Published 2013-08-16 · Federal Register document 2013-18912
Airworthiness Directives; Eclipse Aerospace, Inc. Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for all Eclipse Aerospace, Inc. Model EA500 airplanes equipped with Avio, Avio with ETT, or Avio NG 1.0 avionics suites. This AD was prompted by a report of potential aircraft hardware failure in the autopilot control panel and the center switch panel. This AD requires either incorporating updates to the aircraft computer system software or incorporating a temporary revision to the aircraft flight manual. We are issuing this AD to correct the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2013-a7b684f4a1b4614e
- Source row
- results[252]
- Raw source SHA-256
- a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2013-16-04
- Effective date printed in this edition
- 2013-09-20
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective September 20, 2013.
Exact source excerpt. Text positions 10536–10602, end exclusive, in the original decoded publication. SHA-256: 8b3d5cbc98981c4a4a70d99ff1e976a7d1fedd84be856cfc17a77b32f8d3cdf7
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10602–10631, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to the following Eclipse Aerospace, Inc. Model
EA500 airplanes, all serial numbers, that are certificated in any
category, and are equipped with:
(1) Avio avionics suites; or
(2) Avio with ETT avionics suites; or
(3) Avio NG 1.0 avionics suites.
Exact source excerpt. Text positions 10631–10931, end exclusive, in the original decoded publication. SHA-256: c5e1fdba9c8fa701d925e41e3563079ce9d9f71c8754b35f05fb276cc4ae8cde
Subject
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code, Code 23: Communications.
Exact source excerpt. Text positions 10931–11063, end exclusive, in the original decoded publication. SHA-256: 62731422212e20cc1338600dbd7d51bd349d462db76dfbd5ef8c451088e07765
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a report of potential aircraft hardware
failure in the
[[Page 49910]]
autopilot control panel and the center switch panel. We are issuing
this AD to prevent failure of the hardware/software combination
within the autopilot control panel and/or center switch panel, which
could result in uncommanded fire suppression system activation and
simultaneous shutdown of both engines.
Exact source excerpt. Text positions 11063–11498, end exclusive, in the original decoded publication. SHA-256: 8ac569600a0d33b54f4cfdc2ae13bdfb76cadd968d1e912115407bf3aefa1f98
Compliance
(f) Compliance
Unless already done, do the following actions within the
compliance times specified in paragraph (g) of this AD.
Exact source excerpt. Text positions 11498–11633, end exclusive, in the original decoded publication. SHA-256: ef3be8dc5f58026b28ccc2ec9d91fdc149a556d6eb963cb6e246221f97754525
Update Aircraft Computer Software (ACS)
(g) Update Aircraft Computer Software (ACS)
(1) For airplanes equipped with Avio or Avio with ETT avionics
suites: Within 6 calendar months after September 20, 2013 (the
effective date of this AD), update the ACS following paragraphs 3.A.
through 3.C. of the Accomplishment Instructions in Eclipse
Aerospace, Inc. Mandatory Service Bulletin Number SB 500-31-014,
Rev. A, dated February 15, 2011.
(2) For airplanes equipped with NG 1.0 avionics suites: Within 6
calendar months after September 20, 2013 (the effective date of this
AD), do one of the following:
(i) Insert Temporary Revision No. 016, to EA500 POH and FAA-
Approved Airplane Flight Manual, Firewall Valve, 06-122204-TR016,
issued November 9, 2012, into the Limitations section of the
airplane flight manual following paragraph 3.B.(1)(a) of the
Accomplishment Instructions in Eclipse Aerospace, Inc. Mandatory
Service Bulletin Number SB 500-31-026, Rev. A, dated December 7,
2012, or Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-026, Rev. B, dated March 27, 2013; or
(ii) Update the ACS following paragraphs 3.A. through 3.C. of
the Accomplishment Instructions in Eclipse Aerospace, Inc. Mandatory
Service Bulletin Number SB 500-31-019, Rev. B, dated March 13, 2013.
Exact source excerpt. Text positions 11633–12920, end exclusive, in the original decoded publication. SHA-256: e99625eaad8098be8ca1ab17028a14c50de67861876a459e546a1062747b2153
Alternative Methods of Compliance (AMOCs)
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Chicago 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 the Related Information
section of this AD.
(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.
Exact source excerpt. Text positions 12920–13662, end exclusive, in the original decoded publication. SHA-256: ae487e9da6eb812a15607029745b4ae82aaa3c3224af07026fa488a307f24cd7
Related Information
(i) Related Information
For more information about this AD, contact Scott Fohrman,
Aerospace Engineer, FAA, Chicago ACO, 2300 East Devon Avenue, Room
107, Des Plaines, Illinois 60018; phone: (847) 294-7136; fax: (847)
294-7834; email: [email protected].
Exact source excerpt. Text positions 13662–13925, end exclusive, in the original decoded publication. SHA-256: 6d9cce8c14c4b38bc5c7a8cc6ac68e1dea6de2a1ab21d15952a819432a53ca2a
Material Incorporated by Reference
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number SB
500-31-014, Rev. A, dated February 15, 2011.
(ii) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-019, Rev. B, dated March 13, 2013.
(iii) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-026, Rev. A, dated December 7, 2012.
(iv) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-026, Rev. B, dated March 27, 2013.
(v) Temporary Revision No. 016, to EA500 POH and FAA-Approved
Airplane Flight Manual, Firewall Valve, 06-122204-TR016, issued
November 9, 2012.
(3) For Eclipse Aerospace, Inc. service information identified
in this AD, contact Eclipse Aerospace, Inc. 26 East Palatine Road,
Wheeling, Illinois 60090; telephone: (877) 373-7978; Internet:
www.eclipse.aero.
(4) You may review copies of the 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.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 13925–15649, end exclusive, in the original decoded publication. SHA-256: a256bf6085d09097ffcd0ec63f74a96b0c16aedbba41fbfa1add683941118266
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2013-16-04 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 22deca6d25f5a8c2289122ea368fcdb6a66c43fbc25892ab3f20443a12e6a9ea. Source manifest: aa8fd949e784a91a0248f730f1fa7348ffbece2d466a8e9d7d5f0a7c947a726f.
Official source · 2013-08-16
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 78, Number 159 (Friday, August 16, 2013)]
[Rules and Regulations]
[Pages 49908-49910]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-18912]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0448; Directorate Identifier 2013-CE-007-AD;
Amendment 39-17542; AD 2013-16-04]
RIN 2120-AA64
Airworthiness Directives; Eclipse Aerospace, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for all
Eclipse Aerospace, Inc. Model EA500 airplanes equipped with Avio, Avio
with ETT, or Avio NG 1.0 avionics suites. This AD was prompted by a
report of potential aircraft hardware failure in the autopilot control
panel and the center switch panel. This AD requires either
incorporating updates to the aircraft computer system software or
incorporating a temporary revision to the aircraft flight manual. We
are issuing this AD to correct the unsafe condition on these products.
DATES: This AD is effective September 20, 2013.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of September 20,
2013.
ADDRESSES: For service information identified in this AD, contact
Eclipse Aerospace, Inc., 26 East Palatine Road, Wheeling, Illinois
60090; telephone: (877) 373-7978; Internet: www.eclipse.aero. You may
review copies of the 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.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov; 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 address for the
Docket Office (phone: 800-647-5527) is 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 FURTHER INFORMATION CONTACT: Scott Fohrman, Aerospace Engineer,
FAA, Chicago Aircraft Certification Office, 2300 East Devon Avenue,
Room 107, Des Plaines, Illinois 60018; phone: (847) 294-7136; fax:
(847) 294-7834; email: [email protected].
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 the specified products.
The NPRM published in the Federal Register on May 22, 2013 (78 FR
30243). The NPRM proposed to require either incorporating updates to
the aircraft computer system or incorporating a temporary revision to
the aircraft flight manual.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (78 FR 30243, May 22,
2013) or on the determination of the cost to the public. However, we
have received a revision to one of the service bulletins referenced in
the NPRM. The revision does not add any additional burden to the
owners/operators of the airplanes affected by the NPRM; therefore, we
are including the revised service information into this AD as an
additional method of compliance.
Conclusion
We reviewed the relevant 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:
<bullet> Are consistent with the intent that was proposed in the
NPRM (78 FR 30243, May 22, 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 30243, May 22, 2013).
Differences Between This AD and the Service Information
Eclipse Aerospace, Inc. Mandatory Service Bulletin Number SB 500-
31-026, Rev. A, dated November 6, 2012, and SB 500-31-026, Rev. B,
dated March 27, 2013, which applies only to
[[Page 49909]]
airplanes equipped with NG 1.0 avionics suites, requires incorporating
a temporary revision into the airplane flight manual (AFM) and
incorporating an update to the aircraft computer system (ACS) hardware
with monthly data uploads to Eclipse Aerospace, Inc. until the ACS
software is updated. Specifically, the AFM revision requires an altered
engine start and emergency procedures checklist.
This AD allows doing either the AFM revision or the ACS software
update.
Costs of Compliance
We estimate that this AD affects 81 airplanes of U.S. registry.
There are 38 of the affected airplanes equipped with Avio or Avio ETT
avionics suites and 43 of the affected airplanes equipped with NG 1.0
avionics suites.
We estimate the following costs to comply with this AD. Airplanes
equipped with NG 1.0 avionics suites will be allowed do either the AFM
update or the ACS update:
Estimated Costs for Airplanes Equipped With Avio or Avio ETT Avionics Suites
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
ACS update for airplanes equipped .5 work-hour x $85 $1,950 $1,992.50 $1,992.50 x 38
with Avioor Avio ETT avionics per hour = $42.50. affected airplanes
suites. = $75,715.00.
----------------------------------------------------------------------------------------------------------------
Estimated Costs for Airplanes Equipped With NG 1.0 Avionics Suites
[Requires either the AFM update OR the ACS update]
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
AFM update for airplanes equipped .5 work-hour x $85 Not applicable $42.50 $42.50 x 43 affected
with NG 1.0 avionics suites. per hour = $42.50. airplanes =
$1,827.50.
----------------------------------------------------------------------------------------------------------------
OR
----------------------------------------------------------------------------------------------------------------
ACS update for airplanes equipped .5 work-hour x $85 $37,000 $37,042.50 $37,042.50 x 43
with NG 1.0 avionics suites. per hour. affected airplanes
= $42.50............ = $1,592,827.50.
----------------------------------------------------------------------------------------------------------------
Incorporating the AFM update represents a terminating action for AD
compliance without imposing any limitations on aircraft operations. It
is the operator's choice to incorporate either the AFM update or the
ACS update.
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
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 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.
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 airworthiness
directive (AD):
2013-16-04 Eclipse Aerospace, Inc.: Amendment 39-17542; Docket No.
FAA-2013-0448; Directorate Identifier 2013-CE-007-AD.
(a) Effective Date
This AD is effective September 20, 2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the following Eclipse Aerospace, Inc. Model
EA500 airplanes, all serial numbers, that are certificated in any
category, and are equipped with:
(1) Avio avionics suites; or
(2) Avio with ETT avionics suites; or
(3) Avio NG 1.0 avionics suites.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code, Code 23: Communications.
(e) Unsafe Condition
This AD was prompted by a report of potential aircraft hardware
failure in the
[[Page 49910]]
autopilot control panel and the center switch panel. We are issuing
this AD to prevent failure of the hardware/software combination
within the autopilot control panel and/or center switch panel, which
could result in uncommanded fire suppression system activation and
simultaneous shutdown of both engines.
(f) Compliance
Unless already done, do the following actions within the
compliance times specified in paragraph (g) of this AD.
(g) Update Aircraft Computer Software (ACS)
(1) For airplanes equipped with Avio or Avio with ETT avionics
suites: Within 6 calendar months after September 20, 2013 (the
effective date of this AD), update the ACS following paragraphs 3.A.
through 3.C. of the Accomplishment Instructions in Eclipse
Aerospace, Inc. Mandatory Service Bulletin Number SB 500-31-014,
Rev. A, dated February 15, 2011.
(2) For airplanes equipped with NG 1.0 avionics suites: Within 6
calendar months after September 20, 2013 (the effective date of this
AD), do one of the following:
(i) Insert Temporary Revision No. 016, to EA500 POH and FAA-
Approved Airplane Flight Manual, Firewall Valve, 06-122204-TR016,
issued November 9, 2012, into the Limitations section of the
airplane flight manual following paragraph 3.B.(1)(a) of the
Accomplishment Instructions in Eclipse Aerospace, Inc. Mandatory
Service Bulletin Number SB 500-31-026, Rev. A, dated December 7,
2012, or Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-026, Rev. B, dated March 27, 2013; or
(ii) Update the ACS following paragraphs 3.A. through 3.C. of
the Accomplishment Instructions in Eclipse Aerospace, Inc. Mandatory
Service Bulletin Number SB 500-31-019, Rev. B, dated March 13, 2013.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Chicago 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 the Related Information
section of this AD.
(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.
(i) Related Information
For more information about this AD, contact Scott Fohrman,
Aerospace Engineer, FAA, Chicago ACO, 2300 East Devon Avenue, Room
107, Des Plaines, Illinois 60018; phone: (847) 294-7136; fax: (847)
294-7834; email: [email protected].
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number SB
500-31-014, Rev. A, dated February 15, 2011.
(ii) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-019, Rev. B, dated March 13, 2013.
(iii) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-026, Rev. A, dated December 7, 2012.
(iv) Eclipse Aerospace, Inc. Mandatory Service Bulletin Number
SB 500-31-026, Rev. B, dated March 27, 2013.
(v) Temporary Revision No. 016, to EA500 POH and FAA-Approved
Airplane Flight Manual, Firewall Valve, 06-122204-TR016, issued
November 9, 2012.
(3) For Eclipse Aerospace, Inc. service information identified
in this AD, contact Eclipse Aerospace, Inc. 26 East Palatine Road,
Wheeling, Illinois 60090; telephone: (877) 373-7978; Internet:
www.eclipse.aero.
(4) You may review copies of the 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.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on July 31, 2013.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-18912 Filed 8-15-13; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:53:35.919573+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 092e43727e35c07e05fcf3ce7a1d1c03f92f768aad1e4a33e3ce7cd19dbac2c1
- Text SHA-256
- 22deca6d25f5a8c2289122ea368fcdb6a66c43fbc25892ab3f20443a12e6a9ea
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.