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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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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:33:15.362139+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
5bcfeef022632107ba69790bfedd96a791e843958434254a61c20ebe14391d20
Text SHA-256
c8c2a6421e73694e4050d65abc107673fe92e4c0ea494c6dfabab6c45a616d6e

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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.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.