Airworthiness Directives; Pacific Aerospace Limited Airplanes, 48086-48088 [2021-18444]
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48086
Federal Register / Vol. 86, No. 164 / Friday, August 27, 2021 / Proposed Rules
following the Accomplishment Instructions,
Part A or Part AA, in ASI Aviation Service
Bulletin No. F406–104, Revision 1, dated
December 14, 2018.
(2) Within 100 hours TIS after the effective
date of this AD, and thereafter at intervals not
to exceed 2,400 hours TIS, do a magnetic
particle inspection for cracks of the LH and
RH rudder control pedal torque tubes by
following the Accomplishment Instructions,
Part B, in ASI Aviation Service Bulletin No.
F406–104, Revision 1, dated December 14,
2018.
(3) If, during any inspection required by
paragraph (h)(1) or (2) of this AD, any crack
is detected on a rudder control pedal torque
tube, you are not required to contact ASI
Aviation as specified in steps A.16, AA.5,
and B.4 of ASI Aviation Service Bulletin No.
F406–104, Revision 1, dated December 14,
2018. Instead, before further flight, replace
the rudder control pedal torque tube with a
serviceable part as defined by this AD.
(i) Installation Limitation
As of the effective date of this AD, do not
install a rudder control pedal torque tube P/
N 5115260–1 (LH) or P/N 5115260–2 (RH) on
any airplane unless it is a serviceable part as
defined by this AD.
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(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, International Validation
Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In
accordance with 14 CFR 39.19, send your
request to your principal inspector or local
Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the certification office,
send it to the attention of the person
identified in Related Information or email: 9AVS-AIR-730-AMOC@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(k) Related Information
(1) For more information about this AD,
contact Gregory Johnson, Aviation Safety
Engineer, FAA, General Aviation & Rotorcraft
Section, International Validation Branch, 901
Locust, Room 301, Kansas City, MO 64106;
phone: (720) 626–5462; fax: (816) 329–4090;
email: gregory.johnson@faa.gov.
(2) Refer to European Aviation Safety
Agency (EASA) AD 2019–0016, dated
January 29, 2019, for more information. You
may examine the EASA AD in the AD docket
at https://www.regulations.gov by searching
for and locating it in Docket No. FAA–2021–
0712.
(3) For service information identified in
this AD, contact ASI Aviation, Ae´rodrome de
Reims Prunay, 51360 Prunay, France;
telephone: +33 3 26 48 46 84; fax: +33 3 26
49 18 57; email: contact@asi-aviation.fr;
website: https://asi-aviation.fr/pageAccueil.html. You may view this service
information at the Airworthiness Products
Section, Operational Safety Branch, FAA,
901 Locust, Kansas City, MO 64106. For
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information on the availability of this
material at the FAA, call (816) 329–4148.
Issued on August 20, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–18384 Filed 8–26–21; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0711; Project
Identifier 2019–CE–024–AD]
RIN 2120–AA64
Airworthiness Directives; Pacific
Aerospace Limited Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Pacific Aerospace Limited
Model 750XL airplanes. This proposed
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 chafing of the
engine fuel feed line hoses. This
proposed AD would require inspecting
the engine fuel feed line hoses and the
electrical wiring and rerouting all fuel
lines. The FAA is proposing this AD to
address the unsafe condition on these
products.
SUMMARY:
The FAA must receive comments
on this proposed AD by October 12,
2021.
DATES:
You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
https://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: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For service information identified in
this NPRM, contact the Civil Aviation
ADDRESSES:
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Authority of New Zealand, Level 15,
Asteron Centre, 55 Featherston Street,
Wellington 6011; phone: + 64 4 560
9400; fax: + 64 4 569 2024; email: info@
caa.govt.nz. You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 901 Locust, Kansas City, MO
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 at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–0711; 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
NPRM, the MCAI, any comments
received, and other information. The
street address for Docket Operations is
listed above.
FOR FURTHER INFORMATION CONTACT:
Mike Kiesov, Aviation Safety Engineer,
General Aviation & Rotorcraft Section,
International Validation Branch, FAA,
901 Locust, Room 301, Kansas City, MO
64106; phone: (816) 329–4144; fax: (816)
329–4090; email: mike.kiesov@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2021–0711; Project Identifier
2019–CE–024–AD’’ at the beginning of
your comments. The most helpful
comments reference a specific portion of
the proposal, explain the reason for any
recommended change, and include
supporting data. The FAA will consider
all comments received by the closing
date and may amend this proposal
because of those comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
agency will also post a report
summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
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Federal Register / Vol. 86, No. 164 / Friday, August 27, 2021 / Proposed Rules
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Mike Kiesov, Aviation
Safety Engineer, General Aviation &
Rotorcraft Section, International
Validation Branch, FAA, 901 Locust,
Room 301, Kansas City, MO 64106. Any
commentary that the FAA receives
which is not specifically designated as
CBI will be placed in the public docket
for this rulemaking.
Background
The Civil Aviation Authority (CAA),
which is the aviation authority for New
Zealand, has issued AD No. DCA/
750XL/37, effective April 25, 2019
(referred to after this as ‘‘the MCAI’’), to
correct an unsafe condition for certain
Pacific Aerospace Limited Model 750XL
airplanes. The MCAI states:
FAA’s Determination
This product has been approved by
the aviation authority of another
country and is approved for operation in
the United States. Pursuant to the FAA’s
bilateral agreement with this State of
Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI and service information
referenced above. The FAA is issuing
this NPRM after determining the unsafe
condition described previously is likely
to exist or develop on other products of
the same type design.
Proposed AD Requirements in This
NPRM
This proposed AD would require
accomplishing the actions specified in
the service information described
previously, except as discussed under
‘‘Differences Between this Proposed AD
and the MCAI.’’
You may examine the MCAI in the
AD docket at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2021–
0711.
Differences Between This Proposed AD
and the MCAI
The MCAI requires an inspection at
the next 150 hour maintenance
inspection or within the next 50 hours
time-in-service (TIS), whichever occurs
later, while this proposed AD would
require those actions within 50 hours
TIS or at the next annual inspection
after the effective date of this AD,
whichever occurs later. If there is no
chafing and damage found during the
inspection, the MCAI requires certain
follow-on actions at the next 300 hour
maintenance inspection or within the
next 50 hours TIS, whichever is later.
This proposed AD would require those
actions within 50 hours TIS or at the
next annual inspection, whichever
occurs later, because there is no
regulatory requirement for operators in
the U.S. to have 150-hour or 300-hour
maintenance inspections.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Pacific Aerospace
Mandatory Service Bulletin PACSB/XL/
113, Issue 2, dated March 8, 2019. The
service information contains procedures
for inspecting the engine fuel feed line
hoses and the electrical wiring for
chafing or damage, rerouting all fuel
lines and the fuel transducer and
pressure switch wiring (including
installing P clips), and inspecting the
fuel hose for chafing and replacing
chafed fire sleeves or fuel hoses if
necessary. This service information is
reasonably available because the
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 23
airplanes of U.S. registry. The FAA also
estimates that it would take about 5
work-hours per airplane and require
parts costing $20 per airplane to comply
with the inspection and re-routing that
would be required by this proposed AD.
The average labor rate is $85 per workhour.
Based on these figures, the FAA
estimates the inspection and re-routing
cost of this proposed AD on U.S.
operators to be $10,235, or $445 per
airplane.
DCA/750XL/37 is prompted by a review of
the installation of the engine fuel lines and
the electrical installation forward of the
engine firewall on aircraft fitted with an air
conditioner and/or a standby alternator,
including those aircraft configured for the
installation of an air conditioner and/or a
standby alternator. It was found that the
engine fuel feed lines hoses could possibly
chafe against the adjacent electrical wiring
and the ignition exciter, which could result
in a fuel leak and possible fire. The [CAA]
AD is issued to introduce the corrective
actions in Pacific Aerospace Mandatory
Service Bulletin (MSB) PACSB/XL/113 issue
2, dated 8 March 2019.
lotter on DSK11XQN23PROD with PROPOSALS1
interested parties have access to it
through their normal course of business
or by the means identified in the
ADDRESSES section.
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The FAA has included all known
costs in its cost estimate. According to
the manufacturer, however, some of the
costs of this proposed AD may be
covered under warranty, thereby
reducing the cost impact on affected
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.
The FAA is 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
The FAA 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) Would not affect intrastate
aviation in Alaska, and
(3) Would 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:
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48088
Federal Register / Vol. 86, No. 164 / Friday, August 27, 2021 / Proposed Rules
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Pacific Aerospace Limited: Docket No. FAA–
2021–0711; Project Identifier 2019–CE–
024–AD.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by October 12,
2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Pacific Aerospace
Limited Model 750XL airplanes, serial
numbers 101 through 215 inclusive, 220,
8001, and 8002, certificated in any category,
that are fitted with an air conditioner and/or
a standby alternator, including airplanes
configured for the installation of an air
conditioner and/or a standby alternator, as
shown in Figure 1 of Part A in Pacific
Aerospace Mandatory Service Bulletin
PACSB/XL/113, Issue 2, dated March 8, 2019
(MSB PACSB/XL/113, Issue 2).
(d) Subject
Joint Aircraft System Component (JASC)
Code 2820, Aircraft Fuel Distribution, and
2497, Electrical Power System Wiring.
(e) Unsafe Condition
This AD was prompted by mandatory
continuing airworthiness information (MCAI)
originated by an aviation authority of another
country to identify and address an unsafe
condition on an aviation product. The MCAI
describes the unsafe condition as chafing of
the engine fuel feed line hoses. The FAA is
issuing this AD to prevent chafing of the
engine fuel feed line hoses with electrical
wiring and the ignition exciter located
forward of the engine firewall. The unsafe
condition, if not addressed, could result in a
fuel leak and fire.
lotter on DSK11XQN23PROD with PROPOSALS1
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Within 50 hours time-in-service (TIS) or at
the next annual inspection after the effective
date of this AD, whichever occurs later,
inspect the engine fuel feed line hoses and
the electrical wiring for chafing and damage
in accordance with the Accomplishment
Instructions, Part A steps 3) and 4), in MSB
PACSB/XL/113, Issue 2.
(1) If there is any chafing or damage that
penetrates the orange outer covering of the
fuel line fire sleeve or if there is any chafed
or damaged electrical wiring, before further
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Jkt 253001
flight, inspect the fuel hose for chafing,
replace any chafed fire sleeve or fuel hose,
and reroute all fuel lines in accordance with
the Accomplishment Instructions, Part B, in
MSB PACSB/XL/113, Issue 2.
(2) If there are no chafed or damaged
engine fuel feed line hoses and no chafed or
damaged electrical wiring, within 50 hours
TIS or at the next annual inspection,
whichever occurs later, reroute all fuel lines
in accordance with the Accomplishment
Instructions, Part B, in MSB PACSB/XL/113,
Issue 2.
(h) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, International Validation
Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In
accordance with 14 CFR 39.19, send your
request to your principal inspector or local
Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the certification office,
send it to the attention of the person
identified in Related Information or email: 9AVS-AIR-730-AMOC@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(i) Related Information
(1) For more information about this AD,
contact Mike Kiesov, Aviation Safety
Engineer, General Aviation & Rotorcraft
Section, International Validation Branch,
FAA, 901 Locust, Room 301, Kansas City,
MO 64106; phone: (816) 329–4144; fax: (816)
329–4090; email: mike.kiesov@faa.gov.
(2) Refer to Civil Aviation Authority (CAA)
of New Zealand AD DCA/750XL/37, effective
April 25, 2019, for more information. You
may examine the CAA AD in the AD docket
at https://www.regulations.gov by searching
for and locating it in Docket No. FAA–2021–
0711.
(3) For service information identified in
this AD, contact the CAA of New Zealand,
Level 15, Asteron Centre, 55 Featherston
Street, Wellington 6011; phone: + 64 4 560
9400; fax: + 64 4 569 2024; email: info@
caa.govt.nz. You may view this service
information at the Airworthiness Products
Section, Operational Safety Branch, FAA,
901 Locust, Kansas City, MO 64106. For
information on the availability of this
material at the FAA, call (816) 329–4148.
Issued on August 23, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2021–18444 Filed 8–26–21; 8:45 am]
BILLING CODE 4910–13–P
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2021–0674; Airspace
Docket No. 21–ASW–14]
RIN 2120–AA66
Proposed Amendment Class D and
Class E Airspace; Ardmore, OK
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
This action proposes to
amend the Class D and Class E airspace
at Ardmore, OK. The FAA is proposing
this action as the result of airspace
reviews due to the decommissioning of
the Arbuckle non-directional beacon
(NDB). The geographic coordinates of
the airport would also be updated to
coincide with the FAA’s aeronautical
database.
DATES: Comments must be received on
or before October 12, 2021.
ADDRESSES: Send comments on this
proposal to the U.S. Department of
Transportation, Docket Operations,
West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590; telephone (202)
366–9826, or (800) 647–5527. You must
identify FAA Docket No. FAA–2021–
0674/Airspace Docket No. 21–ASW–14,
at the beginning of your comments. You
may also submit comments through the
internet at https://www.regulations.gov.
You may review the public docket
containing the proposal, any comments
received, and any final disposition in
person in the Dockets Office between
9:00 a.m. and 5:00 p.m., Monday
through Friday, except federal holidays.
FAA Order 7400.11E, Airspace
Designations and Reporting Points, and
subsequent amendments can be viewed
online at https://www.faa.gov/air_
traffic/publications/. For further
information, you can contact the
Airspace Policy Group, Federal Aviation
Administration, 800 Independence
Avenue SW, Washington, DC 20591;
telephone: (202) 267–8783. The Order is
also available for inspection at the
National Archives and Records
Administration (NARA). For
information on the availability of FAA
Order 7400.11E at NARA, email:
fr.inspection@nara.gov or go to https://
www.archives.gov/federal-register/cfr/
ibr-locations.html.
FOR FURTHER INFORMATION CONTACT:
Jeffrey Claypool, Federal Aviation
Administration, Operations Support
SUMMARY:
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]]>Agencies
[Federal Register Volume 86, Number 164 (Friday, August 27, 2021)]
[Proposed Rules]
[Pages 48086-48088]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-18444]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0711; Project Identifier 2019-CE-024-AD]
RIN 2120-AA64
Airworthiness Directives; Pacific Aerospace Limited Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Pacific Aerospace Limited Model 750XL airplanes. This
proposed 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 chafing of the
engine fuel feed line hoses. This proposed AD would require inspecting
the engine fuel feed line hoses and the electrical wiring and rerouting
all fuel lines. The FAA is proposing this AD to address the unsafe
condition on these products.
DATES: The FAA must receive comments on this proposed AD by October 12,
2021.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https://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: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this NPRM, contact the Civil
Aviation Authority of New Zealand, Level 15, Asteron Centre, 55
Featherston Street, Wellington 6011; phone: + 64 4 560 9400; fax: + 64
4 569 2024; email: [email protected]. You may view this service
information at the FAA, Airworthiness Products Section, Operational
Safety Branch, 901 Locust, Kansas City, MO 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 at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0711; 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 NPRM, the MCAI,
any comments received, and other information. The street address for
Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Mike Kiesov, Aviation Safety Engineer,
General Aviation & Rotorcraft Section, International Validation Branch,
FAA, 901 Locust, Room 301, Kansas City, MO 64106; phone: (816) 329-
4144; fax: (816) 329-4090; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2021-0711; Project Identifier
2019-CE-024-AD'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM
[[Page 48087]]
contain commercial or financial information that is customarily treated
as private, that you actually treat as private, and that is relevant or
responsive to this NPRM, it is important that you clearly designate the
submitted comments as CBI. Please mark each page of your submission
containing CBI as ``PROPIN.'' The FAA will treat such marked
submissions as confidential under the FOIA, and they will not be placed
in the public docket of this NPRM. Submissions containing CBI should be
sent to Mike Kiesov, Aviation Safety Engineer, General Aviation &
Rotorcraft Section, International Validation Branch, FAA, 901 Locust,
Room 301, Kansas City, MO 64106. Any commentary that the FAA receives
which is not specifically designated as CBI will be placed in the
public docket for this rulemaking.
Background
The Civil Aviation Authority (CAA), which is the aviation authority
for New Zealand, has issued AD No. DCA/750XL/37, effective April 25,
2019 (referred to after this as ``the MCAI''), to correct an unsafe
condition for certain Pacific Aerospace Limited Model 750XL airplanes.
The MCAI states:
DCA/750XL/37 is prompted by a review of the installation of the
engine fuel lines and the electrical installation forward of the
engine firewall on aircraft fitted with an air conditioner and/or a
standby alternator, including those aircraft configured for the
installation of an air conditioner and/or a standby alternator. It
was found that the engine fuel feed lines hoses could possibly chafe
against the adjacent electrical wiring and the ignition exciter,
which could result in a fuel leak and possible fire. The [CAA] AD is
issued to introduce the corrective actions in Pacific Aerospace
Mandatory Service Bulletin (MSB) PACSB/XL/113 issue 2, dated 8 March
2019.
You may examine the MCAI in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-
0711.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Pacific Aerospace Mandatory Service Bulletin
PACSB/XL/113, Issue 2, dated March 8, 2019. The service information
contains procedures for inspecting the engine fuel feed line hoses and
the electrical wiring for chafing or damage, rerouting all fuel lines
and the fuel transducer and pressure switch wiring (including
installing P clips), and inspecting the fuel hose for chafing and
replacing chafed fire sleeves or fuel hoses 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.
FAA's Determination
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI and
service information referenced above. The FAA is issuing this NPRM
after determining the unsafe condition described previously is likely
to exist or develop on other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in the service information described previously, except as discussed
under ``Differences Between this Proposed AD and the MCAI.''
Differences Between This Proposed AD and the MCAI
The MCAI requires an inspection at the next 150 hour maintenance
inspection or within the next 50 hours time-in-service (TIS), whichever
occurs later, while this proposed AD would require those actions within
50 hours TIS or at the next annual inspection after the effective date
of this AD, whichever occurs later. If there is no chafing and damage
found during the inspection, the MCAI requires certain follow-on
actions at the next 300 hour maintenance inspection or within the next
50 hours TIS, whichever is later. This proposed AD would require those
actions within 50 hours TIS or at the next annual inspection, whichever
occurs later, because there is no regulatory requirement for operators
in the U.S. to have 150-hour or 300-hour maintenance inspections.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 23 airplanes of U.S. registry. The FAA also estimates that it
would take about 5 work-hours per airplane and require parts costing
$20 per airplane to comply with the inspection and re-routing that
would be required by this proposed AD. The average labor rate is $85
per work-hour.
Based on these figures, the FAA estimates the inspection and re-
routing cost of this proposed AD on U.S. operators to be $10,235, or
$445 per airplane.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected 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.
The FAA is 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
The FAA 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) Would not affect intrastate aviation in Alaska, and
(3) Would 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:
[[Page 48088]]
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 airworthiness
directive:
Pacific Aerospace Limited: Docket No. FAA-2021-0711; Project
Identifier 2019-CE-024-AD.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by October 12, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Pacific Aerospace Limited Model 750XL
airplanes, serial numbers 101 through 215 inclusive, 220, 8001, and
8002, certificated in any category, that are fitted with an air
conditioner and/or a standby alternator, including airplanes
configured for the installation of an air conditioner and/or a
standby alternator, as shown in Figure 1 of Part A in Pacific
Aerospace Mandatory Service Bulletin PACSB/XL/113, Issue 2, dated
March 8, 2019 (MSB PACSB/XL/113, Issue 2).
(d) Subject
Joint Aircraft System Component (JASC) Code 2820, Aircraft Fuel
Distribution, and 2497, Electrical Power System Wiring.
(e) Unsafe Condition
This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country to identify and address an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as chafing of the
engine fuel feed line hoses. The FAA is issuing this AD to prevent
chafing of the engine fuel feed line hoses with electrical wiring
and the ignition exciter located forward of the engine firewall. The
unsafe condition, if not addressed, could result in a fuel leak and
fire.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 50 hours time-in-service (TIS) or at the next annual
inspection after the effective date of this AD, whichever occurs
later, inspect the engine fuel feed line hoses and the electrical
wiring for chafing and damage in accordance with the Accomplishment
Instructions, Part A steps 3) and 4), in MSB PACSB/XL/113, Issue 2.
(1) If there is any chafing or damage that penetrates the orange
outer covering of the fuel line fire sleeve or if there is any
chafed or damaged electrical wiring, before further flight, inspect
the fuel hose for chafing, replace any chafed fire sleeve or fuel
hose, and reroute all fuel lines in accordance with the
Accomplishment Instructions, Part B, in MSB PACSB/XL/113, Issue 2.
(2) If there are no chafed or damaged engine fuel feed line
hoses and no chafed or damaged electrical wiring, within 50 hours
TIS or at the next annual inspection, whichever occurs later,
reroute all fuel lines in accordance with the Accomplishment
Instructions, Part B, in MSB PACSB/XL/113, Issue 2.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, International Validation Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the manager of the certification office, send it to the
attention of the person identified in Related Information or email:
[email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(i) Related Information
(1) For more information about this AD, contact Mike Kiesov,
Aviation Safety Engineer, General Aviation & Rotorcraft Section,
International Validation Branch, FAA, 901 Locust, Room 301, Kansas
City, MO 64106; phone: (816) 329-4144; fax: (816) 329-4090; email:
[email protected].
(2) Refer to Civil Aviation Authority (CAA) of New Zealand AD
DCA/750XL/37, effective April 25, 2019, for more information. You
may examine the CAA AD in the AD docket at https://www.regulations.gov by searching for and locating it in Docket No.
FAA-2021-0711.
(3) For service information identified in this AD, contact the
CAA of New Zealand, Level 15, Asteron Centre, 55 Featherston Street,
Wellington 6011; phone: + 64 4 560 9400; fax: + 64 4 569 2024;
email: [email protected]. You may view this service information at
the Airworthiness Products Section, Operational Safety Branch, FAA,
901 Locust, Kansas City, MO 64106. For information on the
availability of this material at the FAA, call (816) 329-4148.
Issued on August 23, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021-18444 Filed 8-26-21; 8:45 am]
BILLING CODE 4910-13-P
