Rule2022-24289
Airworthiness Directives; De Havilland Aircraft of Canada Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
November 8, 2022
Effective
December 13, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is superseding Airworthiness Directive (AD) 2020-04- 20, which applied to certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series airplanes. AD 2020-04-20 required repetitive inspections of certain parts for discrepancies that meet specified criteria, and replacement as necessary; repetitive inspections of certain parts for damage and wear, and rework of parts; and electrical bonding checks of certain couplings. AD 2020-04-20 also required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. For certain airplanes, AD 2020-04-20 allowed a modification that terminates the repetitive inspections. This AD continues to require the actions in AD 2020-04-20, revises the applicability by adding airplanes, and requires, for certain airplanes, the previously optional rework and retrofit of certain parts of the fuel system. Doing the rework and retrofit terminates the retained initial and repetitive inspections in this AD. This AD was prompted by reports of wear on fuel couplings, bonding springs, and sleeves as well as fuel tube end ferrules and fuel component end ferrules, and by a determination that a more robust lightning ignition protection design is necessary. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 87 Issue 215 (Tuesday, November 8, 2022)</title>
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[Federal Register Volume 87, Number 215 (Tuesday, November 8, 2022)]
[Rules and Regulations]
[Pages 67354-67359]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-24289]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0672; Project Identifier MCAI-2020-01606-T;
Amendment 39-22228; AD 2022-23-01]
RIN 2120-AA64
Airworthiness Directives; De Havilland Aircraft of Canada Limited
(Type Certificate Previously Held by Bombardier, Inc.) Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
[[Page 67355]]
ACTION: Final rule.
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SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-04-
20, which applied to certain De Havilland Aircraft of Canada Limited
Model DHC-8-400 series airplanes. AD 2020-04-20 required repetitive
inspections of certain parts for discrepancies that meet specified
criteria, and replacement as necessary; repetitive inspections of
certain parts for damage and wear, and rework of parts; and electrical
bonding checks of certain couplings. AD 2020-04-20 also required
revising the existing maintenance or inspection program, as applicable,
to incorporate new or more restrictive airworthiness limitations. For
certain airplanes, AD 2020-04-20 allowed a modification that terminates
the repetitive inspections. This AD continues to require the actions in
AD 2020-04-20, revises the applicability by adding airplanes, and
requires, for certain airplanes, the previously optional rework and
retrofit of certain parts of the fuel system. Doing the rework and
retrofit terminates the retained initial and repetitive inspections in
this AD. This AD was prompted by reports of wear on fuel couplings,
bonding springs, and sleeves as well as fuel tube end ferrules and fuel
component end ferrules, and by a determination that a more robust
lightning ignition protection design is necessary. The FAA is issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective December 13, 2022.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of May 4, 2020
(85 FR 17473, March 30, 2020).
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-0672; 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 mandatory continuing airworthiness
information (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.
Material Incorporated by Reference
<bullet> For service information identified in this final rule,
contact De Havilland Aircraft of Canada Limited, Dash 8 Series Customer
Response Centre, 5800 Explorer Drive, Mississauga, Ontario, L4W 5K9,
Canada; telephone North America (toll-free): 855-310-1013, Direct: 647-
277-5820; email <a href="/cdn-cgi/l/email-protection#f5819d91b5c994d59d879093c8" http: dehavilland.com">dehavilland.com</a>">thd@<a href="http://dehavilland.com">dehavilland.com</a></a>; website <a href="http://dehavilland.com">dehavilland.com</a>.
<bullet> You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2022-0672.
FOR FURTHER INFORMATION CONTACT: Joseph Catanzaro, Aerospace Engineer,
Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7366; email <a href="/cdn-cgi/l/email-protection#487165293e3b652631292b27652b273b082e2929662f273e"><span class="__cf_email__" data-cfemail="291004485f5a044750484a46044a465a694f4848074e465f">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2020-04-20, Amendment 39-19857 (85 FR
17473, March 30, 2020) (AD 2020-04-20). AD 2020-04-20 applied to
certain De Havilland Aircraft of Canada Limited Model DHC-8-400 series
airplanes. AD 2020-04-20 required repetitive inspections of certain
parts for discrepancies that meet specified criteria, and replacement
as necessary; repetitive inspections of certain parts for damage and
wear, and rework of parts; and electrical bonding checks of certain
couplings. AD 2020-04-20 also required revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations. For certain airplanes, AD
2020-04-20 allowed a modification that terminated the repetitive
inspections. The FAA issued AD 2020-04-20 to address wear on fuel
couplings, bonding springs, and sleeves as well as fuel tube end
ferrules and fuel component end ferrules, which could reduce the
integrity of the electrical bonding paths through the fuel line and
components, and ultimately lead to fuel tank ignition in the event of a
lightning strike.
The NPRM published in the Federal Register on June 9, 2022 (87 FR
35128). The NPRM was prompted by AD CF-2017-04R3, dated April 1, 2020,
issued by Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada (referred to after this as the MCAI). The MCAI
states that wear has been detected on fuel couplings, bonding springs,
and sleeves as well as fuel tube end ferrules and fuel component end
ferrules. The MCAI also states that a more robust lightning ignition
protection design is necessary. The MCAI states that such wear could
reduce the integrity of the electrical bonding paths through the fuel
line and components, and ultimately lead to fuel tank ignition in the
event of a lightning strike.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-0672.
In the NPRM, the FAA proposed to continue to require the actions in
AD 2020-04-20, revise the applicability by adding airplanes, and
require, for certain airplanes, the previously optional rework and
retrofit of certain parts of the fuel system.
The FAA issued a supplemental notice of proposed rulemaking (SNPRM)
to amend 14 CFR part 39 to supersede AD 2020-04-20. The SNPRM published
in the Federal Register on August 31, 2022 (87 FR 53424) (the SNPRM).
The SNPRM was prompted by the FAA's determination that the NPRM
inadvertently limited the proposed new terminating rework and retrofit
to airplanes that had accomplished certain service information. In
addition, the FAA determined that the optional terminating action
specified in AD 2020-04-20, and corresponding credit, should be carried
over to this AD. In the SNPRM, the FAA proposed to continue to require
the actions in AD 2020-04-20, revise the applicability by adding
airplanes, and require, for certain airplanes, the previously optional
rework and retrofit of certain parts of the fuel system. The FAA is
issuing this AD to address the unsafe condition on these products.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from the Air Line Pilots Association,
International (ALPA) who supported the SNPRM without change.
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
referenced above. The FAA reviewed the relevant data, considered the
comment received, and determined that air safety requires adopting this
AD as proposed. Accordingly, the FAA is issuing this AD to address the
unsafe condition on this product. Except for
[[Page 67356]]
minor editorial changes, this AD is adopted as proposed in the SNPRM.
None of the changes will increase the economic burden on any operator.
Related Service Information Under 1 CFR Part 51
This AD requires the following service information, which the
Director of the Federal Register approved for incorporation by
reference as of May 4, 2020 (85 FR 17473, March 30, 2020).
<bullet> Bombardier Service Bulletin 84-28-20, Revision D, dated
November 23, 2018.
<bullet> Bombardier Service Bulletin 84-28-21, Revision C, dated
July 13, 2018.
<bullet> Bombardier Service Bulletin 84-28-26, Revision A, dated
November 29, 2018.
<bullet> Q400 Dash 8 (Bombardier) Temporary Revision ALI-0192,
dated April 24, 2018.
<bullet> Q400 Dash 8 (Bombardier) Temporary Revision ALI-0193,
dated April 24, 2018.
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.
Costs of Compliance
The FAA estimates that this AD affects 54 airplanes of U.S.
registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions *
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost per product operators
----------------------------------------------------------------------------------------------------------------
Retained actions from AD 2020-04- 268 work-hours x $85 $0 $22,780............ $1,230,120.
20. per hour = $22,780.
New actions..................... Up to 1,747 87,385 Up to $235,880..... Up to $12,737,520.
work[dash]hours x
$85 per hour = Up to
$148,495.
----------------------------------------------------------------------------------------------------------------
* Table does not include estimated costs for revising the existing maintenance or inspection program.
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the FAA recognizes that this number may vary from operator to
operator. In the past, the FAA has estimated that this action takes 1
work-hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), the FAA has
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, the FAA estimates the total cost per
operator to be $7,650 (90 work-hours x $85 per work-hour).
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 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:
0
a. Removing Airworthiness Directive (AD) 2020-04-20, Amendment 39-19857
(85 FR 17473, March 30, 2020); and
0
b. Adding the following new AD:
2022-23-01 De Havilland Aircraft of Canada Limited (Type Certificate
previously held by Bombardier, Inc.): Amendment 39-22228; Docket No.
FAA-2022-0672; Project Identifier MCAI-2020-01606-T.
(a) Effective Date
This airworthiness directive (AD) is effective December 13,
2022.
(b) Affected ADs
This AD replaces AD 2020-04-20, Amendment 39-19857 (85 FR 17473,
March 30, 2020) (AD 2020-04-20).
(c) Applicability
This AD applies to De Havilland Aircraft of Canada Limited Model
DHC-8-400, -401, and -402 airplanes, certificated in any category,
manufacturer serial numbers 4001 and 4003 and subsequent.
(d) Subject
Air Transport Association (ATA) of America Code 28, Fuel.
(e) Reason
This AD was prompted by reports of wear on fuel couplings,
bonding springs, and sleeves as well as fuel tube end ferrules and
fuel component end ferrules, and by a determination that a more
robust lightning ignition protection design is necessary. The FAA is
issuing this AD to address such wear, which could reduce the
integrity of the electrical bonding paths through the fuel line and
components, and ultimately lead to fuel tank ignition in the event
of a lightning strike.
[[Page 67357]]
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Initial Inspection Compliance Times, With New Terminating
Action
This paragraph restates the requirements of paragraph (g) of AD
2020-04-20, with new terminating action. For airplanes having serial
numbers 4001 and 4003 through 4575 inclusive that, as of May 4, 2020
(the effective date of AD 2020-04-20), have not done the actions
specified in Bombardier Service Bulletin 84-28-21: At the applicable
times specified in paragraph (g)(1) or (2) of this AD, do the
actions specified in paragraphs (h)(1) and (2) of this AD.
Accomplishing the terminating action required by paragraph (p) of
this AD terminates the initial inspection required by this
paragraph.
(1) For all airplanes except those identified in paragraph
(g)(2) of this AD: Within 6,000 flight hours or 36 months, whichever
occurs first after May 4, 2020 (the effective date of AD 2020-04-
20).
(2) For airplanes with an original airworthiness certificate or
original export certificate of airworthiness issued on or after May
4, 2020 (the effective date of AD 2020-04-20): Within 6,000 flight
hours or 36 months, whichever occurs first after the date of
issuance of the original airworthiness certificate or the date of
issuance of the original export certificate of airworthiness.
(h) Retained Repetitive Inspections and Corrective Actions, With New
Terminating Action
This paragraph restates the requirements of paragraph (h) of AD
2020-04-20, with new terminating action. For airplanes having serial
numbers 4001 and 4003 through 4575 inclusive that, as of May 4, 2020
(the effective date of AD 2020-04-20), have not done the actions
specified in Bombardier Service Bulletin 84-28-21: At the applicable
times specified in paragraph (g)(1) or (2) of this AD, do the
actions specified in paragraphs (h)(1) and (2) of this AD. Repeat
the actions thereafter at intervals not to exceed 6,000 flight hours
or 36 months, whichever occurs first. Accomplishing the terminating
action required by paragraph (p) of this AD terminates the
repetitive inspections required by this paragraph.
(1) Do a detailed inspection of the clamshell coupling bonding
wires, fuel couplings, and associated sleeves for discrepancies that
meet specified criteria, as identified in, and in accordance with,
paragraph 3.B., ``Procedure,'' of the Accomplishment Instructions of
Bombardier Service Bulletin 84-28-20, Revision D, dated November 23,
2018. If any conditions are found meeting the criteria specified in
Bombardier Service Bulletin 84-28-20, Revision D, dated November 23,
2018, before further flight, replace affected parts with new
couplings and sleeves of the same part number, in accordance with
paragraph 3.B., ``Procedure,'' of the Accomplishment Instructions of
Bombardier Bulletin 84-28-20, Revision D, dated November 23, 2018.
(2) Do a detailed inspection of the fuel tube end ferrules, fuel
component end ferrules, and ferrule O-ring flanges for damage and
wear, and rework (repair, replace, or blend, as applicable) the
parts, in accordance with paragraph 3.B., ``Procedure,'' of the
Accomplishment Instructions of Bombardier Service Bulletin 84-28-20,
Revision D, dated November 23, 2018.
(i) Retained Optional Terminating Action for Repetitive Inspections
With No Changes
This paragraph restates the requirements of paragraph (i) of AD
2020-04-20, with no changes. For airplanes having serial numbers
4001 and 4003 through 4575 inclusive: Doing a detailed inspection of
the fuel tube end ferrules, fuel component end ferrules, and ferrule
O-ring flanges for damage and wear, and reworking (repair, replace,
or blend, as applicable) the parts; and doing a retrofit (structural
rework) of the fuel couplings, isolators, and structural provisions,
in accordance with paragraph 3.B., ``Procedure,'' of the
Accomplishment Instructions of Bombardier Service Bulletin 84-28-21,
Revision C, dated July 13, 2018, terminates the inspections
specified in paragraphs (h)(1) and (2) of this AD.
(j) Retained Electrical Bonding Checks/Detailed Inspection, With No
Changes
This paragraph restates the requirements of paragraph (j) of AD
2020-04-20, with no changes. For airplanes having serial numbers
4001, 4003 through 4489 inclusive, and 4491 through 4575 inclusive
that, as of May 4, 2020 (the effective date of AD 2020-04-20), have
done the actions specified in Bombardier Service Bulletin 84-28-21,
Revision A, dated September 29, 2017; and airplanes having serial
numbers 4576 through 4581 inclusive: Within 6,000 flight hours or 36
months after May 4, 2020, whichever occurs first, do the actions
specified in paragraph (j)(1) or (2) of this AD.
(1) Accomplish electrical bonding checks of all threaded
couplings on the inboard vent lines in the left and right wings, in
accordance with paragraph 3.B., ``Procedure,'' of the Accomplishment
Instructions of Bombardier Service Bulletin 84-28-26, Revision A,
dated November 29, 2018.
(2) Do a detailed inspection of the fuel tube end ferrules, fuel
component end ferrules, and ferrule O-ring flanges for damage and
wear, and rework (repair, replace, or blend, as applicable) the
parts; and a retrofit (structural rework) of the fuel couplings,
isolators, and structural provisions; in accordance with paragraph
3.B., ``Procedure,'' of the Accomplishment Instructions of
Bombardier Service Bulletin 84-28-21, Revision C, dated July 13,
2018.
(k) Retained Revision of the Existing Maintenance or Inspection
Program, With No Changes
This paragraph restates the requirements of paragraph (k) of AD
2020-04-20, with no changes. Within 30 days after May 4, 2020 (the
effective date of AD 2020-04-20), revise the existing maintenance or
inspection program, as applicable, to incorporate the information
specified in Q400 Dash 8 (Bombardier) Temporary Revision ALI-0192,
dated April 24, 2018; and Q400 Dash 8 (Bombardier) Temporary
Revision ALI-0193, dated April 24, 2018. Except as specified in
paragraph (l) of this AD, the initial compliance time for doing the
tasks in Q400 Dash 8 (Bombardier) Temporary Revision ALI-0192, dated
April 24, 2018, is at the time specified in Q400 Dash 8 (Bombardier)
Temporary Revision ALI-0192, dated April 24, 2018, or within 30 days
after May 4, 2020, whichever occurs later.
(l) Retained Initial Compliance Time for Task 284000-419, With No
Changes
This paragraph restates the requirements of paragraph (l) of AD
2020-04-20, with no changes. The initial compliance time for task
284000-419 is at the time specified in paragraph (l)(1) or (2) of
this AD, as applicable, or within 30 days after May 4, 2020 (the
effective date of AD 2020-04-20), whichever occurs later.
(1) For airplanes having serial numbers 4001 and 4003 through
4575 inclusive: Within 18,000 flight hours or 108 months, whichever
occurs first, after the earliest date of embodiment of Bombardier
Service Bulletin 84-28-21 on the airplane.
(2) For airplanes having serial numbers 4576 and subsequent:
Within 18,000 flight hours or 108 months, whichever occurs first,
from the date of issuance of the original airworthiness certificate
or original export certificate of airworthiness.
(m) Retained No Alternative Actions, Intervals, or Critical Design
Configuration Control Limitations (CDCCLs), With No Changes
This paragraph restates the requirements of paragraph (m) of AD
2020-04-20, with no changes. After the existing maintenance or
inspection program has been revised as required by paragraph (k) of
this AD, no alternative actions (e.g., inspections), intervals, or
CDCCLs may be used unless the actions, intervals, and CDCCLs are
approved as an alternative method of compliance (AMOC) in accordance
with the procedures specified in paragraph (r)(1) of this AD.
(n) Retained No Reporting Provisions, With No Changes
This paragraph restates the provisions of paragraph (n) of AD
2020-04-20, with no changes. Although Bombardier Service Bulletin
84-28-20, Revision D, dated November 23, 2018, specifies to submit
certain information to the manufacturer, this AD does not include
that requirement.
(o) Retained Credit for Previous Actions, With No Changes
(1) This paragraph restates the provisions of paragraph (o) of
AD 2020-04-20, with no changes. This paragraph provides credit for
the actions required by paragraphs (h)(1) and (2) of this AD, if
those actions were performed before May 4, 2020 (the effective date
of AD 2020-04-20), using the service information specified in
paragraph (o)(1)(i) through (iii) of this AD.
(i) Bombardier Service Bulletin 84-28-20, Revision A, dated
December 14, 2016.
(ii) Bombardier Service Bulletin 84-28-20, Revision B, dated
February 13, 2017.
(iii) Bombardier Service Bulletin 84-28-20, Revision C, dated
April 28, 2017.
[[Page 67358]]
(2) For the airplane having serial number 4164, this paragraph
provides credit for the initial inspections required by paragraphs
(h)(1) and (2) of this AD, if those actions were performed before
May 4, 2020 (the effective date of AD 2020-04-20), using Bombardier
Service Bulletin 84-28-20, dated September 30, 2016.
(3) This paragraph provides credit for the actions specified in
paragraph (i) of this AD if those actions were performed before May
4, 2020 (the effective date of AD 2020-04-20), using the service
information specified in paragraph (o)(3)(i) through (iii) of this
AD.
(i) Bombardier Service Bulletin 84-28-21, dated August 31, 2017.
(ii) Bombardier Service Bulletin 84-28-21, Revision A, dated
September 29, 2017.
(iii) Bombardier Service Bulletin 84-28-21, Revision B, dated
June 8, 2018.
(4) This paragraph provides credit for the actions required by
paragraph (j)(1) of this AD if those actions were performed before
May 4, 2020 (the effective date of AD 2020-04-20), using Bombardier
Service Bulletin 84-28-26, dated August 14, 2018.
(5) This paragraph provides credit for the actions required by
paragraph (j)(2) of this AD if those actions were performed before
May 4, 2020 (the effective date of AD 2020-04-20), using Bombardier
Service Bulletin 84-28-21, Revision B, dated June 8, 2018.
(6) For airplanes having serial numbers 4001, 4003 through 4489
inclusive, and 4491 through 4575 inclusive, and that are post
Bombardier Service Bulletin 84-28-21, Revision A, dated September
29, 2017: This paragraph provides credit for the actions required by
paragraph (j) of this AD if those actions were performed before May
4, 2020 (the effective date of AD 2020-04-20), using the service
information specified in paragraph (o)(6)(i) or (ii) of this AD.
(i) Bombardier Modification Summary Package (ModSum)
IS4Q2800032, dated February 1, 2018.
(ii) Any airworthiness limitation change request (ACR) specified
in figure 1 to paragraph (o)(6)(ii) of this AD.
[GRAPHIC] [TIFF OMITTED] TR08NO22.000
(p) New Rework and Retrofit
For airplanes having serial numbers 4001 and 4003 through 4575
inclusive: At the applicable time specified in paragraph (p)(1) or
(2) of this AD, rework (repair, replace, or blend, as applicable)
the parts (fuel tube end ferrules, fuel component end ferrules, and
ferrule O-ring flanges); and do a retrofit (structural rework) of
the fuel couplings, isolators, and structural provisions; in
accordance with Part B of paragraph 3.B., ``Procedure,'' of the
Accomplishment Instructions of Bombardier Service Bulletin 84-28-21,
Revision C, dated July 13, 2018. Accomplishing these actions
terminates the initial and repetitive inspections required by
paragraphs (g) and (h) of this AD.
(1) For airplanes with greater than 20,000 total flight hours as
of the effective date of this AD: Do the actions within 6,000 flight
hours or 36 months after the effective date of this AD, whichever
occurs first.
(2) For airplanes with less than or equal to 20,000 total flight
hours as of the effective date of this AD: Do the actions within
8,000 flight hours or 48 months after the effective date of this AD,
whichever occurs first.
(q) New Credit for Previous Actions
This paragraph provides credit for the actions required by
paragraph (p) of this AD, if those actions were performed before the
effective date of this AD using the service information specified in
paragraph (q)(1), (2), or (3) of this AD.
(1) Bombardier Service Bulletin 84-28-21, dated August 31, 2017.
(2) Bombardier Service Bulletin 84-28-21, Revision A, dated
September 29, 2017.
(3) Bombardier Service Bulletin 84-28-21, Revision B, dated June
8, 2018.
(r) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO 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 responsible Flight Standards Office, as appropriate. If
sending information directly to the manager of the New York ACO
Branch, mail it to ATTN: Program Manager, Continuing Operational
Safety, at the address identified in paragraph (s)(2) of this AD or
email to: <a href="/cdn-cgi/l/email-protection#87beaae6f1f4aae9fee6e4e8aae4e8f4c7e1e6e6a9e0e8f1"><span class="__cf_email__" data-cfemail="21180c4057520c4f5840424e0c424e52614740400f464e57">[email protected]</span></a>. If mailing information, also
submit information by email. Before using any approved AMOC, notify
your appropriate principal inspector, or lacking a principal
inspector, the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or Transport Canada Civil Aviation (TCCA); or De
Havilland Aircraft of Canada Limited's TCCA Design Approval
Organization (DAO). If approved by the DAO,
[[Page 67359]]
the approval must include the DAO-authorized signature.
(s) Additional Information
(1) Refer to TCCA AD CF-2017-04R3, dated April 1, 2020, for
related information. This TCCA AD may be found in the AD docket at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2022-0672.
(2) For more information about this AD, contact Joseph
Catanzaro, Aerospace Engineer, Airframe and Propulsion Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7366; email <a href="/cdn-cgi/l/email-protection#625b4f0314114f0c1b03010d4f010d11220403034c050d14"><span class="__cf_email__" data-cfemail="ae9783cfd8dd83c0d7cfcdc183cdc1ddeec8cfcf80c9c1d8">[email protected]</span></a>.
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (t)(4) and (5) of this AD.
(t) 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 this AD specifies otherwise.
(3) The following service information was approved for IBR on
May 4, 2020 (85 FR 17473, March 30, 2020).
(i) Bombardier Service Bulletin 84-28-20, Revision D, dated
November 23, 2018.
(ii) Bombardier Service Bulletin 84-28-21, Revision C, dated
July 13, 2018.
(iii) Bombardier Service Bulletin 84-28-26, Revision A, dated
November 29, 2018.
(iv) Bombardier Q400 Dash 8 (Bombardier) Temporary Revision ALI-
0192, dated April 24, 2018.
(v) Q400 Dash 8 (Bombardier) Temporary Revision ALI-0193, dated
April 24, 2018.
(4) For service information identified in this AD, contact De
Havilland Aircraft of Canada Limited, Dash 8 Series Customer
Response Centre, 5800 Explorer Drive, Mississauga, Ontario, L4W 5K9,
Canada; telephone North America (toll-free): 855-310-1013, Direct:
647-277-5820; email <a href="/cdn-cgi/l/email-protection#d2a6bab692eeb3f2baa0b7b4ef" http: dehavilland.com">dehavilland.com</a>">thd@<a href="http://dehavilland.com">dehavilland.com</a></a>; website <a href="http://dehavilland.com">dehavilland.com</a>.
(5) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(6) 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 <a href="/cdn-cgi/l/email-protection#87e1f5a9eee9f4f7e2e4f3eee8e9c7e9e6f5e6a9e0e8f1"><span class="__cf_email__" data-cfemail="5335217d3a3d20233630273a3c3d133d3221327d343c25">[email protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on October 25, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-24289 Filed 11-7-22; 8:45 am]
BILLING CODE 4910-13-P
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</html>Indexed from Federal Register on November 8, 2022.
This is legal information, not legal advice. Laws vary by jurisdiction and change frequently. Always verify current law with official sources and consult a licensed attorney in your jurisdiction for advice on your specific situation.