[Federal Register Volume 81, Number 110 (Wednesday, June 8, 2016)]
[Proposed Rules]
[Pages 36810-36813]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-13249]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-7003; Directorate Identifier 2016-CE-015-AD]
RIN 2120-AA64
Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to adopt a new airworthiness directive (AD) for all
PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, PC-12/47, and PC-12/47E
airplanes that would supersede AD 2014-22-01. This proposed AD results
from 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 a need to incorporate new revisions into the Limitations
section, Chapter 4, of the FAA-approved maintenance program (e.g.,
maintenance manual). We are issuing this proposed AD to require actions
to address the unsafe condition on these products.
DATES: We must receive comments on this proposed AD by July 25, 2016.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room
[[Page 36811]]
W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this proposed AD, contact
PILATUS AIRCRAFT LTD., Customer Service Manager, CH-6371 STANS,
Switzerland; telephone: +41 (0) 41 619 33 33; fax: +41 (0) 41 619 73
11; Internet: http://www.pilatus-aircraft.com or email:
aircraft.com">SupportPC12@pilatus-aircraft.com 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 by searching for and locating Docket No. FAA-2016-
7003; 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 proposed AD, 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.
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:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2016-7003;
Directorate Identifier 2016-CE-015-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
We will post all comments we receive, without change, to http://regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.
Discussion
On October 20, 2014, we issued AD 2014-22-01, Amendment 39-18005
(79 FR 67343, November 13, 2014) (``AD 2014-22-01''). That AD required
actions intended to address an unsafe condition on all PILATUS AIRCRAFT
LTD. Models PC-12, PC-12/45, PC-12/47, and PC-12/47E airplanes and was
based on mandatory continuing airworthiness information (MCAI)
originated by an aviation authority of another country.
Since we issued AD 2014-22-01, PILATUS AIRCRAFT LTD. has issued
revisions to the Limitations section of the airplane maintenance manual
to include repetitive inspections of the main landing gear (MLG)
attachment bolts.
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued AD
No. 2016-0083, dated April 28, 2016 (referred to after this as ``the
MCAI''), to correct an unsafe condition for the specified products. The
MCAI states:
The airworthiness limitations are currently defined and
published in the Pilatus PC-12 Aircraft Maintenance Manual(s) (AMM)
under Chapter 4, Structural, Component and Miscellaneous--
Airworthiness Limitations Section (ALS) documents. The limitations
contained in these documents have been identified as mandatory for
continued airworthiness.
Failure to comply with these instructions could result in an
unsafe condition.
EASA issued AD 2014-0170 requiring the actions as specified in
ALS, Chapter 4 of AMM report 02049 issue 28, for PC-12, PC-12/45 and
PC-12/47 aeroplanes, and Chapter 4 of AMM report 02300 issue 11, for
PC-12/47E aeroplanes.
Since that AD was issued, Pilatus issued Chapter 4 of PC-12 AMM
report 02049 issue 31, and Chapter 4 of PC-12 AMM report 02300 issue
14 (hereafter collectively referred to as `the applicable ALS' in
this AD), to incorporate new six-year and ten-year inspection
intervals for several main landing gear (MLG) attachment bolts, and
an annual inspection interval for the MLG shock absorber attachment
bolts, which was previously included in the AMM Chapter 5 annual
inspection. After a further review of the in-service data, Pilatus
issued Service Letter (SL) 186, extending the special compliance
time applicable for the MLG bolts inspection.
For the reasons described above, this AD retains the
requirements of EASA AD 2014-0170, which is superseded, and requires
the accomplishment of the new maintenance tasks, as described in the
applicable ALS.
You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
7003.
Related Service Information Under 1 CFR Part 51
PILATUS AIRCRAFT LTD. has issued Structural, Component and
Miscellaneous--Airworthiness Limitations, document 12-A-04-00-00-00A-
000A-A, dated September 28, 2015, and Structural and Component
Limitations--Airworthiness Limitations, document 12-B-04-00-00-00A-
000A-A, dated September 28, 2015. 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 NPRM.
FAA's Determination and Requirements of the Proposed AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are proposing this AD because
we evaluated all information and determined the unsafe condition exists
and is likely to exist or develop on other products of the same type
design.
Costs of Compliance
We estimate that this AD will affect 770 products of U.S. registry.
We also estimate that it would take about 1.5 work-hours per product to
comply with the basic requirements of this proposed AD. The average
labor rate is $85 per work-hour. Based on these figures, we estimate
the cost of this proposed AD on U.S. operators to be $98,175, or
$127.50 per product. This breaks down as follows:
Incorporating new revisions into the Limitations section,
Chapter 4, of the FAA-approved maintenance program (e.g., maintenance
manual): .5 work-hour for a fleet cost of $32,725, or $42.50 per
product.
New inspections: MLG attachment bolts: 1 work-hour with no
parts cost for fleet cost of $65,450 or $85 per product.
In addition, we estimate that any necessary corrective actions (on-
condition costs) that must be taken based on the proposed inspections,
would take about 1 work-hour and require parts costing approximately
$100 for a cost of $185 per product. We have no way of determining the
number of products that may need these necessary corrective actions.
This breaks down as follows:
The only costs that would be imposed by this proposed AD over that
already
[[Page 36812]]
required by AD 2014-22-01 is insertion of the revised Limitation
section and the MLG attachment bolts inspection and replacement as
necessary.
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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 proposed
regulation:
(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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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 39-18005 (79 FR
67343, November 13, 2014), and adding the following new AD:
PILATUS AIRCRAFT LTD.: Docket No. FAA-2016-7003; Directorate
Identifier 2016-CE-015-AD.
(a) Comments Due Date
We must receive comments by July 25, 2016.
(b) Affected ADs
This AD replaces AD 2014-22-01, 39-18005 (79 FR 67343, November
13, 2014).
(c) Applicability
This AD applies to PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45,
PC-12/47, and PC-12/47E airplanes, all manufacturer serial numbers
(MSNs), certificated in any category.
(d) Subject
Air Transport Association of America (ATA) Code 5: Time Limits.
(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 a need to
incorporate new revisions into the Limitations section, Chapter 4,
of the FAA-approved maintenance program (e.g., maintenance manual).
The limitations were revised to include repetitive inspections of
the main landing gear (MLG) attachment bolts. These actions are
required to ensure the continued operational safety of the affected
airplanes.
(f) Actions and Compliance
Unless already done, do the actions in paragraphs (f)(1) through
(f)(6) of this AD:
(1) Before further flight after July 13, 2016 (the effective
date of this AD), insert the following revisions into the
Limitations section of the FAA-approved maintenance program (e.g.,
maintenance manual):
(i) STRUCTURAL, COMPONENT AND MISCELLANEOUS--AIRWORTHINESS
LIMITATIONS, Data module code 12-A-04-00-00-00A-000A-A, dated
September 28, 2015, of the Pilatus Model type--PC-12, PC-12/45, PC-
12/47, Aircraft Maintenance Manual (AMM), Document No. 02049, 12-A-
AM-00-00-00-I, revision 31, dated November 10, 2015; and
(ii) STRUCTURAL AND COMPONENT LIMITATIONS--AIRWORTHINESS
LIMITATIONS, Data module code 12-B-04-00-00-00A-000A-A, dated
September 28, 2015, of the Pilatus Model type--PC-12/47E MSN-1001-
UP, Aircraft Maintenance Manual (AMM), Document No. 02300, 12-B-AM-
00-00-00-I, revision 14, dated November 6, 2015.
(2) The limitations section revisions listed in paragraphs
(f)(1)(i) and (f)(1)(ii) of this AD do the following:
(i) Establish inspections of the MLG attachment bolts,
(ii) Specify replacement of components before or upon reaching
the applicable life limit, and
(iii) Specify accomplishment of all applicable maintenance tasks
within certain thresholds and intervals.
(3) Only authorized Pilatus Service Centers can do the
Supplemental Structural Inspection Document (SSID) as required by
the documents in paragraphs (f)(1)(i) and (f)(1)(ii) of this AD
because deviations from the type design in critical locations could
make the airplane ineligible for this life extension.
(4) If no compliance time is specified in the documents listed
in paragraphs (f)(1)(i) and (f)(1)(ii) of this AD when doing any
corrective actions where discrepancies are found as required in
paragraph (f)(2)(iii) of this AD, do these corrective actions before
further flight after doing the applicable maintenance task.
(5) During the accomplishment of the actions required in
paragraph (f)(2) of this AD, including all subparagraphs, if a
discrepancy is found that is not identified in the documents listed
in paragraphs (f)(1)(i) and (f)(1)(ii) of this AD, before further
flight after finding the discrepancy, contact PILATUS AIRCRAFT LTD.
at the address specified in paragraph (h) of this AD for a repair
scheme and incorporate that repair scheme.
(6) Within the next 6 years time-in-service after July 13, 2016
(the effective date of this AD) or within the next 3 months TIS
after July 13, 2016 (the effective date of this AD), whichever
occurs later, inspect the MLG attachment bolts for cracks and
corrosion take all necessary corrective actions.
(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].
(i) 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.
(ii) AMOCs approved for AD 2014-22-01, 39-18005 (79 FR 67343,
November 13, 2014) are not approved as AMOCs for this AD.
(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
[[Page 36813]]
(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.
2016-0083, dated April 28, 2016, for related information. You may
examine the MCAI on the Internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2016-7003. For service
information related to this AD, contact PILATUS AIRCRAFT LTD.,
Customer Service Manager, CH-6371 STANS, Switzerland; telephone: +41
(0) 41 619 33 33; fax: +41 (0) 41 619 73 11; Internet: http://
www.pilatus-aircraft.com or email: aircraft.com">SupportPC12@pilatus-aircraft.com.
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.
Issued in Kansas City, Missouri, on May 27, 2016.
Melvin Johnson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-13249 Filed 6-7-16; 8:45 am]
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