Published 2018-03-19 · Federal Register document 2018-05355
Airworthiness Directives; Pacific Aerospace Limited Airplanes
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:58.123663+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2018-258c65fa72d503e0
- Source row
- results[88]
- Raw source SHA-256
- 258c65fa72d503e0b0dfb928a28beb1793ddc7dd9218bce0413e53dfe11d78fb
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2018-06-09
- Effective date printed in this edition
- 2018-04-09
Read 9 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) becomes effective April 9,
2018.
Exact source excerpt. Text positions 10359–10452, end exclusive, in the original decoded publication. SHA-256: f2e43c228c57d9b28e91e734976a3a1885290ae3dc06f8c4c7a5f0a57176b3ba
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10452–10481, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(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.
Exact source excerpt. Text positions 10481–10666, end exclusive, in the original decoded publication. SHA-256: ad576fd6fd267cbe0dfc8490e1c5d93359ca3755e4c2fed685f6ada73ff54313
Subject
(d) Subject
Air Transport Association of America (ATA) Code 27: Flight
Controls.
Exact source excerpt. Text positions 10666–10754, end exclusive, in the original decoded publication. SHA-256: cff97c7a02aad764608e75ad6e1339103f6eb6475cfd8403dd9a5a86a6d2c6e2
Reason
(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.
[[Page 11875]]
Exact source excerpt. Text positions 10754–11295, end exclusive, in the original decoded publication. SHA-256: 08d3050a8d5c529d9509e6b32e17af1098e1650781007173a14d35b891d411b2
Actions and Compliance
(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.
Exact source excerpt. Text positions 11295–11993, end exclusive, in the original decoded publication. SHA-256: ee8efcc1d86b36f9bab2736bb2d47742e4f6a1a880d92773ec0466bab713ab4f
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,
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 information 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: [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) 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).
Exact source excerpt. Text positions 11993–12992, end exclusive, in the original decoded publication. SHA-256: fdd4391de0d7131e28e8f4ed8c3f47ffb40ed1974bf5bd6ad3ac85061bc23c1e
Related Information
(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.
Exact source excerpt. Text positions 12992–13347, end exclusive, in the original decoded publication. SHA-256: 8c7d211e2f6c2e15d49fbe92998b0ca13c1264b6e2fed77e878a0c266d9fea2c
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.
(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 Aerospace Limited, Airport Road, Hamilton, Private Bag 3027,
Hamilton 3240, New Zealand; phone: +64 7843 6144; fax: +64 843 6134;
email: [email protected]; 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.
Exact source excerpt. Text positions 13347–14730, end exclusive, in the original decoded publication. SHA-256: 7bd7f48445001d460b06323e84d0a40424bf4cfafd90ae8cab4bbd9aeb954a15
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 2018-06-09 · 0 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: 9e6189a2227bb0e52f62b4d74e1f01b6e1636cee7236f3d217fb5d6e7db17a31. Source manifest: 880ec17cf6a8073e9f1f1040af1e94927a32415008779f953c0e145ab40d38dc.
Official source · 2018-03-19
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 83, Number 53 (Monday, March 19, 2018)]
[Rules and Regulations]
[Pages 11873-11875]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-05355]
-----------------------------------------------------------------------
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:
<bullet> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
<bullet> Fax: (202) 493-2251.
<bullet> 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.
<bullet> 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:
[email protected]; 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:
[email protected].
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
[[Page 11874]]
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
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 adding the following new AD:
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.
[[Page 11875]]
(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 information 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: [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) 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 Aerospace Limited, Airport Road, Hamilton, Private Bag 3027,
Hamilton 3240, New Zealand; phone: +64 7843 6144; fax: +64 843 6134;
email: [email protected]; 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.
[FR Doc. 2018-05355 Filed 3-16-18; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
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- Text SHA-256
- 9e6189a2227bb0e52f62b4d74e1f01b6e1636cee7236f3d217fb5d6e7db17a31
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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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