AD 2014-04-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Diamond Aircraft Industries GmbH | DA 42 NG | Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes |
| aircraft | Diamond Aircraft Industries GmbH | DA 42 M-NG | Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes |
Unsafe Condition
Failure of the alternator indication system to indicate warning when one alternator is inoperative.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install the Secondary Configuration Card P/N 010-12074-02 'Additional ALTN FAIL trigger' and System Software P/N 010-00670-10 for all DA 42 NG and DA 42 M-NG airplanes. Install GEA Alternator fail control cable P/N D62-2510-97-00-SB on certain model DA 42 M-NG airplanes. Prohibit installation of System Software prior to P/N 010-00670-10.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Diamond Aircraft Industries GmbH Models DA 42 NG and DA 42 M-NG airplanes, all serial numbers certificated in any category, except those with Supplemental Type Certificate (STC) SA02725NY.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for certain Diamond Aircraft Industries GmbH Models DA 42 NG and DA 42 M-NG 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 the failure of the alternator indication system to indicate warning when one alternator is inoperative. We are issuing this AD to require actions to address the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Diamond Aircraft Industries GmbH Models DA 42
NG and DA 42 M NG airplanes, all serial numbers certificated in any
category, except those that have incorporated Supplemental Type
Certificate (STC) SA02725NY (<a href="http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/286A29A0C46D66048625764900624649?OpenDocument&Highlight=sa02725ny">http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/286A29A0C46D66048625764900624649?OpenDocument&Highlight=sa02725ny</a>).
Note 1 to paragraph (c) of this AD: STC SA02725NY uses
different electrical system architecture and the unsafe condition
addressed in this AD does not apply to that system.
[[Page 11697]]
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 79, Number 41 (Monday, March 3, 2014)]
[Rules and Regulations]
[Pages 11695-11697]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2014-03604]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0937; Directorate Identifier 2013-CE-029-AD;
Amendment 39-17762; AD 2014-04-04]
RIN 2120-AA64
Airworthiness Directives; Diamond Aircraft Industries GmbH
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Diamond Aircraft Industries GmbH Models DA 42 NG and DA 42 M-NG
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 the failure of the alternator
indication system to indicate warning when one alternator is
inoperative. We are issuing this AD to require actions to address the
unsafe condition on these products.
DATES: This AD is effective April 7, 2014.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of April 7, 2014.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating it in Docket No. FAA-
2013-0937; 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 Diamond
Aircraft Industries GmbH, N.A. Otto-Stra[szlig]e 5, A-2700 Wiener
Neustadt, Austria, telephone: +43 2622 26700; fax: +43 2622 26700 1369;
email: <a href="/cdn-cgi/l/email-protection#4d2c243f3a223f39252423283e3e0d29242c20222329602c243f632c39"><span class="__cf_email__" data-cfemail="fb9a92898c94898f9392959e8888bb9f929a9694959fd69a9289d59a8f">[email protected]</span></a>; Internet: <a href="http://www.diamond-air.at">http://www.diamond-air.at</a>. 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: Mike Kiesov, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4144; fax: (816) 329-4090; email:
<a href="/cdn-cgi/l/email-protection#3f5256545a1154565a4c50497f595e5e11585049"><span class="__cf_email__" data-cfemail="14797d7f713a7f7d71677b62547275753a737b62">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to certain Diamond Aircraft
Industries GmbH Models DA 42 NG and DA 42 M-NG airplanes. That NPRM was
published in the Federal Register on November 6, 2013 (78 FR 66666).
That 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:
During maintenance troubleshooting of the DA 42 NG alternator
indication system it has been discovered that, with one alternator
inoperative, the system did not give a warning indication as
described in the Airplane Flight Manual.
Subsequent investigation results showed that the voltage
regulator warning circuit,
[[Page 11696]]
which is part of the engine, monitors Bus Voltage and is the only
trigger for the alternator fail annunciation. As a result, one
alternator may fail but the related voltage regulator does not
trigger the alternator fail annunciation as the voltage is being
held at the regular level by the second alternator on board.
The remaining generating system indication for the pilot is
unaffected. The ampere-meter is indicating a load on each alternator
and in case of a Low Voltage condition a caution message will be
displayed.
This condition, if not corrected, could lead to an undetected
loss of one engine alternator and reduced capability of the
electrical generating power system, possibly impairing safe
continuation of the flight.
Prompted by this event, Diamond Aircraft Industries (DAI)
introduced at airframe level an additional independent alternator
fail caution trigger by using the G1000 ampere-meter signals. The
trigger is set once an alternator provides less than 5A and thus
indicates electrical power supply failure to the ship system.
DAI issued Mandatory Service Bulletin (MSB) 42NG-003/12
providing instructions for installation of the Secondary
Configuration Card Part Number (P/N) 010-12074-02 ``Additional ALTN
FAIL trigger'' with system software P/N 010-00670-10 applicable for
all DA 42 NG and DA 42 M-NG aeroplanes.
In addition, model DA 42 M-NG now incorporates an output of the
GEA 71 to activate the alternator fail relay. DAI issued Mandatory
Service Bulletin (MSB) 42MNG-006 to provide instructions for
installation of that additional control cable P/N D62-2510-97-00-SB.
For the reasons described above, this AD requires installation
of the Secondary Configuration Card P/N 010-12074-02 ``Additional
ALTN FAIL trigger'' and System Software P/N 010-00670-10 for all DA
42 NG and DA 42 M-NG aeroplanes and installation of GEA Alternator
fail control cable P/N D62-2510-97-00-SB on certain model DA 42 M-NG
aeroplanes.
This AD also prohibits installation of System Software prior to
P/N 010-00670-10.
The MCAI can be found in the AD docket on the Internet at: <a href="http://www.regulations.gov/#!documentDetail">http://www.regulations.gov/#!documentDetail</a>;D=FAA-2013-0937-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (78 FR 66666, November 6,
2013) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data, considered the comments received,
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:
<bullet> Are consistent with the intent that was proposed in the
NPRM (78 FR 66666, November 6, 2013) for correcting the unsafe
condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (78 FR 66666, November 6, 2013).
Costs of Compliance
We estimate that this AD will affect 26 products of U.S. registry.
We also estimate that it would take about 2 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts would cost about $ 115 per
product.
Based on these figures, we estimate the cost of the AD on U.S.
operators to be $7,410, or $285 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 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a>; 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:
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:
2014-04-04 Diamond Aircraft Industries GmbH: Amendment 39-17762;
Docket No. FAA-2013-0937; Directorate Identifier 2013-CE-029-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective April 7,
2014.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Diamond Aircraft Industries GmbH Models DA 42
NG and DA 42 M NG airplanes, all serial numbers certificated in any
category, except those that have incorporated Supplemental Type
Certificate (STC) SA02725NY (<a href="http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/286A29A0C46D66048625764900624649?OpenDocument&Highlight=sa02725ny">http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/286A29A0C46D66048625764900624649?OpenDocument&Highlight=sa02725ny</a>).
Note 1 to paragraph (c) of this AD: STC SA02725NY uses
different electrical system architecture and the unsafe condition
addressed in this AD does not apply to that system.
[[Page 11697]]
(d) Subject
Air Transport Association of America (ATA) Code 24: Electric
Power.
(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 failure of the
alternator indication system to indicate warning when one alternator
is inoperative. We are issuing this AD to prevent the undetected
loss of one engine alternator, which could result in reduced
capability of the electrical generating power system.
(f) Actions and Compliance
Unless already done, do the following actions as specified in
paragraphs (f)(1) through (f)(3) of this AD, including all
subparagraphs:
(1) For all DA 42 NG airplanes: Within the next 12 months after
April 7, 2014 (the effective date of this AD), install Secondary
Configuration Card part number (P/N) 010-12074-02 ``Additional ALTN
FAIL trigger'' and System Software P/N 010-00670-10 following the
Accomplishment/Instructions in Diamond Aircraft Industries GmbH
Mandatory Service Bulletin No. MSB 42NG-003/13, dated October 11,
2013; or the Accomplishment/Instructions in Diamond Aircraft
Industries GmbH Mandatory Service Bulletin No. MSB 42NG-003/12,
dated July 8, 2013.
(2) For DA 42 M-NG airplanes, serial numbers (S/Ns) 42.339,
42.MN001 through 42.MN0026, and all S/Ns modified through Optional
Service Bulletin (OSB) 42-081, using Work Instruction (WI) OSB-42-
081 up to Revision 1 inclusive: Within the next 100 hours time-in-
service after April 7, 2014 (the effective date of this AD) or
within the next 12 months after April 7, 2014 (the effective date of
this AD), whichever occurs first:
(i) Install GEA Alternator fail control cable P/N D62-2510-97-
00-SB following the Instructions in Diamond Aircraft Industries GmbH
Work Instruction WI-MSB 42MNG-006, dated July 8, 2013, as specified
in the Accomplishments/Instructions in Diamond Aircraft Industries
GmbH Mandatory Service Bulletin No. MSB 42MNG-006, July 8, 2013; and
(ii) Install Secondary Configuration Card P/N 010-12074-02
``Additional ALTN FAIL trigger'' and System Software P/N 010-00670-
10 following the Accomplishment/Instructions in Diamond Aircraft
Industries GmbH Mandatory Service Bulletin No. MSB 42NG-003/13,
dated October 11, 2013; or the Accomplishment/Instructions in
Diamond Aircraft Industries GmbH Mandatory Service Bulletin No. MSB
42NG-003/12, dated July 8, 2013.
(3) For all airplanes: As of April 7, 2014 (the effective date
of this AD), do not install on any airplane System Software prior to
P/N 010-00670-10.
(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: Mike Kiesov, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4144; fax: (816) 329-4090; email:
<a href="/cdn-cgi/l/email-protection#f39e9a9896dd989a96809c85b3959292dd949c85"><span class="__cf_email__" data-cfemail="d1bcb8bab4ffbab8b4a2bea791b7b0b0ffb6bea7">[email protected]</span></a>. 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 European Aviation Safety Agency (EASA) AD No.:
2013-0224, dated September 19, 2013, for more information. The MCAI
can be found in the AD docket on the Internet at: <a href="http://www.regulations.gov/#!documentDetail">http://www.regulations.gov/#!documentDetail</a>;D=FAA-2013-0937-0002. You may
also refer to Diamond Aircraft Industries GmbH Optional Service
Bulletin OSB 42-081/1 and Diamond Aircraft Industries GmbH Work
Instruction WI-OSB 42-081, Rev. 1, both dated December 23, 2010; and
Diamond Aircraft Industries GmbH Optional Service Bulletin OSB 42-
081 and Diamond Aircraft Industries GmbH Work Instruction WI-OSB 42-
081, Rev. 0, both dated March 17, 2010, for more information. For
service information related to this AD, you may contact the
manufacturer using the information found in paragraph (i)(3) of this
AD.
(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) Diamond Aircraft Industries GmbH Mandatory Service Bulletin
No. MSB 42NG-003/13, dated October 11, 2013.
(ii) Diamond Aircraft Industries GmbH Mandatory Service Bulletin
No. MSB 42NG-003/12, dated July 8, 2013.
(iii) Diamond Aircraft Industries GmbH Mandatory Service
Bulletin MSB 42MNG-006, dated July 8, 2013.
(iv) Diamond Aircraft Industries GmbH Work Instruction WI-MSB
42MNG-006, dated July 8, 2013.
(3) For Diamond Aircraft Industries GmbH service information
identified in this AD, contact Diamond Aircraft Industries GmbH,
N.A. Otto-Stra[szlig]e 5, A-2700 Wiener Neustadt, Austria,
telephone: +43 2622 26700; fax: +43 2622 26700 1369; email:
<a href="/cdn-cgi/l/email-protection#c2a3abb0b5adb0b6aaabaca7b1b182a6aba3afadaca6efa3abb0eca3b6"><span class="__cf_email__" data-cfemail="d1b0b8a3a6bea3a5b9b8bfb4a2a291b5b8b0bcbebfb5fcb0b8a3ffb0a5">[email protected]</span></a>; Internet: <a href="http://www.diamond-air.at">http://www.diamond-air.at</a>.
(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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Kansas City, Missouri, on February 12, 2014.
Steven W. Thompson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-03604 Filed 2-28-14; 8:45 am]
BILLING CODE 4910-13-P
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