Published 2021-11-05 · Federal Register document 2021-24084
Airworthiness Directives; Pacific Aerospace Limited Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain Pacific Aerospace Limited Model 750XL airplanes. This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as chafing damage in the port wing skin caused by the fuel system finger filters. This AD requires inspecting the wing internal skin for chafing and taking any necessary corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:08.106391+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2021-9c919420683447c6
- Source row
- results[390]
- Raw source SHA-256
- 9c919420683447c683ad0c877cb886e341c11862be32b47c536a001b1d76dcb5
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2021-21-10
- Effective date printed in this edition
- 2021-12-10
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective December 10,
2021.
Exact source excerpt. Text positions 8550–8642, end exclusive, in the original decoded publication. SHA-256: 287db8c8ee7fa50f1a5cad14174125e7dbdb7b01c5c573a38b21250c0efc711a
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 8642–8671, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Pacific Aerospace Limited Model 750XL
airplanes, serial numbers 100 through 205, 207 through 213, and
8001, certificated in any category.
Exact source excerpt. Text positions 8671–8854, end exclusive, in the original decoded publication. SHA-256: 49bf7b742f332fe9957db8d4e0d35221b2f7067d3c4dcbf511f6952eda711a0a
Subject
(d) Subject
Joint Aircraft System Component (JASC) Code 2800, Aircraft Fuel
System.
Exact source excerpt. Text positions 8854–8945, end exclusive, in the original decoded publication. SHA-256: 64027590fc8a096e22b261d1c2fc5ebd5d1cb8c31dfb419d8967b6a699d6fc50
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country to identify and correct an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as chafing damage
in the port wing skin caused by the fuel system finger filters. The
FAA is issuing this AD to detect and correct chafing in the left
hand (LH) wing leading edge tank skin, which if not detected and
corrected, could result in a port wing fuel leak and lead to engine
failure or fire.
Exact source excerpt. Text positions 8945–9522, end exclusive, in the original decoded publication. SHA-256: 05046eece39484b64d2f8cfa6e098719236a16b276bb6eaad750fea337a4677b
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 9522–9624, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Required Actions
(g) Required Actions
Within 165 hours time-in-service after the effective date of
this AD, modify the LH inspection panel assembly and inspect the LH
wing and fuel tank for chafing, and then, before further flight,
repair any chafing and install the panels in accordance with the
Accomplishment Instructions in Pacific Aerospace Limited Mandatory
Service Bulletin PACSB/XL/099, Issue 1, dated January 16, 2019.
Exact source excerpt. Text positions 9624–10046, end exclusive, in the original decoded publication. SHA-256: a3618486edd5d54932ff568721527f103162864ba5ac7a4f9a4a743a302ce145
Alternative Methods of Compliance (AMOCs)
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, International Validation Branch, 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 paragraph (i)(1) of this AD 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.
Exact source excerpt. Text positions 10046–10801, end exclusive, in the original decoded publication. SHA-256: f5409ce0685c34135870cbcbbe7a903613f45835c369f206ad936fbbfa169e36
Related Information
(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
No. DCA/750XL/34, effective date February 7, 2019, for more
information. You may examine the CAA AD in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-
2021-0603.
Exact source excerpt. Text positions 10801–11388, end exclusive, in the original decoded publication. SHA-256: 4ee05c2455fd10f29d796b0b395b4f7482299044632dbfc2b3aaa5c6687ddf02
Material Incorporated by Reference
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 Limited Mandatory Service Bulletin PACSB/
XL/099, Issue 1, dated January 16, 2019.
(ii) [Reserved]
(3) For service information identified in this AD, 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].
(4) You may view this service information at 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.
(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, email: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 11388–12664, end exclusive, in the original decoded publication. SHA-256: e35435c9d01d6fd74a7234c3bd25b47c5fe1c6a883285213e08ff5a877d3eb66
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 2021-21-10 · 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: 64eee36658727577fc5dcc5539f28131db3ad3930f970a9fdb0bab673175c162. Source manifest: a4d073520e519a4f2cc6f30cf30ee0625e1ebf89b093aa77a9c5ff8c93739c5e.
Official source · 2021-11-05
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 86, Number 212 (Friday, November 5, 2021)]
[Rules and Regulations]
[Pages 61063-61064]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-24084]
[[Page 61063]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0603; Project Identifier 2019-CE-006-AD; Amendment
39-21770; AD 2021-21-10]
RIN 2120-AA64
Airworthiness Directives; Pacific Aerospace Limited Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Pacific Aerospace Limited Model 750XL airplanes. This AD was
prompted by mandatory continuing airworthiness information (MCAI)
originated by an aviation authority of another country to identify and
correct an unsafe condition on an aviation product. The MCAI identifies
the unsafe condition as chafing damage in the port wing skin caused by
the fuel system finger filters. This AD requires inspecting the wing
internal skin for chafing and taking any necessary corrective actions.
The FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective December 10, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 10,
2021.
ADDRESSES: For service information identified in this final rule,
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. It
is also available at https://www.regulations.gov by searching for and
locating Docket No. FAA-2021-0603.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0603; 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 final rule, the
MCAI, any comments received, and other information. The address for
Docket Operations is 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 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:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain serial-numbered
Pacific Aerospace Limited Model 750XL airplanes. The NPRM published in
the Federal Register on July 28, 2021 (86 FR 40384). The NPRM was
prompted by MCAI originated by the Civil Aviation Authority (CAA),
which is the aviation authority for New Zealand. The CAA of New Zealand
has issued AD No. DCA/750XL/34, effective date February 7, 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/34 is prompted by a report of finding chafing damage
in the port wing skin caused by the fuel finger filters. The [CAA]
AD is issued to introduce inspection and repair requirements with
the issue of Pacific Aerospace Mandatory Service Bulletin (MSB)
PACSB/XL/099 issue 1, dated 16 January 2019.
The MCAI requires inspecting the wing internal skin for chafing and
taking any necessary corrective actions.
You may examine the MCAI in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-
0603.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the costs.
Conclusion
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 reviewed the relevant
data and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these products. This AD is adopted as proposed in the
NPRM.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Pacific Aerospace Limited Mandatory Service
Bulletin PACSB/XL/099, Issue 1, dated January 16, 2019. The service
information contains procedures for removing and modifying the
inspection panel assembly, inspecting the wing internal skin for
chafing, repairing any chafing damage and replacing the fuel filter as
necessary, and reinstalling the inspection panel assembly. 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 ADDRESSES.
Costs of Compliance
The FAA estimates that this AD affects 23 airplanes of U.S.
registry. The FAA also estimates that it would take about 5 work-hours
per airplane to do the inspection and modification requirements of this
proposed AD, and no parts would be necessary. Based on these figures,
the FAA estimates the cost of the inspection and modification for U.S.
operators to be $9,725, or $425 per airplane.
In addition, the FAA estimates that that any necessary follow-on
actions for repair or replacement requirements of this AD will take
about 6 work-hours and require parts costing $150, for a cost of $660
per airplane. The FAA has no way of determining the number of airplanes
that may need these actions.
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
[[Page 61064]]
develop on products identified in this rulemaking action.
Regulatory Findings
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) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The 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 airworthiness
directive:
2021-21-10 Pacific Aerospace Limited: Amendment 39-21770; Docket No.
FAA-2021-0603; Project Identifier 2019-CE-006-AD.
(a) Effective Date
This airworthiness directive (AD) is effective December 10,
2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Pacific Aerospace Limited Model 750XL
airplanes, serial numbers 100 through 205, 207 through 213, and
8001, certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code 2800, Aircraft Fuel
System.
(e) Unsafe Condition
This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country to identify and correct an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as chafing damage
in the port wing skin caused by the fuel system finger filters. The
FAA is issuing this AD to detect and correct chafing in the left
hand (LH) wing leading edge tank skin, which if not detected and
corrected, could result in a port wing fuel leak and lead to engine
failure or fire.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 165 hours time-in-service after the effective date of
this AD, modify the LH inspection panel assembly and inspect the LH
wing and fuel tank for chafing, and then, before further flight,
repair any chafing and install the panels in accordance with the
Accomplishment Instructions in Pacific Aerospace Limited Mandatory
Service Bulletin PACSB/XL/099, Issue 1, dated January 16, 2019.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, International Validation Branch, 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 paragraph (i)(1) of this AD 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
No. DCA/750XL/34, effective date February 7, 2019, for more
information. You may examine the CAA AD in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-
2021-0603.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 Limited Mandatory Service Bulletin PACSB/
XL/099, Issue 1, dated January 16, 2019.
(ii) [Reserved]
(3) For service information identified in this AD, 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].
(4) You may view this service information at 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.
(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, email: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on October 8, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-24084 Filed 11-4-21; 8:45 am]
BILLING CODE 4910-13-P
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- 64eee36658727577fc5dcc5539f28131db3ad3930f970a9fdb0bab673175c162
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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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