[Federal Register Volume 81, Number 131 (Friday, July 8, 2016)]
[Rules and Regulations]
[Pages 44492-44494]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-15864]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-5578; Directorate Identifier 2016-CE-005-AD;
Amendment 39-18587; AD 2016-14-06]
RIN 2120-AA64
Airworthiness Directives; Pacific Aerospace Limited Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are superseding Airworthiness Directive (AD) 2006-13-05 for
certain Pacific Aerospace Limited Model 750XL (type certificate
previously held by Pacific Aerospace Corporation Ltd.) 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 some critical rivets on the wing not being
fully age-hardened and being installed in specific locations where
reduction in rivet strength reduces wing strength. We are issuing this
AD to require actions to address the unsafe condition on these
products.
DATES: This AD is effective August 12, 2016.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of August 12,
2016.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of July
31, 2006 (71 FR 35509, June 21, 2006).
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
5578; 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 Pacific
Aerospace Limited, Airport Road, Hamilton, Private Bag 3027, Hamilton
3240, New Zealand; telephone: +64 7 843 6144; facsimile: +64 7 843
6134; email: [email protected]; Internet: www.aerospace.co.nz.
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 Docket No. FAA-2016-5578.
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4123; fax: (816) 329-4090; email:
[email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Pacific Aerospace
Limited Model 750XL (type certificate previously held by Pacific
Aerospace Corporation Ltd.) airplanes. That NPRM was published in the
Federal Register on April 12, 2016 (81 FR 21489), and proposed to
supersede AD 2006-13-05, Amendment 39-14658 (71 FR 35509, June 21,
2006) (``AD 2006-13-05'').
Since we issued AD 2006-13-05, additional airplanes have been
identified that need to be added to the applicability of the AD.
The Civil Aviation Authority (CAA), which is the aviation authority
for New Zealand, has issued AD No. DCA/750XL/7B, dated February 25,
2016 (referred to after this as ``the MCAI''), to correct an unsafe
condition for the specified products. The MCAI states:
DCA/750XL/7B revised to introduce PACSB/XL/018 issue 4, dated 20
January 2016, which reduces the applicability to S/N 101 through to
131 with no change to the requirements. Aircraft with S/N 132
onwards have been modified in accordance with PACSB/XL/018 at
manufacture, which is a terminating action for the requirements of
this AD.
This AD requires you to remove rivets that have not been fully age
hardened and replace them with bolts, washers, and nuts in specific
locations where reduction in rivet strength affects overall structural
capability. The AD retains the airplane weight AFM limitations until
the rivets are replaced with the bolts, washers, and nuts. You may
examine the MCAI on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2016-5578-002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (81 FR 21489, April 12,
2016) 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:
Are consistent with the intent that was proposed in the
NPRM (81 FR 21489, April 12, 2016) for correcting the unsafe condition;
and
Do not add any additional burden upon the public than was
already proposed in the NPRM (81 FR 21489, April 12, 2016).
[[Page 44493]]
Related Service Information
We reviewed Pacific Aerospace Limited Service Bulletin PACSB/XL/
018, Issue 4, dated January 20, 2016. The service bulletin describes
procedures for removing rivets (part number (P/N) MS20470 DD6) and
installing bolts (P/N NAS 6203-7X or NAS 6203-6X), washers (P/N AN960-
10), and nuts (P/N MS21044N3) in place of the rivets to restore
airplane to full take-off weight of 7,500 pounds. 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 the AD.
Costs of Compliance
We estimate that this AD will affect 9 products of U.S. registry.
We also estimate that it will take about 32 work-hours per product to
comply with the replacement requirements of this AD. The average labor
rate is $85 per work-hour. Required parts will cost about $519 per
product.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $29,151, or $3,239 per product.
AD 2006-13-05 affected 8 of the 9 U.S.-registered airplanes
reflected in the above cost information. This AD will only increase the
cost already required by AD 2006-13-05 by one additional airplane. The
FAA has a report that the additional airplane is already in compliance,
thus this AD will impose no additional cost impact on U.S. operators.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation in Alaska, and
(4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
5578; 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 39-14658 (71 FR
35509, June 21, 2006), and adding the following new AD:
2016-14-06 Pacific Aerospace Limited: Amendment 39-18587; Docket No.
FAA-2016-5578; Directorate Identifier 2016-CE-005-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective August 12,
2016.
(b) Affected ADs
This AD replaces AD 2006-13-05, Amendment 39-14658 (71 FR 35509,
June 21, 2006) (``AD 2006-13-05'').
(c) Applicability
This AD applies to the following Pacific Aerospace Limited Model
750XL airplanes (type certificate previously held by Pacific
Aerospace Corporation Ltd.), that are certificated in any category.
(1) Airplanes previously affected by AD 2006-13-05: Serial
numbers 101, 102, 104 through 120, and 125.
(2) Airplanes new to this AD: Serial numbers 103, 121, 122, 123,
124, and 126 to 131.
(d) Subject
Air Transport Association of America (ATA) Code 57: Wings.
(e) Reason
This 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 some critical
rivets on the wing not being fully age-hardened and being installed
in specific locations where reduction in rivet strength reduces wing
strength. We are issuing this AD to add airplane serial numbers to
the Applicability section, paragraph (c) of this AD, and to ensure
wing ultimate load requirements are met. If wing ultimate load
requirements are not met, wing failure could result with consequent
loss of control.
(f) Actions and Compliance
Unless already done, do the following actions:
(1) Insert the following information into the Limitations
section of the airplane flight manual (AFM) at the compliance time
specified in paragraphs (f)(1)(i) and (ii) of this AD. You may do
this by inserting a copy of this AD into the Limitations section of
the AFM: ``The maximum takeoff weight is reduced from 7,500 pounds
to 7,125 pounds.'' The owner/operator holding at least a private
pilot certificate as authorized by section 43.7 of the Federal
Aviation Regulations (14 CFR 43.7) may do the flight manual changes
requirement of this AD. Make an entry in the aircraft records
showing compliance with this portion of the AD following section
43.9 of the Federal Aviation Regulations (14 CFR 43.9).
(i) For airplanes previously affected by AD 2006-13-05: Before
further flight after January 16, 2006 (the effective date retained
from AD 2005-26-53, Amendment 39-14451 (71 FR 2453, January 17,
2006), which was replaced by AD 2006-13-05).
(ii) For airplanes new to this AD: Before further flight after
August 12, 2016 (the effective date of this AD).
(2) Remove rivets, part number (P/N) MS20470 DD6, on the main
spar web and
[[Page 44494]]
replace with bolts, P/N NAS 6203-6X or -7X, as indicated for the
position, assembled with washers, P/N AN960-10, and nut, P/N
MS21044N3, at the compliance time specified in paragraphs (f)(2)(i)
and (ii) of this AD.
(i) For airplanes previously affected by AD 2006-13-05: Within
the next 100 hours time-in-service (TIS) after July 31, 2006 (the
effective date retained from AD 2006-13-05). Do the removal and
replacement actions following Pacific Aerospace Corporation Ltd.
Service Bulletin PACSB/XL/018, Issue 3, dated December 23, 2005, and
amended January 16, 2006.
(ii) For airplanes new to this AD: Within the next 100 hours TIS
after August 12, 2016 (the effective date of this AD) or within the
next 12 months after August 12, 2016 (the effective date of this
AD), whichever occurs first. Do the removal and replacement actions
following Pacific Aerospace Limited Service Bulletin PACSB/XL/018,
Issue 4, dated January 20, 2016.
(3) For all affected airplanes: Before further flight after
doing the action required in paragraph (f)(2) of this AD, remove the
restrictive information from the Limitations section of the AFM that
you were required to insert in paragraph (f)(1) of this AD. The
owner/operator holding at least a private pilot certificate as
authorized by section 43.7 of the Federal Aviation Regulations (14
CFR 43.7) may do the flight manual changes requirement of this AD.
(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: Karl Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4123; 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 Authority (CAA) AD No. DCA/750XL/
7B, dated February 25, 2016, for related information. You may
examine the MCAI on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2016-5578-002.
(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
August 12, 2016.
(i) Pacific Aerospace Limited Service Bulletin PACSB/XL/018,
Issue 4, dated January 20, 2016.
(ii) Reserved.
(4) The following service information was approved for IBR on
July 31, 2006 (71 FR 35509, June 21, 2006).
(i) Pacific Aerospace Corporation Ltd. Service Bulletin PACSB/
XL/018, Issue 3, dated December 23, 2005, and amended January 16,
2006.
(ii) Reserved.
(5) For Pacific Aerospace Limited service information identified
in this AD, contact Pacific Aerospace Limited, Airport Road,
Hamilton, Private Bag 3027, Hamilton 3240, New Zealand; telephone:
+64 7 843 6144; facsimile: +64 7 843 6134; email:
[email protected]; Internet: www.aerospace.co.nz.
(6) You may view this service information at 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-2016-5578.
(7) 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 June 28, 2016.
Pat Mullen,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-15864 Filed 7-7-16; 8:45 am]
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