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2018-06-09 PACIFIC AEROSPACE LIMITED:
Amendment 39-19229; Docket No. FAA-2018-0210; Directorate Identifier 2018-CE-004-AD.

(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective April 9, 2018.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies  to  Pacific Aerospace Limited Models 750XL airplanes,
    all  serial  numbers  up   to  and  including  serial   number  XL215,
    certificated in any category.

(d) SUBJECT

    Air Transport Association of America (ATA) Code 27: Flight Controls.

(e) REASON

    This AD was prompted by mandatory continuing airworthiness information
    (MCAI) issued by the aviation authority of another country to identify
    and  correct an  unsafe condition  on an  aviation product.  The  MCAI
    describes  the unsafe  condition as  the possibility  for the  control
    column to snag on the cockpit control tee handles on certain aircraft.
    We  are  issuing this  AD  to prevent  the  control tee  handles  from
    snagging the control column and becoming jammed, which could result in
    uncontrollable flight.

(f) ACTIONS AND COMPLIANCE

    Unless already  done, do  the actions  in paragraph  (f)(1) and (2) of
    this AD following the Accomplishment Instructions in Pacific Aerospace
    Mandatory Service Bulletin PACSB/XL/093,  Issue 1,  dated December 15,
    2017.

(1) Within 30 days  after  April 9, 2018  (the effective date of this AD),
    inspect  the  ventilation,  heater,  and air filter bypass control tee
    handles (as applicable) for snagging of the control column.

(2) If the control column snags the adjacent heater,  ventilation,  or  an
    engine  air filter  bypass control  tee handle  during the  inspection
    required  in  paragraph  (f)(1) of  this  AD,  before further  flight,
    reorient the affected tee handle.

(g) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, Small Airplane
    Standards Branch, FAA, has the authority to approve AMOCs for this AD,
    if requested using the procedures found in 14 CFR 39.19. Send informa-
    tion to ATTN: Mike Kiesov,  Aerospace Engineer,  FAA,  Small  Airplane
    Standards Branch,  901 Locust,  Room 301, Kansas City, Missouri 64106;
    telephone: (816) 329-4144; fax: (816) 329-4090; email: mike.kiesov@faa
    .gov. 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) Contacting the Manufacturer:  For any requirement in this AD to obtain
    corrective  actions   from  a   manufacturer,  the   action  must   be
    accomplished using a method approved by the Manager, Standards Office,
    FAA; or the Civil Aviation Authority of New Zealand (CAA).

(h) RELATED INFORMATION

    Refer to the MCAI by the CAA, AD DCA/750XL/23, dated December 28, 2017
    and Pacific Aerospace Mandatory Service Bulletin PACSB/XL/093, Issue 1
    dated December 15, 2017, for related information.  You may examine the
    MCAI on the internet  at  http://www.regulations.gov  by searching for
    and locating Docket No. FAA-2018-0210.

(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.

(i) Pacific Aerospace  Mandatory  Service Bulletin PACSB/XL/093,  Issue 1,
    dated December 15, 2017.

(ii) Reserved.

(3) For service information identified in this AD,  contact  Pacific Aero-
    space Limited, Airport Road, Hamilton, Private Bag 3027, Hamilton 3240
    New Zealand; phone: +64 7843 6144; fax: +64 843 6134;  email: pacific@
    aerospace.co.nz; internet: www.aerospace.co.nz.

(4) You may view this service information at the FAA Policy and Innovation
    Division, 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 locating Docket No. FAA-2018-0210.

(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 March 9, 2018.  Pat Mullen,  Acting
Deputy Director,  Policy  &  Innovation  Division,  Aircraft Certification
Service.

FOR FURTHER INFORMATION CONTACT:  Mike Kiesov,  Aerospace  Engineer,  FAA,
Small Airplane Standards Branch, 901 Locust, Rm 301, Kansas City, Missouri
64106; telephone: (816) 329-4144; fax: (816) 329-4090; email: mike.kiesov@
faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0210; Product Identifier 2018-CE-004-AD; Amendment
39-19229; AD 2018-06-09]
RIN 2120-AA64

Airworthiness Directives; Pacific Aerospace Limited Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for Pacific
Aerospace Limited Model 750XL airplanes. This AD results from mandatory
continuing airworthiness information (MCAI) issued by the aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as the possibility for the control column to snag on the
cockpit control tee handles on certain airplanes. We are issuing this
AD to require actions to address the unsafe condition on these
products.

DATES: This AD is effective April 9, 2018.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of April 9,
2018.
We must receive comments on this AD by May 3, 2018.

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 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 AD, contact Pacific
Aerospace Limited, Airport Road, Hamilton, Private Bag 3027, Hamilton
3240, New Zealand; phone: +64 7843 6144; fax: +64 843 6134; email:
pacific@aerospace.co.nz; internet: www.aerospace.co.nz. You may view
this referenced service information at the FAA, Policy and Innovation
Division, 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 locating Docket No. FAA-2018-0210.

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-2018-
0210; or in person at Docket Operations 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 street address for Docket Operations (telephone (800)
647-5527) is in the ADDRESSES section. Comments will be available in
the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Mike Kiesov, Aerospace Engineer, FAA,
Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; email:
mike.kiesov@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

The Civil Aviation Authority, which is the aviation authority for
New Zealand, has issued CAA AD DCA/750XL/22, dated December 19, 2017
(referred to after this as ``the MCAI''), to correct an unsafe
condition for Pacific Aerospace Limited Model 750XL airplanes. To
accompany that MCAI, the CAA issued Notification of Airworthiness
Directive issued for New Zealand Aeronautical Products IAW ICAO Annex
8, dated December 21, 2017; the Notification states:

This [CAA] AD is prompted by a ground inspection which found it
is possible for the control column to snag on the cockpit control
tee handles on certain aircraft. When the tee handle is pulled out
to the maximum limit it fouls with the control column in the extreme
forward right and left positions. The tee handles are mounted below
the switch panels adjacent to the centre console.
This [CAA] AD with effective date 28 December 2017 mandates the
inspection and corrective actions per the Accomplishment
Instructions in Pacific Aerospace Mandatory Service Bulletin (MSB)
PACSB/XL/093 issue 1, dated 15 December 2017, or later approved
revision.

You may examine the MCAI on the internet at http://www.regulations.gov
by searching for and locating Docket No. FAA-2018-0210.

Related Service Information Under 1 CFR Part 51

Pacific Aerospace Limited has issued Pacific Aerospace Mandatory
Service Bulletin PACSB/XL/093, Issue 1, dated December 15, 2017. The
service information describes procedures for inspecting the
ventilation, heater, and air filter bypass control tee handles for
snagging of the control column, and adjustment of the control tee
handle if necessary. 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.

FAA's Determination and Requirements of the 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 issuing this AD because we
evaluated all information provided by the State of Design Authority and
determined the unsafe condition exists and is likely to exist or
develop on other products of the same type design.

FAA's Determination of the Effective Date

An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice and comment prior to adoption of this rule because
interference with the control column operations can result in the
flight controls becoming jammed, which could result in uncontrollable
flight. Therefore, we find good cause that notice and opportunity for
prior public comment are impracticable. In addition, for the reason(s)
stated above, we find that good cause exists for making this amendment
effective in less than 30 days.

Comments Invited

This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2018-0210; Directorate
Identifier 2018-CE-004-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD because of
those comments.
We will post all comments we receive, without change, to http://www.
regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.

Costs of Compliance

We estimate that this AD will affect 22 products of U.S. registry.
We also estimate that it would take about 2 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour.
Based on these figures, we estimate the cost of the AD on U.S.
operators to be $3,740, or $170 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
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 that 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.

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


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]


2. The FAA amends Sec. 39.13 by adding the following new AD: