Airworthiness Directives; Alpha Aviation Concept Limited Airplanes, 26608-26610 [2014-10058]
Download as PDF
26608
Federal Register / Vol. 79, No. 90 / Friday, May 9, 2014 / Rules and Regulations
detailed and surface high-frequency eddy
current inspections for cracks in the tension
ties at body station (BS) 880 to 1100, 1120,
1160, 1200, and 1220, and do all applicable
corrective actions, in accordance with the
Accomplishment Instructions of Boeing Alert
Service Bulletin 747–53A2610, Revision 1,
dated December 4, 2012, except as required
by paragraph (j)(3) of this AD. Do all
applicable corrective actions before further
flight. Repeat the inspections thereafter at the
applicable time specified in paragraph 1.E.,
‘‘Compliance,’’ of Boeing Alert Service
Bulletin 747–53A2610, Revision 1, dated
December 4, 2012, until the tension ties have
been modified as required by paragraph (h)
of this AD or as specified in paragraph (i) of
this AD. Repair or modification of a tension
tie at any location in accordance with Part 3
of the Accomplishment Instructions of
Boeing Alert Service Bulletin 747–53A2610,
Revision 1, dated December 4, 2012,
terminates the repetitive inspection
requirements of this AD for that tension tie
location only.
(h) Tension Tie Modification: BS 880 to 1100
At the applicable time specified in
paragraph 1.E., ‘‘Compliance,’’ of Boeing
Alert Service Bulletin 747–53A2610,
Revision 1, dated December 4, 2012, except
as specified in paragraph (j)(2) of this AD:
Modify the tension ties from BS 880 to 1100,
and do all applicable related investigative
and corrective actions, in accordance with
Part 3 of the Accomplishment Instructions of
Boeing Alert Service Bulletin 747–53A2610,
Revision 1, dated December 4, 2012, except
as required by paragraph (j)(3) of this AD. Do
all applicable related investigative and
corrective actions before further flight.
Modification as required by this paragraph
terminates the repetitive inspection
requirements of paragraph (g) of this AD for
the affected tension tie location(s) only.
ehiers on DSK2VPTVN1PROD with RULES
(i) Optional Terminating Action: BS 1120 to
1220
Modification of a tension tie at BS 1120 to
1220 in accordance with Boeing Service
Bulletin 747–53A2559, Revision 1, dated
August 4, 2011, except as required by
paragraph (j)(4) of this AD, terminates the
requirements of paragraph (g) of this AD for
that tension tie location only. Paragraph (p)
of AD 2012–15–13, Amendment 39–17142
(77 FR 47267, August 8, 2012), mandates the
accomplishment of the modification and
associated actions specified in Boeing
Service Bulletin 747–53A2559, Revision 1,
dated August 4, 2011.
(j) Service Information Clarification and
Exceptions
(1) Paragraph 1.E., ‘‘Compliance,’’ of
Boeing Alert Service Bulletin 747–53A2610,
Revision 1, dated December 4, 2012, specifies
certain compliance times ‘‘after August 28,
2007.’’ August 28, 2007, is the effective date
of AD 2007–16–19, Amendment 39–15158
(72 FR 45151, August 13, 2007).
(2) Where Boeing Alert Service Bulletin
747–53A2610, Revision 1, dated December 4,
2012, specifies a compliance time ‘‘after the
Revision 1 date of this service bulletin,’’ this
AD requires compliance within the specified
time after the effective date of this AD.
VerDate Mar<15>2010
13:40 May 08, 2014
Jkt 232001
(3) Where Boeing Alert Service Bulletin
747–53A2610, Revision 1, dated December 4,
2012, specifies to contact Boeing for certain
repair instructions: Repair before further
flight using a method approved in
accordance with the procedures specified in
paragraph (l) of this AD.
(4) Where Boeing Service Bulletin 747–
53A2559, Revision 1, dated August 4, 2011,
specifies to contact Boeing for repair
instructions or additional modification
requirements, repair of the cracking or
additional actions must be done using a
method approved in accordance with the
procedures specified in paragraph (l) of this
AD.
(k) Credit for Previous Actions
This paragraph provides credit for the
detailed inspections, repairs, and
modification specified in paragraphs (g) and
(h) of this AD, for that affected tension tie
location only, if those actions were
performed before the effective date of this AD
using Boeing Alert Service Bulletin 747–
53A2610, dated May 10, 2007 (which is not
incorporated by reference in this AD).
(l) 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 (m)(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) AMOCs approved previously in
accordance with AD 2007–16–19,
Amendment 39–15158 (72 FR 45151, August
13, 2007), are approved as AMOCs for the
corresponding provisions of this AD.
(m) Related Information
(1) For more information about this AD,
contact Bill Ashforth, Aerospace Engineer,
Airframe Branch, ANM–120S, FAA, Seattle
Aircraft Certification Office (ACO), 1601 Lind
Avenue SW., Renton, WA 98057–3356;
phone: 425–917–6432; fax: 425–917–6590;
email: bill.ashforth@faa.gov.
(2) Service information identified in this
AD that is not incorporated by reference may
be viewed at the addresses specified in
paragraphs (n)(4) and (n)(5) of this AD.
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
(n) 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.
(3) The following service information was
approved for IBR on June 13, 2014.
(i) Boeing Alert Service Bulletin 747–
53A2610, Revision 1, dated December 4,
2012.
(ii) Reserved.
(4) The following service information was
approved for IBR on September 12, 2012 (77
FR 47267, August 8, 2012).
(i) Boeing Service Bulletin 747–53A2559,
Revision 1, dated August 4, 2011.
(ii) Reserved.
(5) 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.
(6) You may view this service information
at FAA, 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/ibrlocations.html.
Issued in Renton, Washington, on April 22,
2014.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2014–09832 Filed 5–8–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0130; Directorate
Identifier 2014–CE–005–AD; Amendment
39–17847; AD 2014–09–12]
RIN 2120–AA64
Airworthiness Directives; Alpha
Aviation Concept Limited Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for certain
Alpha Aviation Concept Limited Model
R2160 airplanes. This AD results from
SUMMARY:
E:\FR\FM\09MYR1.SGM
09MYR1
Federal Register / Vol. 79, No. 90 / Friday, May 9, 2014 / Rules and Regulations
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 the
metal screen shield over the ignition
switch may ground out the ignition
terminals. We are issuing this AD to
require actions to address the unsafe
condition on these products.
DATES: This AD is effective June 13,
2014.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of June 13, 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–
0130; or in person at Document
Management Facility, U.S. Department
of Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue SE., Washington, DC 20590.
For service information identified in
this AD, contact Alpha Aviation, 59
Hautapu Road, RD 1, Cambridge 3493,
New Zealand; telephone: +64 7 827
0528; fax: +64 7 929 2878; Internet:
www.alphaaviation.co.nz. 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.
FOR FURTHER INFORMATION CONTACT: Karl
Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4123 ; fax: (816)
329–4090; email:
karl.schletzbaum@faa.gov.
SUPPLEMENTARY INFORMATION:
ehiers on DSK2VPTVN1PROD with RULES
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to add an AD that would apply
to certain Alpha Aviation Concept
Limited Model R2160 airplane. The
NPRM was published in the Federal
Register on March 3, 2014 (79 FR
11723). The NPRM proposed to correct
an unsafe condition for the specified
products and was based on mandatory
continuing airworthiness information
(MCAI) originated by an aviation
authority of another country. The MCAI
states:
The AD is prompted by an overseas
DR300/180R aircraft accident which occurred
during take-off. Investigation revealed a
distorted metal screen shield which
VerDate Mar<15>2010
13:40 May 08, 2014
Jkt 232001
grounded the ignition switch terminals and
resulted in loss of engine power.
Robin aircraft manufactured prior to 1985
were fitted with ignition switches protected
with a metal screen shield. With subsequent
radio and electrical system improvements
ignition switch shielding is no longer
required, and most aircraft do not have metal
screen shielded ignition switches.
This AD requires a one-time inspection of
the ignition switch to determine if a metal
screen shield is installed, and depending on
findings, to modify or replace the ignition
switch with a serviceable part. The AD
prohibits the installation of a metal screen
shield ignition switch on any aircraft.
The MCAI can be found in the AD
docket on the Internet at https://
www.regulations.gov/
#!documentDetail;D=FAA-2014-01300002.
26609
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 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
11723, March 3, 2014) for correcting the
unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM (79 FR 11723,
March 3, 2014).
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.
Costs of Compliance
Examining the AD Docket
We estimate that this AD will affect
10 products of U.S. registry. We also
estimate that it will take about 3 workhours per product to comply with the
basic requirements of this AD. The
average labor rate is $85 per work-hour.
Based on these figures, we estimate
the cost of this AD on U.S. operators to
be $2,550, or $255 per product.
In addition, we estimate that any
necessary follow-on actions will take
about 3 work-hours and require parts
costing $100, for a cost of $355 per
product. We have no way of
determining the number of products
that may need these actions.
You may examine the AD docket on
the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2012–
0130; 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.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM (79
FR 11723, March 3, 2014) or on the
determination of the cost to the public.
Conclusion
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
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
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,
E:\FR\FM\09MYR1.SGM
09MYR1
26610
Federal Register / Vol. 79, No. 90 / Friday, May 9, 2014 / Rules and Regulations
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
■
2014–09–12 Alpha Aviation Concept
Limited: Amendment 39–17847; Docket
No. FAA–2014–0130; Directorate
Identifier 2014–CE–005–AD.
(a) Effective Date
This airworthiness directive (AD) becomes
effective June 13, 2014.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Alpha Aviation
Concept Limited Model R2160 airplanes,
serial numbers 001 through 378, certificated
in any category.
(d) Subject
Air Transport Association of America
(ATA) Code 74: Ignition.
ehiers on DSK2VPTVN1PROD with RULES
(f) Actions and Compliance
Unless already done, do the actions in
paragraphs (f)(1) through (f)(3) of this AD:
(1) Within the next 50 hours time-inservice after June 13, 2014 (the effective date
of this AD) or within the next 3 months after
June 13, 2014 (the effective date of this AD),
whichever occurs first, inspect the airplane
ignition switch for the presence of a metal
screen shield. Do the inspection following
the Accomplishment Instructions in Alpha
Aviation Service Bulletin AA–SB–24–002,
Revision 0, dated January 2014.
(2) If a metal screen is found during the
inspection required in paragraph (f)(1) of this
AD, before further flight, modify or replace
the ignition switch following the
Accomplishment Instructions in Alpha
Aviation Service Bulletin AA–SB–24–002,
Revision 0, dated January 2014.
(3) As of June 13, 2014 (the effective date
of this AD), do not install an ignition switch
with a metal screen shield.
(g) Other FAA AD Provisions
The following provisions also apply to this
AD:
13:40 May 08, 2014
Jkt 232001
(h) Related Information
Refer to MCAI Civil Aviation Authority
(CAA) AD DCA/R2000/42, dated January 29,
2014, for related information. You may
examine the MCAI on the Internet at https://
www.regulations.gov/
#!documentDetail;D=FAA-2014-0130-0002.
(i) Material Incorporated by Reference
(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 the metal
screen shield over the ignition switch may
ground out the ignition terminals. We are
issuing this AD to prevent the ignition switch
metal screen from grounding out the ignition
switch terminals, which could cause the
engine to shut down.
VerDate Mar<15>2010
(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: Karl Schletzbaum, Aerospace
Engineer, FAA, Small Airplane Directorate,
901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329–4123; fax: (816)
329–4090; email: karl.schletzbaum@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.
(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) Alpha Aviation Service Bulletin AA–
SB–24–002, Revision 0, dated January 2014.
(ii) Reserved.
(3) For Alpha Aviation Concept Limited
service information identified in this AD,
contact Alpha Aviation, 59 Hautapu Road,
RD 1, Cambridge 3493, New Zealand;
telephone: +64 7 827 0528; fax: +64 7 929
2878; Internet: www.alphaaviation.co.nz.
(4) You may view this service information
at the FAA, Small Airplane Directorate, 901
Locust, Kansas City, Missouri 64106. For
information on the availability of this
material at the FAA, call (816) 329–4148.
(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 Kansas City, Missouri, on April
25, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2014–10058 Filed 5–8–14; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
Frm 00020
Fmt 4700
Sfmt 4700
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0092; Directorate
Identifier 2014–CE–002–AD; Amendment
39–17846; AD 2014–09–11]
RIN 2120–AA64
Airworthiness Directives; GROB–
WERKE Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for certain
GROB–WERKE Models G115EG and
G120A 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 cracks
in the left hand elevator flange. We are
issuing this AD to require actions to
address the unsafe condition on these
products.
SUMMARY:
This AD is effective June 13,
2014.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of June 13, 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–
0092; or in person at Document
Management Facility, U.S. Department
of Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue SE., Washington, DC 20590.
For service information identified in
this AD, contact Grob Aircraft AG,
Customer Service, Lettenbachstrasse 9,
86874 Tussenhausen-Mattsies,
Germany, telephone: + 49 (0) 8268–998–
105; fax; + 49 (0) 8268–998–200; email:
productsupport@grob-aircraft.com;
Internet: grob-aircraft.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.
FOR FURTHER INFORMATION CONTACT: Karl
Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4123; fax: (816)
DATES:
E:\FR\FM\09MYR1.SGM
09MYR1
Agencies
[Federal Register Volume 79, Number 90 (Friday, May 9, 2014)]
[Rules and Regulations]
[Pages 26608-26610]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-10058]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0130; Directorate Identifier 2014-CE-005-AD;
Amendment 39-17847; AD 2014-09-12]
RIN 2120-AA64
Airworthiness Directives; Alpha Aviation Concept Limited
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Alpha Aviation Concept Limited Model R2160 airplanes. This AD results
from
[[Page 26609]]
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 the metal screen shield over the ignition switch may
ground out the ignition terminals. We are issuing this AD to require
actions to address the unsafe condition on these products.
DATES: This AD is effective June 13, 2014.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of June 13,
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-
0130; or in person at Document Management Facility, U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
For service information identified in this AD, contact Alpha
Aviation, 59 Hautapu Road, RD 1, Cambridge 3493, New Zealand;
telephone: +64 7 827 0528; fax: +64 7 929 2878; Internet:
www.alphaaviation.co.nz. 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.
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4123 ; fax: (816) 329-4090; email:
karl.schletzbaum@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 certain Alpha Aviation Concept
Limited Model R2160 airplane. The NPRM was published in the Federal
Register on March 3, 2014 (79 FR 11723). The NPRM proposed to correct
an unsafe condition for the specified products and was based on
mandatory continuing airworthiness information (MCAI) originated by an
aviation authority of another country. The MCAI states:
The AD is prompted by an overseas DR300/180R aircraft accident
which occurred during take-off. Investigation revealed a distorted
metal screen shield which grounded the ignition switch terminals and
resulted in loss of engine power.
Robin aircraft manufactured prior to 1985 were fitted with
ignition switches protected with a metal screen shield. With
subsequent radio and electrical system improvements ignition switch
shielding is no longer required, and most aircraft do not have metal
screen shielded ignition switches.
This AD requires a one-time inspection of the ignition switch to
determine if a metal screen shield is installed, and depending on
findings, to modify or replace the ignition switch with a
serviceable part. The AD prohibits the installation of a metal
screen shield ignition switch on any aircraft.
The MCAI can be found in the AD docket on the Internet at https://www.regulations.gov/#!documentDetail;D=FAA-2014-0130-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 11723, March 3,
2014) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (79 FR 11723, March 3, 2014) for correcting the unsafe condition;
and
Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 11723, March 3, 2014).
Costs of Compliance
We estimate that this AD will affect 10 products of U.S. registry.
We also estimate that it will take about 3 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $2,550, or $255 per product.
In addition, we estimate that any necessary follow-on actions will
take about 3 work-hours and require parts costing $100, for a cost of
$355 per product. 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-2012-
0130; 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,
[[Page 26610]]
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 adding the following new AD:
2014-09-12 Alpha Aviation Concept Limited: Amendment 39-17847;
Docket No. FAA-2014-0130; Directorate Identifier 2014-CE-005-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective June 13,
2014.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Alpha Aviation Concept Limited Model R2160
airplanes, serial numbers 001 through 378, certificated in any
category.
(d) Subject
Air Transport Association of America (ATA) Code 74: Ignition.
(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 the metal screen
shield over the ignition switch may ground out the ignition
terminals. We are issuing this AD to prevent the ignition switch
metal screen from grounding out the ignition switch terminals, which
could cause the engine to shut down.
(f) Actions and Compliance
Unless already done, do the actions in paragraphs (f)(1) through
(f)(3) of this AD:
(1) Within the next 50 hours time-in-service after June 13, 2014
(the effective date of this AD) or within the next 3 months after
June 13, 2014 (the effective date of this AD), whichever occurs
first, inspect the airplane ignition switch for the presence of a
metal screen shield. Do the inspection following the Accomplishment
Instructions in Alpha Aviation Service Bulletin AA-SB-24-002,
Revision 0, dated January 2014.
(2) If a metal screen is found during the inspection required in
paragraph (f)(1) of this AD, before further flight, modify or
replace the ignition switch following the Accomplishment
Instructions in Alpha Aviation Service Bulletin AA-SB-24-002,
Revision 0, dated January 2014.
(3) As of June 13, 2014 (the effective date of this AD), do not
install an ignition switch with a metal screen shield.
(g) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Office, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. Send
information to ATTN: Karl Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4123; fax: (816) 329-4090;
email: karl.schletzbaum@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.
(h) Related Information
Refer to MCAI Civil Aviation Authority (CAA) AD DCA/R2000/42,
dated January 29, 2014, for related information. You may examine the
MCAI on the Internet at https://www.regulations.gov/#!documentDetail;D=FAA-2014-0130-0002.
(i) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Alpha Aviation Service Bulletin AA-SB-24-002, Revision 0,
dated January 2014.
(ii) Reserved.
(3) For Alpha Aviation Concept Limited service information
identified in this AD, contact Alpha Aviation, 59 Hautapu Road, RD
1, Cambridge 3493, New Zealand; telephone: +64 7 827 0528; fax: +64
7 929 2878; Internet: www.alphaaviation.co.nz.
(4) You may view this service information at the FAA, Small
Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148.
(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/ibr-locations.html
Issued in Kansas City, Missouri, on April 25, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2014-10058 Filed 5-8-14; 8:45 am]
BILLING CODE 4910-13-P