Rule2022-15485
Airworthiness Directives; BAE Systems (Operations) Limited 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
July 21, 2022
Effective
August 25, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is superseding Airworthiness Directive (AD) 2015-07- 05, which applied to all BAE Systems (Operations) Limited Model BAe 146 series airplanes and Model Avro 146-RJ series airplanes. AD 2015-07-05 required repetitive external eddy current inspections on the aft skin lap joints of the rear fuselage for cracking, corrosion, and other defects, and repair if necessary. This AD continues to require the actions in AD 2015-07-05, at certain revised compliance times, and also requires repetitive low frequency eddy current (LFEC) inspections for any cracking, corrosion, and other defects in the aft skin lap joints of the rear fuselage and in the fuselage skin panels, and repair if necessary. This AD was prompted by a report of a pressurization problem on an airplane during climb-out; a subsequent investigation showed a crack in the fuselage skin; and that repetitive LFEC inspections in the rear fuselage aft skin lap joints and in the fuselage skin panels are necessary. Certain compliance times must also be revised. 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 139 (Thursday, July 21, 2022)</title>
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[Federal Register Volume 87, Number 139 (Thursday, July 21, 2022)]
[Rules and Regulations]
[Pages 43400-43403]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-15485]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0508; Project Identifier MCAI-2021-01120-T;
Amendment 39-22118; AD 2022-14-13]
RIN 2120-AA64
Airworthiness Directives; BAE Systems (Operations) Limited
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2015-07-
05, which applied to all BAE Systems (Operations) Limited Model BAe 146
series airplanes and Model Avro 146-RJ series airplanes. AD 2015-07-05
required repetitive external eddy current inspections on the aft skin
lap joints of the rear fuselage for cracking, corrosion, and other
defects, and repair if necessary. This AD continues to require the
actions in AD 2015-07-05, at certain revised compliance times, and also
requires repetitive low frequency eddy current (LFEC) inspections for
any cracking, corrosion, and other defects in the aft skin lap joints
of the rear fuselage and in the fuselage skin panels, and repair if
necessary. This AD was prompted by a report of a pressurization problem
on an airplane during climb-out; a subsequent investigation showed a
crack in the fuselage skin; and that repetitive LFEC inspections in the
rear fuselage aft skin lap joints and in the fuselage skin panels are
necessary. Certain compliance times must also be revised. The FAA is
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective August 25, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 25,
2022.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of May
19, 2015 (80 FR 19871, April 14, 2015).
[[Page 43401]]
ADDRESSES: For service information identified in this final rule,
contact BAE Systems (Operations) Limited, Customer Information
Department, Prestwick International Airport, Ayrshire, KA9 2RW,
Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292
675704; email <a href="/cdn-cgi/l/email-protection#d88a99a8adbab4b1bbb9acb1b7b6ab98bab9bdaba1abacbdb5abf6bbb7b5"><span class="__cf_email__" data-cfemail="3a687b4a4f585653595b4e535554497a585b5f4943494e5f574914595557">[email protected]</span></a>; internet <a href="https://www.baesystems.com/Businesses/RegionalAircraft/index.htm">https://www.baesystems.com/Businesses/RegionalAircraft/index.htm</a>. You may view
this referenced 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 on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2022-
0508.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2022-
0508; 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, 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: Todd Thompson, Aerospace Engineer,
Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; telephone 206-231-3228; email
<a href="/cdn-cgi/l/email-protection#65310a01014b310d0a0815160a0b250304044b020a13"><span class="__cf_email__" data-cfemail="cd99a2a9a9e399a5a2a0bdbea2a38dabacace3aaa2bb">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The Civil Aviation Authority (CAA), which is the aviation authority
for the United Kingdom, has issued CAA AD G-2021-0008, dated September
8, 2021 (also referred to as the Mandatory Continuing Airworthiness
Information, or the MCAI), to correct an unsafe condition for all BAE
Systems (Operations) Limited Model BAe 146 series airplanes and Model
Avro 146-RJ series airplanes. You may examine the MCAI in the AD docket
on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and
locating Docket No. FAA-2022-0508.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2015-07-05, Amendment 39-18133 (80 FR
19871, April 14, 2015) (AD 2015-07-05). AD 2015-07-05 applied to all
BAE Systems (Operations) Limited Model BAe 146 series airplanes and
Model Avro 146-RJ series airplanes. The NPRM published in the Federal
Register on May 6, 2022 (87 FR 27037). The NPRM was prompted by a
report of a pressurization problem on an airplane during climb-out; a
subsequent investigation showed a crack in the fuselage skin; and that
repetitive LFEC inspections in the rear fuselage aft skin lap joints
and in the fuselage skin panels are necessary. Certain compliance times
must also be revised. The NPRM proposed to continue the actions
required in AD 2015-07-05, at certain revised compliance times, and
also require repetitive LFEC inspections for any cracking, corrosion,
and other defects in the aft skin lap joints of the rear fuselage and
in the fuselage skin panels, and repair if necessary. The FAA is
issuing this AD to address cracking, corrosion, and other defects on
the rear fuselage aft skin joints and frames and in the fuselage
panels, which could affect the structural integrity of the airplane.
See the MCAI for additional background information.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
requires adopting this AD as proposed. Except for minor editorial
changes, this AD is adopted as proposed in the NPRM. None of the
changes will increase the economic burden on any operator. Accordingly,
the FAA is issuing this AD to address the unsafe condition on these
products.
Related Service Information Under 1 CFR Part 51
BAE Systems (Operations) Limited has issued Inspection Service
Bulletin 53-239, Revision 5, including Appendix 2, Revision 5, and
Appendix 3, Revision 1, all dated March 2, 2017. This service
information describes procedures for repetitive external eddy current
and LFEC inspections on the aft skin lap joints of the rear fuselage
and in the fuselage skin panels, for any cracking, corrosion, and other
defects (e.g., surface damage and spot displacement); and repair if
necessary.
This AD also requires BAE Systems (Operations) Limited Inspection
Service Bulletin 53-239, including Appendix 2, Revision 3, dated May 7,
2014, which the Director of the Federal Register approved for
incorporation by reference as of May 19, 2015 (80 FR 19871, April 14,
2015).
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 20 airplanes of U.S.
registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Parts
Action Labor cost cost Cost per product Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Retained actions from AD 8 work-hours x $0 $680 per inspection cycle $13,600 per inspection
2015[dash]07[dash]05. $85 per hour = cycle.
$680 per
inspection cycle.
New proposed actions.......... 5 work-hours x 0 $425..................... $8,500 per inspection
$85 per hour = cycle.
$425.
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The FAA has received no definitive data on which to base the cost
estimates for the repairs specified in this AD.
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
[[Page 43402]]
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) 2015-07-05, Amendment 39-18133
(80 FR 19871, April 14, 2015); and
0
b. Adding the following new AD:
2022-14-13 BAE Systems (Operations) Limited: Amendment 39-22118;
Docket No. FAA-2022-0508; Project Identifier MCAI-2021-01120-T.
(a) Effective Date
This airworthiness directive (AD) is effective August 25, 2022.
(b) Affected Airworthiness Directives (ADs)
This AD replaces AD 2015-07-05, Amendment 39-18133 (80 FR 19871,
April 14, 2015) (AD 2015-07-05).
(c) Applicability
This AD applies to all BAE Systems (Operations) Limited Model
BAe 146-100A, -200A, and -300A airplanes; and Model Avro 146-RJ70A,
146-RJ85A, and 146-RJ100A airplanes; certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Reason
This AD was prompted by a report of a pressurization problem on
an airplane during climb-out; a subsequent investigation showed a
crack in the fuselage skin; and that repetitive low frequency eddy
current (LFEC) inspections in the rear fuselage aft skin lap joints
and in the fuselage skin panels are necessary. Certain compliance
times must also be revised. The FAA is issuing this AD to address
cracking, corrosion, and other defects on the rear fuselage aft skin
joints and frames and in the fuselage panels, which could affect the
structural integrity of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Repetitive Inspections, With New Service Information
This paragraph restates the requirements of paragraph (g) of AD
2015-07-05, with new service information.
(1) Within the compliance times specified in paragraphs
(g)(1)(i) and (ii) of this AD, as applicable: Do an external eddy
current inspection on the aft skin lap joints of the rear fuselage
for cracking, corrosion, and other defects (i.e., surface damage and
spot displacement); in accordance with paragraph 2.C. of the
Accomplishment Instructions of BAE Systems (Operations) Limited
Inspection Service Bulletin 53-239, including Appendix 2, Revision
3, dated May 7, 2014; or paragraph 2. of the Accomplishment
Instructions of BAE Systems (Operations) Limited Inspection Service
Bulletin 53-239, Revision 5, including Appendix 2, Revision 5, and
Appendix 3, Revision 1, all dated March 2, 2017. As of the effective
date of this AD, use BAE Systems (Operations) Limited Inspection
Service Bulletin 53-239, Revision 5, including Appendix 2, Revision
5, and Appendix 3, Revision 1, all dated March 2, 2017, only.
(i) For any airplane which has accumulated 9,000 flight cycles
or more since the airplane's first flight as of May 19, 2015 (the
effective date of AD 2015-07-05): Do the inspection within 1,000
flight cycles or 6 months after May 19, 2015, whichever occurs
first.
(ii) For any airplane which has accumulated less than 9,000
flight cycles since the airplane's first flight as of May 19, 2015
(the effective date of AD 2015-07-05): Do the inspection before
accumulating 10,000 flight cycles since the airplane's first flight.
(2) Repeat the inspection required by paragraph (g)(1) of this
AD thereafter at intervals not to exceed the times specified in
paragraphs (g)(2)(i) and (ii) of this AD, as applicable to the
airplane's modification status.
(i) For Model BAe 146 series airplanes and Model Avro 146-RJ
series airplanes post modification HCM50070E, or post modification
HCM50070F, or post modification HCM50259A, repeat the inspection at
intervals not to exceed 4,000 flight cycles.
(ii) For Model BAe 146 series airplanes and Model Avro 146-RJ
series airplanes premodification HCM50070E, and premodification
HCM50070F, and premodification HCM50259A, repeat the inspection at
intervals not to exceed 7,500 flight cycles.
(h) Retained Corrective Action With Revised Repair Approval
This paragraph restates the requirements of paragraph (h) of AD
2015-07-05, with revised repair approval. If any cracking,
corrosion, or other defect is found during any inspection required
by AD 2015-07-05: Before further flight as of May 19, 2015 (the
effective date of AD 2015-07-05), repair using a method approved by
the Manager, Large Aircraft Section, International Validation
Branch, FAA; or the European Aviation Safety Agency (EASA); or BAE
Systems (Operations) Limited's EASA Design Organization Approval
(DOA). If approved by the DOA, the approval must include the DOA-
authorized signature. Accomplishment of the repair does not
constitute a terminating action for the inspections required by
paragraph (g) of this AD. As of the effective date of this AD,
repair approvals must be obtained through the Manager, Large
Aircraft Section, International Validation Branch, FAA; or the Civil
Aviation Authority of the United Kingdom (UK CAA); or BAE Systems
(Operations) Limited's UK CAA DOA.
(i) New Requirement of This AD: Repetitive LFEC Inspections
After the effective date of this AD, at the applicable times
specified in paragraph 1.D. ``Compliance'' of BAE Systems
(Operations) Limited Inspection Service Bulletin 53-239, Revision 5,
including Appendix 2, Revision 5, and Appendix 3, Revision 1, all
dated March 2, 2017: Do an LFEC inspection for any cracking,
corrosion, and other defects in the aft skin lap joints of the rear
fuselage and in the fuselage skin panels, in accordance with
paragraph ``1. Procedure'' of Appendix 2 and Appendix 3 of BAE
Systems (Operations) Limited Inspection Service Bulletin 53-239,
Revision 5, including Appendix 2, Revision 5, and Appendix 3,
Revision 1, all dated March 2, 2017. Repeat the LFEC inspection
thereafter at intervals not to exceed the times specified in
paragraph 1.D. ``Compliance'' of BAE
[[Page 43403]]
Systems (Operations) Limited Inspection Service Bulletin 53-239,
Revision 5, including Appendix 2, Revision 5, and Appendix 3,
Revision 1, all dated March 2, 2017.
(j) New Requirement of This AD: Corrective Action
If any cracking, corrosion, or other defect is found during any
inspection required by this AD: Before further flight, repair using
a method approved by the Manager, Large Aircraft Section,
International Validation Branch, FAA; or the UK CAA; or BAE Systems
(Operations) Limited's UK CAA DOA. If approved by the DOA, the
approval must include the DOA-authorized signature. Accomplishment
of the repair does not constitute a terminating action for the
inspections required by paragraph (i) of this AD.
(k) Credit for Previous Actions
This paragraph provides credit for the following actions
required by this AD.
(1) This paragraph provides credit for the initial inspection
and corrective action on stringer 30, left hand (LH) and right hand
(RH), as required by paragraph (g) of this AD, if those actions were
performed before May 19, 2015 (the effective date of AD 2015-07-05),
using BAE Systems (Operations) Limited Inspection Service Bulletin
53-239, dated June 13, 2012, which is not incorporated by reference
in this AD.
(2) This paragraph provides credit for the initial inspection
and corrective action, as required by paragraph (g) of this AD, if
those actions were performed before May 19, 2015 (the effective date
of AD 2015-07-05), using BAE Systems (Operations) Limited Inspection
Service Bulletin 53-239, Revision 1, dated June 18, 2013, which is
not incorporated by reference in this AD.
(3) This paragraph provides credit for the initial inspection
and corrective action, as required by paragraph (g) of this AD, if
those actions were performed before May 19, 2015 (the effective date
of AD 2015-07-05), using BAE Systems (Operations) Limited Inspection
Service Bulletin 53-239, Revision 2, dated July 15, 2013, which is
not incorporated by reference in this AD.
(4) This paragraph provides credit for the initial inspection
and corrective action, as required by paragraph (g) of this AD, if
those actions were performed before May 19, 2015 (the effective date
of AD 2015-07-05), using BAE Systems (Operations) Limited Inspection
Service Bulletin 53-239, including Appendix 2, Revision 3, dated May
7, 2014, which was incorporated by reference in AD 2015-07-05,
Amendment 39-18133 (80 FR 19871, April 14, 2015).
(5) This paragraph provides credit for the actions required by
paragraph (i) of this AD, if those actions were performed before the
effective date of this AD using BAE Systems (Operations) Limited
Inspection Service Bulletin 53-239, Revision 4, including Appendix
2, Revision 4, and Appendix 3, Initial issue, dated March 31, 2016.
(l) No Reporting Requirement
Although BAE Systems (Operations) Limited Inspection Service
Bulletin 53-239, Revision 5, including Appendix 2, Revision 5, and
Appendix 3, Revision 1, all dated March 2, 2017, specifies to report
inspection findings, this AD does not require any report.
(m) Other FAA AD Provisions
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Large Aircraft Section, 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 responsible Flight
Standards Office, as appropriate. If sending information directly to
the Large Aircraft Section, International Validation Branch, send it
to the attention of the person identified in paragraph (n)(2) of
this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#e9d0c4a8bfbac4a8a0bbc4dedad9c4a8a4a6aaa98f8888c78e869f"><span class="__cf_email__" data-cfemail="96afbbd7c0c5bbd7dfc4bba1a5a6bbd7dbd9d5d6f0f7f7b8f1f9e0">[email protected]</span></a>.
(i) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(ii) AMOCs for the repetitive external eddy current inspections
approved previously for AD 2015-07-05 are approved as AMOCs for the
corresponding actions in paragraph (g) of this AD.
(2) Contacting the Manufacturer: As of the effective date of
this AD, for any requirement in this AD to obtain instructions from
a manufacturer, the instructions must be accomplished using a method
approved by the Manager, Large Aircraft Section, International
Validation Branch, FAA; or the UK CAA; or BAE Systems (Operations)
Limited's UK CAA DOA. If approved by the DOA, the approval must
include the DOA-authorized signature.
(n) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) CAA AD G-2021-0008, dated September 8, 2021, for related
information. This MCAI may be found in the AD docket on the internet
at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket
No. FAA-2022-0508.
(2) For more information about this AD, contact Todd Thompson,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
206-231-3228; email <a href="/cdn-cgi/l/email-protection#89dde6ededa7dde1e6e4f9fae6e7c9efe8e8a7eee6ff"><span class="__cf_email__" data-cfemail="b9edd6dddd97edd1d6d4c9cad6d7f9dfd8d897ded6cf">[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 (o)(5) and (6) of this AD.
(o) 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
August 25, 2022.
(i) BAE Systems (Operations) Limited Inspection Service Bulletin
53-239, Revision 5, including Appendix 2, Revision 5, and Appendix
3, Revision 1, all dated March 2, 2017.
(ii) [Reserved]
(4) The following service information was approved for IBR on
May 19, 2015 (80 FR 19871, April 14, 2015).
(i) BAE Systems (Operations) Limited Inspection Service Bulletin
53-239, including Appendix 2, Revision 3, dated May 7, 2014.
(ii) [Reserved]
(5) For service information identified in this AD, contact BAE
Systems (Operations) Limited, Customer Information Department,
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United
Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email
<a href="/cdn-cgi/l/email-protection#3a687b4a4f585653595b4e535554497a585b5f4943494e5f574914595557"><span class="__cf_email__" data-cfemail="2e7c6f5e5b4c42474d4f5a4741405d6e4c4f4b5d575d5a4b435d004d4143">[email protected]</span></a>; internet <a href="https://www.baesystems.com/Businesses/RegionalAircraft/index.htm">https://www.baesystems.com/Businesses/RegionalAircraft/index.htm</a>.
(6) 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.
(7) 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#91f7e3bff8ffe2e1f4f2e5f8feffd1fff0e3f0bff6fee7"><span class="__cf_email__" data-cfemail="3f594d1156514c4f5a5c4b5650517f515e4d5e11585049">[email protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on June 30, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022-15485 Filed 7-20-22; 8:45 am]
BILLING CODE 4910-13-P
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