Published 2015-07-16 · Federal Register document 2015-17193
Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes
Publication summary
We are revising an airworthiness directive (AD) 2015-06-02 for GA 8 Airvan (Pty) Ltd Model GA8-TC320 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 missing required engine mount fire seal washers, which could reduce the engine retention capability in the event of a fire. We are issuing this AD to require actions to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:48.517946+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2015-3bb842c840a7e6e6
- Source row
- results[152]
- Raw source SHA-256
- 3bb842c840a7e6e6e43779ca68008e1e63ad8287ad840c3a981d1f66a934b14b
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2015-06-02 R1
- Effective date printed in this edition
- 2015-08-20
Read 9 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) becomes effective August 20,
2015.
Exact source excerpt. Text positions 9070–9165, end exclusive, in the original decoded publication. SHA-256: f624b694689edfabc2e175f4318cac11e2c6104e9b1c4161730737e1847d2467
Affected ADs
(b) Affected ADs
This AD revises AD 2015-06-02, Amendment 39-18120 (80 FR 14810;
March 20, 2015).
Exact source excerpt. Text positions 9165–9270, end exclusive, in the original decoded publication. SHA-256: d8ae89ae7d15146dc69a8d3c0fe177a412d492cd32578d7ca5603d26594574be
Applicability wording · Applicability
(c) Applicability
This AD applies to GA 8 Airvan (Pty) Ltd GA8-TC320 airplanes,
all serial numbers up to and including GA8-TC 320-14-205,
certificated in any category.
Exact source excerpt. Text positions 9270–9446, end exclusive, in the original decoded publication. SHA-256: 3f1ef5d001abaf4620c88c1d880d32fef1c3ed61bcf5dad9c962b7e8b6757e99
Subject
(d) Subject
Air Transport Association of America (ATA) Code 71: Power Plant.
Exact source excerpt. Text positions 9446–9529, end exclusive, in the original decoded publication. SHA-256: 663fcf04f03d27f6d7df5dbdd8ab3a372c2dabbdd72506c9e6318d2be1d1cefa
Reason
(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 missing required
engine mount fire seal washers, which could reduce the engine
retention capability in the event of a fire. We are issuing this AD
to revise the applicable airplane serial numbers and to detect and
correct the omission of steel washers at each isolator mount
location, which, if not corrected, could result in reduced engine
retention capability in the event of a fire.
Exact source excerpt. Text positions 9529–10185, end exclusive, in the original decoded publication. SHA-256: e6fea66fd7c353164f6534252a1522a51d08a4af1d6d19254bc2f8ad4ac19d06
Actions and Compliance
(f) Actions and Compliance
Unless already done, comply with this AD within the compliance
times specified in paragraphs (f)(1) through (f)(3) of this AD:
(1) Within the next 300 hours time-in-service after April 24,
2015 (the effective date retained from AD 2015-22-14) or within the
next 12 months after April 24, 2015 (the effective date retained
from AD 2015-22-14), whichever occurs first, inspect the orientation
of the engine isolator mounts to verify that the mounts have been
installed properly following the Accomplishment Instructions in
GippsAero Mandatory Service Bulletin SB-GA8-2014-115, Issue 1, dated
October 6, 2014.
(2) Before reinstalling the engine isolator mounts following the
inspection required in paragraph (f)(1) of this AD, before further
flight, install a part number J-2218-61 steel washer on the forward
side of each of the four engine isolator mounts, following the
Accomplishment Instructions in GippsAero Mandatory Service Bulletin
SB-GA8-2014-115, Issue 1, dated October 6, 2014.
(3) If during the inspection required in paragraph (f)(1) of
this AD, any of the engine isolator mounts are found to not comply
with the specifications found in the Accomplishment Instructions of
GippsAero Mandatory Service Bulletin SB-GA8-2014-115, Issue 1, dated
October 6, 2014, before further flight, re-install the isolators to
the correct orientation, or if damage is found, replace with
airworthy parts.
Exact source excerpt. Text positions 10185–11647, end exclusive, in the original decoded publication. SHA-256: 835e674363c23b9710e3773be29b6b7f21025a5b1a7767aa718ed1dc95a1a8d1
Other FAA AD Provisions
(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: Doug Rudolph, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email:
[email protected]. 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.
Exact source excerpt. Text positions 11647–12746, end exclusive, in the original decoded publication. SHA-256: d063ef0f27939364dc0b5c4159813f77def93ae1f5dbd41b25246048278f74a5
Related Information
(h) Related Information
Refer to MCAI Civil Aviation Safety Authority (CASA) AD No. AD/
GA8/8, Amdt 1, dated March 26, 2015. The MCAI can be found in the AD
docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-1123-0007.
Exact source excerpt. Text positions 12746–13003, end exclusive, in the original decoded publication. SHA-256: 68fa341e4b2368e7153a60f0543a420f1fd0005990ace598bce18cf200a66229
Material Incorporated by Reference
(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.
(3) The following service information was approved for IBR on
April 24, 2015 (80 FR 14810, March 20, 2015).
(i) GippsAero Mandatory Service Bulletin SB-GA8-2014-115, Issue
1, dated October 6, 2014.
(ii) Reserved.
(4) For GippsAero service information identified in this AD,
contact GA 8 Airvan (Pty) Ltd, c/o GippsAero Pty Ltd, Attn:
Technical Services, P.O. Box 881, Morwell Victoria 3840, Australia;
telephone: + 61 03 5172 1200; fax: +61 03 5172 1201; email:
[email protected]; Internet: http://www.gippsaero.com/customer-support/technical-publications.aspx.
(5) 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. In addition, you can access this service information
on the Internet at http://www.regulations.gov by searching for and
locating Docket No. FAA-2014-1123.
(6) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://
[[Page 42012]]
www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 13003–14639, end exclusive, in the original decoded publication. SHA-256: 5ba5c2c970ea363ee5eba4c7b7f8cd75c7e014be4c44bc1b310f43df2970e023
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 2015-06-02 R1 · 1 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: c8c2a6421e73694e4050d65abc107673fe92e4c0ea494c6dfabab6c45a616d6e. Source manifest: 78a5917d4e7023556cc117c5f407d1263161a559f9b672f7fc4e81ea134dc5cb.
Official source · 2015-07-16
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 80, Number 136 (Thursday, July 16, 2015)]
[Rules and Regulations]
[Pages 42010-42012]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-17193]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-1123; Directorate Identifier 2014-CE-037-AD;
Amendment
[39-18209; AD 2015-06-02 R1]
RIN 2120-AA64
Airworthiness Directives; GA 8 Airvan (Pty) Ltd Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are revising an airworthiness directive (AD) 2015-06-02 for
GA 8 Airvan (Pty) Ltd Model GA8-TC320 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 missing required engine mount fire seal washers, which
could reduce the engine retention capability in the event of a fire. We
are issuing this AD to require actions to address the unsafe condition
on these products.
DATES: This AD is effective August 20, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of April
24, 2015 (80 FR 14810, March 20, 2015).
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
1123; or in person at the Docket Management Facility, U.S. Department
of Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
For service information identified in this AD, contact GA 8 Airvan
(Pty) Ltd, c/o GippsAero Pty Ltd, Attn: Technical Services, P.O. Box
881, Morwell Victoria 3840, Australia; telephone: + 61 03 5172 1200;
fax: +61 03 5172 1201; email: [email protected]; Internet: http://www.gippsaero.com/customer-support/technical-publications.aspx. 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.
It is also available on the Internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2014-1123.
FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email:
[email protected].
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 GA 8 Airvan (Pty) Ltd Model
GA8-TC320 airplanes. The NPRM was published in the Federal Register on
April 17, 2015 (74 FR 21193), and proposed to revise AD 2015-06-02,
Amendment 39-18120 (80 FR 14810; March 20, 2015).
The NPRM proposed to correct an unsafe condition for the specified
products and was based on mandatory continuing airworthiness
information originated by an airworthiness authority of another
country. The MCAI states that:
A recent review of the engine mount installation on the GA8-TC
320 aircraft has highlighted the omission of engine mount fire seal
washers during the assembly process.
The current engine mount configuration does not meet the
certification basis for the aircraft, specifically regulation 23.865
of the Federal Aviation Regulations of the United States of America,
where engine mounts located in designated fire zones are required to
be suitably shielded so that they are capable of withstanding the
effects of a fire.
The Gippsland Aeronautics GA8-TC 320 aircraft require the
installation of an approved steel washer at each of the engine mount
locations to address a potential risk of reduced engine retention
capability in the event of a fire.
This AD, AD/GA8/8 Amdt 1, amends the applicability statement to
be inclusive of the affected aircraft serial number range.
The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-1123-0007.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (74 FR 21193, April 17,
2015) 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:
<bullet> Are consistent with the intent that was proposed in the
NPRM (74 FR 21193, April 17, 2015) for correcting the unsafe condition;
and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (74 FR 21193, April 17, 2015).
Relative Service Information Under 1 CFR Part 51
We reviewed GippsAero Mandatory Service Bulletin SB-GA8-2014-115,
Issue 1, dated October 6, 2014. The service bulletin describes
procedures for inspecting the orientation of the engine isolator mounts
to verify proper installation, re-installing if necessary, and
installing steel washers on the forward side of each side of the engine
isolator mounts. This service information is reasonably available
because the interested parties have access to it through their normal
course of business or by the means identified in the ADDRESSES section
of this AD.
Costs of Compliance
We estimate that this AD will affect 13 products of U.S. registry.
We also estimate that it would take about 5 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 $10 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
[[Page 42011]]
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 http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
1123; 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 removing Amendment 39-18120 (80 FR
14810, March 20, 2015), and adding the following new AD:
2015-06-02 R1 GA 8 Airvan (Pty) Ltd: Amendment 39-18209; Docket No.
FAA-2014-1123; Directorate Identifier 2014-CE-037-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective August 20,
2015.
(b) Affected ADs
This AD revises AD 2015-06-02, Amendment 39-18120 (80 FR 14810;
March 20, 2015).
(c) Applicability
This AD applies to GA 8 Airvan (Pty) Ltd GA8-TC320 airplanes,
all serial numbers up to and including GA8-TC 320-14-205,
certificated in any category.
(d) Subject
Air Transport Association of America (ATA) Code 71: Power Plant.
(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 missing required
engine mount fire seal washers, which could reduce the engine
retention capability in the event of a fire. We are issuing this AD
to revise the applicable airplane serial numbers and to detect and
correct the omission of steel washers at each isolator mount
location, which, if not corrected, could result in reduced engine
retention capability in the event of a fire.
(f) Actions and Compliance
Unless already done, comply with this AD within the compliance
times specified in paragraphs (f)(1) through (f)(3) of this AD:
(1) Within the next 300 hours time-in-service after April 24,
2015 (the effective date retained from AD 2015-22-14) or within the
next 12 months after April 24, 2015 (the effective date retained
from AD 2015-22-14), whichever occurs first, inspect the orientation
of the engine isolator mounts to verify that the mounts have been
installed properly following the Accomplishment Instructions in
GippsAero Mandatory Service Bulletin SB-GA8-2014-115, Issue 1, dated
October 6, 2014.
(2) Before reinstalling the engine isolator mounts following the
inspection required in paragraph (f)(1) of this AD, before further
flight, install a part number J-2218-61 steel washer on the forward
side of each of the four engine isolator mounts, following the
Accomplishment Instructions in GippsAero Mandatory Service Bulletin
SB-GA8-2014-115, Issue 1, dated October 6, 2014.
(3) If during the inspection required in paragraph (f)(1) of
this AD, any of the engine isolator mounts are found to not comply
with the specifications found in the Accomplishment Instructions of
GippsAero Mandatory Service Bulletin SB-GA8-2014-115, Issue 1, dated
October 6, 2014, before further flight, re-install the isolators to
the correct orientation, or if damage is found, replace with
airworthy parts.
(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: Doug Rudolph, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email:
[email protected]. 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 Safety Authority (CASA) AD No. AD/
GA8/8, Amdt 1, dated March 26, 2015. The MCAI can be found in the AD
docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-1123-0007.
(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.
(3) The following service information was approved for IBR on
April 24, 2015 (80 FR 14810, March 20, 2015).
(i) GippsAero Mandatory Service Bulletin SB-GA8-2014-115, Issue
1, dated October 6, 2014.
(ii) Reserved.
(4) For GippsAero service information identified in this AD,
contact GA 8 Airvan (Pty) Ltd, c/o GippsAero Pty Ltd, Attn:
Technical Services, P.O. Box 881, Morwell Victoria 3840, Australia;
telephone: + 61 03 5172 1200; fax: +61 03 5172 1201; email:
[email protected]; Internet: http://www.gippsaero.com/customer-support/technical-publications.aspx.
(5) 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. In addition, you can access this service information
on the Internet at http://www.regulations.gov by searching for and
locating Docket No. FAA-2014-1123.
(6) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://
[[Page 42012]]
www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on July 7, 2015.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2015-17193 Filed 7-15-15; 8:45 am]
BILLING CODE 4910-13-P
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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.
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