct such
cracks, which could grow and result in a fuel
leak and possible fire.
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(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Inspections: Group 1
For airplanes identified in Group 1 of
Boeing Special Attention Service Bulletin
737–57–1318, dated May 15, 2013: At the
applicable time specified in paragraph 1.E.,
‘‘Compliance,’’ of Boeing Special Attention
Service Bulletin 737–57–1318, dated May 15,
2013, except as required by paragraph (i) of
this AD, do inspections and applicable
corrective actions using a method approved
in accordance with the procedures specified
in paragraph (j) of this AD.
(h) Inspections: Groups 2–7
For airplanes identified in Groups 2
through 7 of Boeing Special Attention
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Service Bulletin 737–57–1318, dated May 15,
2013: At the applicable time specified in
paragraph 1.E., ‘‘Compliance,’’ of Boeing
Special Attention Service Bulletin 737–57–
1318, dated May 15, 2013, except as required
by paragraph (i) of this AD, do high
frequency eddy current inspections to detect
cracking of the aft support fitting for the MLG
beam, and the rear spar upper chord and rear
spar web in the area of rear spar station
224.14, as applicable, in accordance with
Option 1, 2, or 3 of the Accomplishment
Instructions of Boeing Special Attention
Service Bulletin 737–57–1318, dated May 15,
2013.
(1) If no crack is found, repeat the
inspection thereafter at the time specified in
paragraph 1.E., ‘‘Compliance,’’ of Boeing
Special Attention Service Bulletin 737–57–
1318, dated May 15, 2013, as applicable.
Accomplishment of the inspection of the 12
fastener holes (locations 1–12) in accordance
with Option 2, Action 3; or Option 3, Action
3; as specified in note (b) of tables 2 through
5 of paragraph 1.E., ‘‘Compliance,’’ of Boeing
Special Attention Service Bulletin 737–57–
1318, dated May 15, 2013; terminates only
the corresponding inspections that include
note (b) in the ‘‘Repeat Interval’’ column of
the applicable table.
(2) If any crack is found during any
inspection required by paragraph (g) or (g)(1)
of this AD, repair before further flight using
a method approved in accordance with the
procedures specified in paragraph (j) of this
AD.
(i) Exception to Service Information
Specifications
Where Boeing Special Attention Service
Bulletin 737–57–1318, dated May 15, 2013,
specifies a compliance time ‘‘after the
original issue date of this service bulletin,’’
this AD requires compliance within the
specified compliance time after the effective
date of this AD.
(j) 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 (k) 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), which 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.
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(k) Related Information
For more information about this AD,
contact Nancy Marsh, Aerospace Engineer,
Airframe Branch, ANM–120S, FAA, Seattle
Aircraft Certification Office (ACO), 1601 Lind
Avenue SW., Renton, WA 98057–3356;
phone: 425–917–6440; fax: 425–917–6590;
email: nancy.marsh@faa.gov.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) Boeing Special Attention Service
Bulletin 737–57–1318, dated May 15, 2013.
(ii) Reserved.
(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 January
18, 2014.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2014–02521 Filed 3–4–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2013–0702; Directorate
Identifier 2012–NM–181–AD; Amendment
39–17753; AD 2014–03–15]
RIN 2120–AA64
Airworthiness Directives; 328 Support
Services GmbH (Type Certificate
Previously Held by AvCraft Aerospace
GmbH; Fairchild Dornier GmbH;
Dornier Luftfahrt GmbH) Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are superseding
airworthiness directive (AD) 2008–14–
SUMMARY:
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Federal Register / Vol. 79, No. 43 / Wednesday, March 5, 2014 / Rules and Regulations
16 for certain 328 Support Services
GmbH (Type Certificate Previously Held
by AvCraft Aerospace GmbH; Fairchild
Dornier GmbH; Dornier Luftfahrt GmbH)
Model 328–100 and 328–300 airplanes.
AD 2008–14–16 required installing
warning placards on the inside of the
passenger door and service doors and
modifying the hinge supports and
support struts of the passenger doors.
This new AD continues to require the
actions required by AD 2008–14–16 and
also requires replacing the fasteners
which were installed as part of the
modification with new fasteners of the
correct length, adds new airplanes, and
removes one airplane. This AD was
prompted by reports that certain
fasteners, which were installed as part
of the modification, are the wrong
length. We are issuing this AD to
prevent incidents of inadvertent
opening and possible detachment of a
passenger door in-flight, resulting in
damage to airframe and systems and
loss of control of the airplane.
DATES: This AD becomes effective April
9, 2014.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of April 9, 2014.
The Director of the Federal Register
approved the incorporation by reference
of certain other publications listed in
this AD as of August 21, 2008 (73 FR
40955, July 17, 2008).
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov/#!docketDetail;
D=FAA–2013–0702; or in person at the
Docket Management Facility, U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE., Washington,
DC.
For service information identified in
this AD, contact 328 Support Services
GmbH, Global Support Center, P.O. Box
1252, D–82231 Wessling, Federal
Republic of Germany; telephone +49
8153 88111 6666; fax +49 8153 88111
6565; email gsc.op@328support.de;
Internet https://www.328support.de. 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.
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue SW, Renton, WA
98057–3356; telephone (425) 227–1175;
fax (425) 227–1149.
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SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2008–14–16,
Amendment 39–15611 (73 FR 40955,
July 17, 2008). AD 2008–14–16 applied
to certain 328 Support Services GmbH
(Type Certificate Previously Held by
AvCraft Aerospace GmbH; Fairchild
Dornier GmbH; Dornier Luftfahrt GmbH)
Model 328–100 and 328–300 airplanes.
The NPRM published in the Federal
Register on August 27, 2013 (78 FR
52872). The NPRM was prompted by
reports that certain fasteners, which
were installed as part of the
modification, are the wrong length. The
NPRM proposed to continue to require
installing warning placards on the
inside of the passenger door and service
doors and modifying the hinge supports
and support struts of the passenger
doors. The NPRM also proposed to
require replacing the fasteners which
were installed as part of the
modification with new fasteners of the
correct length, adds new airplanes, and
removes one airplane. We are issuing
this AD to prevent incidents of
inadvertent opening and possible
detachment of a passenger door inflight, resulting in damage to airframe
and systems and loss of control of the
airplane.
The European Aviation Safety Agency
(EASA), which is the aviation authority
for Member States of the European
Community, has issued EASA
Airworthiness Directive 2012–0183R1,
dated September 28, 2012 (referred to
after this as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for the specified products. The MCAI
states:
At least one incident occurred where,
immediately after take-off, the passenger door
of a Dornier 328 aeroplane completely
opened. The flight crew reportedly had no
cockpit indication or audible chime prior to
this event. The aeroplane returned to the
departure airfield and made an uneventful
emergency landing. Substantial damage to
the door, handrails, door hinge arms and
fuselage skin were found.
The subsequent investigation could not
find any deficiency in the design of the main
cabin door locking mechanism. In addition,
no technical failure could be determined that
precipitated the event. The flight data
recorder showed that the door was closed
and locked before take-off and opened
shortly afterwards. Although final proof
could not be obtained, the most likely way
in which the door opened was that the door
handle was inadvertently operated during the
take-off run.
In response to the incident, AvCraft (the
TC holder at the time) developed a placard
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12371
set to warn the occupants against touching
the door handle, as well as a structural
modification of the passenger door hinge
supports described in [Dornier 328 Support
Services] Service Bulletin (SB) SB–328–52–
460 and SB–328J–52–213 to make certain
that the door does not separate from the
aeroplane when inadvertently opened during
flight, allowing a safe descent and landing.
EASA issued AD 2007–0199 (https://
ad.easa.europa.eu/ad/2007-0199) to require
the installation of warning placards and
modification as detailed in these SB
instructions.
Since that [EASA] AD [2007–0199] was
issued, 328 Support Services GmbH (the
current type certificate holder) have
determined that certain fasteners, identified
by Part Number (P/N) NAS6703U1 and P/N
NAS6703U2, which were installed as part of
the modification, have the wrong length and
must be replaced.
For the reasons described above, this
[EASA] AD retains the requirements of EASA
AD 2007–0199, which is superseded, and
requires replacement of the affected fasteners
by the ones that have the correct length.
This [EASA] AD has been revised to
correct and clarify the actions required by
paragraph (3).
This AD also adds new airplanes and
removes one airplane from the
applicability of this AD. You may
examine the MCAI in the AD docket on
the Internet at https://
www.regulations.gov/
#!docketDetail;D=FAA-2013-0702.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM (78
FR 52872, August 27, 2013), or on the
determination of the cost to the public.
Conclusion
We reviewed the available data and
determined that air safety and the
public interest require adopting this 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 (78 FR
52872, August 27, 2013) for correcting
the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM (78 FR 52872,
August 27, 2013).
Costs of Compliance
We estimate that this AD affects 35
airplanes of U.S. registry.
The actions that are required by AD
2008–14–16, Amendment 39–15611 (73
FR 40955, July 17, 2008), and retained
in this AD take about 38 work-hours per
product, at an average labor rate of $85
per work-hour. Required parts cost
about $11,961 per product. Based on
these figures, the estimated cost of the
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actions that were required by AD 2008–
14–16 is $15,191 per product.
We also estimate that it will take
about 25 work-hours per product to
comply with the new basic
requirements of this AD. The average
labor rate is $85 per work-hour.
Required parts will cost about $0 per
product. Based on these figures, we
estimate the cost of this AD on U.S.
operators to be $74,375, or $2,125 per
product.
Facility between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal
holidays. The AD docket contains this
AD, the regulatory evaluation, any
comments received, and other
information. The street address for the
Docket Operations
Authority for This Rulemaking
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
(f) Compliance
You are responsible for having the actions
required by this AD performed within the
compliance times specified, unless the
actions have already been done.
Examining the AD Docket
(d) Subject
Air Transport Association (ATA) of
America Code 11, Placards and Markings;
and Code 52, Doors.
(g) Retained Installation and Modification
for Airplanes Identified in AD 2008–14–16,
Amendment 39–15611 (73 FR 40955, July 17,
2008) With Revised Service Information
This paragraph restates the requirements of
paragraph (f) of AD 2008–14–16, Amendment
39–15611 (73 FR 40955, July 17, 2008), with
revised service information.
(1) For Model 328–100 airplanes, serial
numbers 3005 through 3098 inclusive, 3100,
3106, 3109, 3110, 3112, 3113, 3115, 3117,
and 3119; and Model 328–300 airplanes,
having serial numbers 3102, 3105, 3108,
3111, 3114, 3116, 3118, and 3120 through
3224 inclusive: Within 30 days after August
21, 2008, (the effective date of AD 2008–14–
16, Amendment 39–15611 (73 FR 40955, July
17, 2008)), install warning placards on the
inside of the passenger door and service
doors, in accordance with the
Accomplishment Instructions of the service
information specified in paragraph (g)(1)(i) or
(g)(1)(ii) of this AD, as applicable.
(i) Dornier Service Bulletin SB–328–11–
454, dated May 3, 2004 (for Model 328–100
airplanes).
(ii) Dornier Service Bulletin SB–328J–11–
209, dated May 3, 2004 (for Model 328–300
airplanes).
(2) For Model 328–100 airplanes, serial
numbers 3005 through 3098 inclusive, 3100,
3106, 3109, 3110, 3112, 3113, 3115, 3117,
and 3119; and Model 328–300 airplanes,
having serial numbers 3102, 3105, 3108,
3111, 3114, 3116, 3118, and 3120 through
3224 inclusive: Within 12 months after
August 21, 2008, the effective date of AD
2008–14–16, Amendment 39–15611 (73 FR
0955, July 17, 2008), modify the hinge
supports and support struts of the passenger
doors, in accordance with the
Accomplishment Instructions of the service
information specified in paragraphs (g)(2)(i)
through (g)(2)(iv) of this AD, as applicable.
As of the effective date of this AD only the
service information specified in paragraph
(g)(2)(ii) or (g)(2)(iv) of this AD, as applicable,
may be used.
(i) Dornier Service Bulletin SB–328–52–
460, dated February 4, 2005 (for Model 328–
100 airplanes).
(ii) 328 Support Services Service Bulletin
SB–328–52–460, Revision 2, dated March 1,
2012 (for Model 328–100 airplanes).
(iii) Dornier Service Bulletin SB–328J–52–
213, dated February 4, 2005, (for Model 328–
300 airplanes).
(iv) 328 Support Services Service Bulletin
SB–328J–52–213, Revision 1, dated August
17, 2011 (for Model 328–300 airplanes).
You may examine the AD docket on
the Internet at https://
www.regulations.gov/
#!docketDetail;D=FAA-2013-0702; or in
person at the Docket Management
(e) Reason
This AD was prompted by reports that
certain fasteners, which were installed as
part of a modification, are the wrong length.
We are issuing this AD to prevent incidents
(h) New Installation and Modification for
Newly Added Airplanes
For airplanes not identified in paragraph
(g) of this AD, do the actions required by
paragraphs (h)(1) and (h)(2) of this AD.
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.
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List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
of inadvertent opening and possible
detachment of a passenger door in-flight,
resulting in damage to airframe and systems
and loss of control of the airplane.
Regulatory Findings
We determined that this AD will not
have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in
Alaska; and
4. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
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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 Airworthiness Directive (AD)
2008–14–16, Amendment 39–15611 (73
FR 40955, July 17, 2008), and adding the
following new AD:
■
2014–03–15 328 Support Services GmbH
(Type Certificate Previously Held by
AvCraft Aerospace GmbH; Fairchild
Dornier GmbH; Dornier Luftfahrt
GmbH): Amendment 39–17753. Docket
No. FAA–2013–0702; Directorate
Identifier 2012–NM–181–AD.
(a) Effective Date
This airworthiness directive (AD) becomes
effective April 9, 2014.
(b) Affected ADs
This AD supersedes AD 2008–14–16,
Amendment 39–15611 (73 FR 40955, July 17,
2008).
(c) Applicability
This AD applies to 328 Support Services
GmbH (Type Certificate previously held by
AvCraft Aerospace GmbH; Fairchild Dornier
GmbH; Dornier Luftfahrt GmbH) airplanes,
certificated in any category, identified in
paragraphs (c)(1) and (c)(2) of this AD.
(1) Model 328–100 airplanes, serial
numbers 3005 through 3101 inclusive, 3103,
3104, 3106, 3109, 3110, 3112, 3113, 3115,
3117, and 3119.
(2) Model 328–300 airplanes, all serial
numbers.
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(1) Within 30 days after the effective date
of this AD, install warning placards on the
inside of the passenger door and service
doors, in accordance with the
Accomplishment Instructions of Dornier
Service Bulletin SB–328–11–454, dated May
3, 2004 (for Model 328–100 airplanes); or
Dornier Service Bulletin SB–328J–11–209,
dated May 3, 2004 (for Model 328–300
airplanes); as applicable.
(2) Within 12 months after the effective
date of this AD, modify the hinge supports
and support struts of the passenger doors, in
accordance with the Accomplishment
Instructions of 328 Support Services Service
Bulletin SB–328–52–460, Revision 2, dated
March 1, 2012 (for Model 328–100 airplanes);
or 328 Support Services Service Bulletin SB–
328J–52–213, Revision 1, dated August 17,
2011 (for Model 328–300 airplanes); as
applicable.
(i) New Replacement of Fasteners for All
Airplanes
For airplanes on which 26 part number
NAS6703U1 fasteners were installed as
specified in the service information in
paragraphs (g)(2)(i) and (g)(2)(iii) of this AD:
Within 6 months after the effective date of
this AD, replace the 20 affected part number
NAS6703U1 fasteners with new fasteners
having part number NAS6703U2, in
accordance with the Accomplishment
Instructions of 328 Support Services Service
Bulletin SB–328–52–460, Revision 2, dated
March 1, 2012 (for Model 328–100 airplanes);
or 328 Support Services Service Bulletin SB–
328J–52–213, Revision 1, dated August 17,
2011 (for Model 328–300 airplanes); as
applicable.
Note 1 to paragraph (i) of this AD: 328
Support Services Service Bulletin SB–328–
52–460, Revision 2, dated March 1, 2012, and
328 Support Services Service Bulletin SB–
328J–52–213, Revision 1, dated August 17,
2011, identify 20 of 26 part number
NAS6703U1 fasteners requiring to be
replaced due to incorrect length.
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(j) Credit for Previous Actions
This paragraph provides credit for certain
actions required by paragraph (g) and (h)(2)
of this AD, if those actions were performed
before the effective date of this AD using 328
Support Services Service Bulletin SB–328–
52–460, Revision 1, dated August 17, 2011,
which is not incorporated by reference.
(k) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Branch, ANM–116, Transport Airplane
Directorate, 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 International Branch, send it to ATTN:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116, Transport
Airplane Directorate, FAA, 1601 Lind
Avenue SW., Renton, WA 98057–3356;
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telephone (425) 227–1175; fax (425) 227–
1149. Information may be emailed to: 9ANM-116-AMOC-REQUESTS@faa.gov.
Before using any approved AMOC, notify
your appropriate principal inspector, or
lacking a principal inspector, the manager of
the local flight standards district office/
certificate holding district office. The AMOC
approval letter must specifically reference
this AD.
(2) 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.
(l) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) European
Aviation Safety Agency Airworthiness
Directive 2012–0183R1, dated September 28,
2012, for related information. You may
examine the MCAI in the AD docket on the
Internet at https://www.regulations.gov/
#!docketDetail;D=FAA-2013-0702.
(2) Service information identified in this
AD that is not incorporated by reference in
this AD may be obtained at the addresses
specified in paragraphs (m)(3) and (m)(4) of
this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(3) The following service information was
approved for IBR on April 9, 2014.
(i) 328 Support Services Service Bulletin
SB–328–52–460, Revision 2, dated March 1,
2012.
(ii) 328 Support Services Service Bulletin
SB–328J–52–213, Revision 1, dated August
17, 2011.
(4) The following service information was
approved for IBR on August 21, 2008 (73 FR
40955, July 17, 2008).
(i) Dornier Service Bulletin SB–328–11–
454, dated May 3, 2004.
(ii) Dornier Service Bulletin SB–328J–11–
209, dated May 3, 2004.
(iii) Dornier Service Bulletin SB–328–52–
460, dated February 4, 2005.
(iv) Dornier Service Bulletin SB–328J–52–
213, dated February 4, 2005.
(5) For service information identified in
this AD, contact 328 Support Services GmbH,
Global Support Center, P.O. Box 1252, D–
82231 Wessling, Federal Republic of
Germany; telephone +49 8153 88111 6666;
fax +49 8153 88111 6565; email gsc.op@
328support.de; Internet https://
www.328support.de.
(6) You may view this service information
at the FAA, Transport Airplane Directorate,
1601 Lind Avenue SW., Renton, WA. For
information on the availability of this
material at the FAA, call 425–227–1221.
PO 00000
Frm 00021
Fmt 4700
Sfmt 4700
12373
(7) 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 January
31, 2014.
John P. Piccola,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2014–02995 Filed 3–4–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2013–0351; Directorate
Identifier 2009–SW–049–AD; Amendment
39–17770; AD 2014–04–11]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters (Type Certificate
Previously Held by Eurocopter France)
(Airbus Helicopters)
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for Airbus
Helicopters Model AS350B, BA, B1, B2,
B3, and D, and Model AS355E, F, F1,
F2, and N helicopters with certain tail
rotor (T/R) blades. This AD requires
installing additional rivets to secure
each T/R blade trailing edge tab (tab),
and inspecting for evidence of
debonding of the tab after the rivets are
installed. This AD was prompted by
reports of T/R blade tab debonding. The
actions of this AD are intended to
prevent loss of a T/R blade tab, which
could result in excessive vibration and
loss of control of the helicopter.
DATES: This AD is effective April 9,
2014.
The Director of the Federal Register
approved the incorporation by reference
of certain documents listed in this AD
as of April 9, 2014.
ADDRESSES: For service information
identified in this AD, contact Airbus
Helicopters, Inc., 2701 N. Forum Drive,
Grand Prairie, TX 75052; telephone
(972) 641–0000 or (800) 232–0323; fax
(972) 641–3775; or at https://
www.airbushelicopters.com/techpub.
You may review the referenced service
information at the FAA, Office of the
Regional Counsel, Southwest Region,
SUMMARY:
E:\FR\FM\05MRR1.SGM
05MRR1
]]>Agencies
[Federal Register Volume 79, Number 43 (Wednesday, March 5, 2014)]
[Rules and Regulations]
[Pages 12370-12373]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-02995]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0702; Directorate Identifier 2012-NM-181-AD;
Amendment 39-17753; AD 2014-03-15]
RIN 2120-AA64
Airworthiness Directives; 328 Support Services GmbH (Type
Certificate Previously Held by AvCraft Aerospace GmbH; Fairchild
Dornier GmbH; Dornier Luftfahrt GmbH) Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are superseding airworthiness directive (AD) 2008-14-
[[Page 12371]]
16 for certain 328 Support Services GmbH (Type Certificate Previously
Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier
Luftfahrt GmbH) Model 328-100 and 328-300 airplanes. AD 2008-14-16
required installing warning placards on the inside of the passenger
door and service doors and modifying the hinge supports and support
struts of the passenger doors. This new AD continues to require the
actions required by AD 2008-14-16 and also requires replacing the
fasteners which were installed as part of the modification with new
fasteners of the correct length, adds new airplanes, and removes one
airplane. This AD was prompted by reports that certain fasteners, which
were installed as part of the modification, are the wrong length. We
are issuing this AD to prevent incidents of inadvertent opening and
possible detachment of a passenger door in-flight, resulting in damage
to airframe and systems and loss of control of the airplane.
DATES: This AD becomes effective April 9, 2014.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of April 9,
2014.
The Director of the Federal Register approved the incorporation by
reference of certain other publications listed in this AD as of August
21, 2008 (73 FR 40955, July 17, 2008).
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2013-0702; or in person at the
Docket Management Facility, U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC.
For service information identified in this AD, contact 328 Support
Services GmbH, Global Support Center, P.O. Box 1252, D-82231 Wessling,
Federal Republic of Germany; telephone +49 8153 88111 6666; fax +49
8153 88111 6565; email gsc.op@328support.de; Internet https://www.328support.de. 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.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW, Renton, WA 98057-3356; telephone (425) 227-1175;
fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2008-14-16, Amendment 39-15611 (73 FR 40955,
July 17, 2008). AD 2008-14-16 applied to certain 328 Support Services
GmbH (Type Certificate Previously Held by AvCraft Aerospace GmbH;
Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Model 328-100 and 328-
300 airplanes. The NPRM published in the Federal Register on August 27,
2013 (78 FR 52872). The NPRM was prompted by reports that certain
fasteners, which were installed as part of the modification, are the
wrong length. The NPRM proposed to continue to require installing
warning placards on the inside of the passenger door and service doors
and modifying the hinge supports and support struts of the passenger
doors. The NPRM also proposed to require replacing the fasteners which
were installed as part of the modification with new fasteners of the
correct length, adds new airplanes, and removes one airplane. We are
issuing this AD to prevent incidents of inadvertent opening and
possible detachment of a passenger door in-flight, resulting in damage
to airframe and systems and loss of control of the airplane.
The European Aviation Safety Agency (EASA), which is the aviation
authority for Member States of the European Community, has issued EASA
Airworthiness Directive 2012-0183R1, dated September 28, 2012 (referred
to after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states:
At least one incident occurred where, immediately after take-
off, the passenger door of a Dornier 328 aeroplane completely
opened. The flight crew reportedly had no cockpit indication or
audible chime prior to this event. The aeroplane returned to the
departure airfield and made an uneventful emergency landing.
Substantial damage to the door, handrails, door hinge arms and
fuselage skin were found.
The subsequent investigation could not find any deficiency in
the design of the main cabin door locking mechanism. In addition, no
technical failure could be determined that precipitated the event.
The flight data recorder showed that the door was closed and locked
before take-off and opened shortly afterwards. Although final proof
could not be obtained, the most likely way in which the door opened
was that the door handle was inadvertently operated during the take-
off run.
In response to the incident, AvCraft (the TC holder at the time)
developed a placard set to warn the occupants against touching the
door handle, as well as a structural modification of the passenger
door hinge supports described in [Dornier 328 Support Services]
Service Bulletin (SB) SB-328-52-460 and SB-328J-52-213 to make
certain that the door does not separate from the aeroplane when
inadvertently opened during flight, allowing a safe descent and
landing.
EASA issued AD 2007-0199 (https://ad.easa.europa.eu/ad/2007-0199)
to require the installation of warning placards and modification as
detailed in these SB instructions.
Since that [EASA] AD [2007-0199] was issued, 328 Support
Services GmbH (the current type certificate holder) have determined
that certain fasteners, identified by Part Number (P/N) NAS6703U1
and P/N NAS6703U2, which were installed as part of the modification,
have the wrong length and must be replaced.
For the reasons described above, this [EASA] AD retains the
requirements of EASA AD 2007-0199, which is superseded, and requires
replacement of the affected fasteners by the ones that have the
correct length.
This [EASA] AD has been revised to correct and clarify the
actions required by paragraph (3).
This AD also adds new airplanes and removes one airplane from the
applicability of this AD. You may examine the MCAI in the AD docket on
the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2013-
0702.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (78 FR 52872, August 27,
2013), or on the determination of the cost to the public.
Conclusion
We reviewed the available data and determined that air safety and
the public interest require adopting this 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 (78 FR 52872, August 27, 2013) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (78 FR 52872, August 27, 2013).
Costs of Compliance
We estimate that this AD affects 35 airplanes of U.S. registry.
The actions that are required by AD 2008-14-16, Amendment 39-15611
(73 FR 40955, July 17, 2008), and retained in this AD take about 38
work-hours per product, at an average labor rate of $85 per work-hour.
Required parts cost about $11,961 per product. Based on these figures,
the estimated cost of the
[[Page 12372]]
actions that were required by AD 2008-14-16 is $15,191 per product.
We also estimate that it will take about 25 work-hours per product
to comply with the new basic requirements of this AD. The average labor
rate is $85 per work-hour. Required parts will cost about $0 per
product. Based on these figures, we estimate the cost of this AD on
U.S. operators to be $74,375, or $2,125 per product.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that
authority because it addresses an unsafe condition that is likely
to exist or develop on products identified in this rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2013-0702; or in person at the
Docket Management Facility between 9 a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD docket contains this AD, the
regulatory evaluation, any comments received, and other information.
The street address for the Docket Operations
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
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 Airworthiness Directive (AD)
2008-14-16, Amendment 39-15611 (73 FR 40955, July 17, 2008), and adding
the following new AD:
2014-03-15 328 Support Services GmbH (Type Certificate Previously
Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier
Luftfahrt GmbH): Amendment 39-17753. Docket No. FAA-2013-0702;
Directorate Identifier 2012-NM-181-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective April 9,
2014.
(b) Affected ADs
This AD supersedes AD 2008-14-16, Amendment 39-15611 (73 FR
40955, July 17, 2008).
(c) Applicability
This AD applies to 328 Support Services GmbH (Type Certificate
previously held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH;
Dornier Luftfahrt GmbH) airplanes, certificated in any category,
identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Model 328-100 airplanes, serial numbers 3005 through 3101
inclusive, 3103, 3104, 3106, 3109, 3110, 3112, 3113, 3115, 3117, and
3119.
(2) Model 328-300 airplanes, all serial numbers.
(d) Subject
Air Transport Association (ATA) of America Code 11, Placards and
Markings; and Code 52, Doors.
(e) Reason
This AD was prompted by reports that certain fasteners, which
were installed as part of a modification, are the wrong length. We
are issuing this AD to prevent incidents of inadvertent opening and
possible detachment of a passenger door in-flight, resulting in
damage to airframe and systems and loss of control of the airplane.
(f) Compliance
You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.
(g) Retained Installation and Modification for Airplanes Identified in
AD 2008-14-16, Amendment 39-15611 (73 FR 40955, July 17, 2008) With
Revised Service Information
This paragraph restates the requirements of paragraph (f) of AD
2008-14-16, Amendment 39-15611 (73 FR 40955, July 17, 2008), with
revised service information.
(1) For Model 328-100 airplanes, serial numbers 3005 through
3098 inclusive, 3100, 3106, 3109, 3110, 3112, 3113, 3115, 3117, and
3119; and Model 328-300 airplanes, having serial numbers 3102, 3105,
3108, 3111, 3114, 3116, 3118, and 3120 through 3224 inclusive:
Within 30 days after August 21, 2008, (the effective date of AD
2008-14-16, Amendment 39-15611 (73 FR 40955, July 17, 2008)),
install warning placards on the inside of the passenger door and
service doors, in accordance with the Accomplishment Instructions of
the service information specified in paragraph (g)(1)(i) or
(g)(1)(ii) of this AD, as applicable.
(i) Dornier Service Bulletin SB-328-11-454, dated May 3, 2004
(for Model 328-100 airplanes).
(ii) Dornier Service Bulletin SB-328J-11-209, dated May 3, 2004
(for Model 328-300 airplanes).
(2) For Model 328-100 airplanes, serial numbers 3005 through
3098 inclusive, 3100, 3106, 3109, 3110, 3112, 3113, 3115, 3117, and
3119; and Model 328-300 airplanes, having serial numbers 3102, 3105,
3108, 3111, 3114, 3116, 3118, and 3120 through 3224 inclusive:
Within 12 months after August 21, 2008, the effective date of AD
2008-14-16, Amendment 39-15611 (73 FR 0955, July 17, 2008), modify
the hinge supports and support struts of the passenger doors, in
accordance with the Accomplishment Instructions of the service
information specified in paragraphs (g)(2)(i) through (g)(2)(iv) of
this AD, as applicable. As of the effective date of this AD only the
service information specified in paragraph (g)(2)(ii) or (g)(2)(iv)
of this AD, as applicable, may be used.
(i) Dornier Service Bulletin SB-328-52-460, dated February 4,
2005 (for Model 328-100 airplanes).
(ii) 328 Support Services Service Bulletin SB-328-52-460,
Revision 2, dated March 1, 2012 (for Model 328-100 airplanes).
(iii) Dornier Service Bulletin SB-328J-52-213, dated February 4,
2005, (for Model 328-300 airplanes).
(iv) 328 Support Services Service Bulletin SB-328J-52-213,
Revision 1, dated August 17, 2011 (for Model 328-300 airplanes).
(h) New Installation and Modification for Newly Added Airplanes
For airplanes not identified in paragraph (g) of this AD, do the
actions required by paragraphs (h)(1) and (h)(2) of this AD.
[[Page 12373]]
(1) Within 30 days after the effective date of this AD, install
warning placards on the inside of the passenger door and service
doors, in accordance with the Accomplishment Instructions of Dornier
Service Bulletin SB-328-11-454, dated May 3, 2004 (for Model 328-100
airplanes); or Dornier Service Bulletin SB-328J-11-209, dated May 3,
2004 (for Model 328-300 airplanes); as applicable.
(2) Within 12 months after the effective date of this AD, modify
the hinge supports and support struts of the passenger doors, in
accordance with the Accomplishment Instructions of 328 Support
Services Service Bulletin SB-328-52-460, Revision 2, dated March 1,
2012 (for Model 328-100 airplanes); or 328 Support Services Service
Bulletin SB-328J-52-213, Revision 1, dated August 17, 2011 (for
Model 328-300 airplanes); as applicable.
(i) New Replacement of Fasteners for All Airplanes
For airplanes on which 26 part number NAS6703U1 fasteners were
installed as specified in the service information in paragraphs
(g)(2)(i) and (g)(2)(iii) of this AD: Within 6 months after the
effective date of this AD, replace the 20 affected part number
NAS6703U1 fasteners with new fasteners having part number NAS6703U2,
in accordance with the Accomplishment Instructions of 328 Support
Services Service Bulletin SB-328-52-460, Revision 2, dated March 1,
2012 (for Model 328-100 airplanes); or 328 Support Services Service
Bulletin SB-328J-52-213, Revision 1, dated August 17, 2011 (for
Model 328-300 airplanes); as applicable.
Note 1 to paragraph (i) of this AD: 328 Support Services Service
Bulletin SB-328-52-460, Revision 2, dated March 1, 2012, and 328
Support Services Service Bulletin SB-328J-52-213, Revision 1, dated
August 17, 2011, identify 20 of 26 part number NAS6703U1 fasteners
requiring to be replaced due to incorrect length.
(j) Credit for Previous Actions
This paragraph provides credit for certain actions required by
paragraph (g) and (h)(2) of this AD, if those actions were performed
before the effective date of this AD using 328 Support Services
Service Bulletin SB-328-52-460, Revision 1, dated August 17, 2011,
which is not incorporated by reference.
(k) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, 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 International Branch, send it to ATTN: Todd
Thompson, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone (425) 227-1175; fax (425) 227-1149.
Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov.
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding district
office. The AMOC approval letter must specifically reference this
AD.
(2) 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.
(l) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) European Aviation Safety Agency Airworthiness Directive 2012-
0183R1, dated September 28, 2012, for related information. You may
examine the MCAI in the AD docket on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2013-0702.
(2) Service information identified in this AD that is not
incorporated by reference in this AD may be obtained at the
addresses specified in paragraphs (m)(3) and (m)(4) of this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(3) The following service information was approved for IBR on
April 9, 2014.
(i) 328 Support Services Service Bulletin SB-328-52-460,
Revision 2, dated March 1, 2012.
(ii) 328 Support Services Service Bulletin SB-328J-52-213,
Revision 1, dated August 17, 2011.
(4) The following service information was approved for IBR on
August 21, 2008 (73 FR 40955, July 17, 2008).
(i) Dornier Service Bulletin SB-328-11-454, dated May 3, 2004.
(ii) Dornier Service Bulletin SB-328J-11-209, dated May 3, 2004.
(iii) Dornier Service Bulletin SB-328-52-460, dated February 4,
2005.
(iv) Dornier Service Bulletin SB-328J-52-213, dated February 4,
2005.
(5) For service information identified in this AD, contact 328
Support Services GmbH, Global Support Center, P.O. Box 1252, D-82231
Wessling, Federal Republic of Germany; telephone +49 8153 88111
6666; fax +49 8153 88111 6565; email gsc.op@328support.de; Internet
https://www.328support.de.
(6) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
(7) 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 Renton, Washington, on January 31, 2014.
John P. Piccola,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-02995 Filed 3-4-14; 8:45 am]
BILLING CODE 4910-13-P
