Proposed Rule2024-20159
Airworthiness Directives; The Boeing Company 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
September 9, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to supersede Airworthiness Directive (AD) 2019-22-02, which applies to all The Boeing Company Model 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747-8F, and 747-8 series airplanes. AD 2019-22-02 was prompted by reports of uncommanded fore and aft movement of the Captain's and First Officer's seats. AD 2019-22-02 requires identifying the part number, and the serial number if applicable, of the Captain's and First Officer's seats, and applicable on-condition actions for affected seats. AD 2019- 22-02 also requires a one-time detailed inspection and repetitive checks of the horizontal movement system (HMS) of the Captain's and First Officer's seats, and applicable on-condition actions. AD 2019-22- 02 also provides an optional terminating action for the repetitive actions for certain seats. Since the FAA issued AD 2019-22-02, the FAA has determined that additional seats are affected by the unsafe condition. This proposed AD would retain the actions required by AD 2019-22-02 and adds an inspection of previously omitted part numbers. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 89 Issue 174 (Monday, September 9, 2024)</title>
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[Federal Register Volume 89, Number 174 (Monday, September 9, 2024)]
[Proposed Rules]
[Pages 73014-73020]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-20159]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2137; Project Identifier AD-2023-00297-T]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2019-22-02, which applies to all The Boeing Company Model 747-200B,
747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747-8F, and
747-8 series airplanes. AD 2019-22-02 was prompted by reports of
uncommanded fore and aft movement of the Captain's and First Officer's
seats. AD 2019-22-02 requires identifying the part number, and the
serial number if applicable, of the Captain's and First Officer's
seats, and applicable on-condition actions for affected seats. AD 2019-
22-02 also requires a one-time detailed inspection and repetitive
checks of the horizontal movement system (HMS) of the Captain's and
First Officer's seats, and applicable on-condition actions. AD 2019-22-
02 also provides an optional terminating action for the repetitive
actions for certain seats. Since the FAA issued AD 2019-22-02, the FAA
has determined that additional seats are affected by the unsafe
condition. This proposed AD would retain the actions required by AD
2019-22-02 and adds an inspection of previously omitted part numbers.
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 24,
2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-2137; 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, any comments received, and other
information. The street address for Docket Operations is listed above.
Material Incorporated by Reference:
<bullet> For Boeing material identified in this proposed AD,
contact Boeing Commercial Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Boulevard, MC 110-SK57, Seal Beach,
CA 90740-5600; phone 562-797-1717; website <a href="http://myboeingfleet.com">myboeingfleet.com</a>.
<bullet> You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th Street,
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> by
searching for and locating Docket No. FAA-2024-2137.
FOR FURTHER INFORMATION CONTACT: Courtney Tuck, Aviation Safety
Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone
206-231-3986; email <a href="/cdn-cgi/l/email-protection#80c3eff5f2f4eee5f9aecbaed4f5e3ebc0e6e1e1aee7eff6"><span class="__cf_email__" data-cfemail="dc9fb3a9aea8b2b9a5f297f288a9bfb79cbabdbdf2bbb3aa">[email protected]</span></a>.
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-2024-2137; Project Identifier
AD-2023-00297-T'' at the beginning of your comments. The most helpful
comments
[[Page 73015]]
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
<a href="http://regulations.gov">regulations.gov</a>, 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 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
Courtney Tuck, Aviation Safety Engineer, FAA, 2200 South 216th Street,
Des Moines, WA 98198; phone 206-231-3986; email
<a href="/cdn-cgi/l/email-protection#5c1f33292e2832392572177208293f371c3a3d3d723b332a"><span class="__cf_email__" data-cfemail="d497bba1a6a0bab1adfa9ffa80a1b7bf94b2b5b5fab3bba2">[email protected]</span></a>. Any commentary that the FAA receives that is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.
Background
The FAA issued AD 2019-22-02, Amendment 39-19781 (84 FR 67854,
December 12, 2019) (AD 2019-22-02), for all The Boeing Company Model
747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F,
747-8F, and 747-8 series airplanes. AD 2019-22-02 was prompted by
reports of uncommanded fore and aft movement of the Captain's and First
Officer's seats. AD 2019-22-02 requires an identification of the part
number, and if applicable the serial number, of the Captain's and First
Officer's seats, and applicable on-condition actions. AD 2019-22-02
also requires a one-time detailed inspection and repetitive checks of
the HMS of the Captain's and First Officer's seats, and applicable on-
condition actions. AD 2019-22-02 also provides an optional terminating
action for the repetitive checks of the HMS for certain airplanes. The
FAA issued AD 2019-22-02 to address uncommanded fore and aft movement
of the Captain's and First Officer's seats. An uncommanded fore or aft
seat movement during a critical part of a flight, such as takeoff or
landing, could cause a flight control obstruction or unintended flight
control input, which could result in the loss of the ability to control
the airplane.
Actions Since AD 2019-22-02 Was Issued
Since the FAA issued AD 2019-22-02, Boeing and the seat supplier
(Ipeco) determined that certain seat part numbers were inadvertently
omitted from the service information required by AD 2019-22-02. Ipeco
subsequently updated their service information to include the
additional part numbers, and Boeing updated their service information
as well. Based on this, the FAA has determined that additional seats
are affected by the unsafe condition.
FAA's Determination
The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed Boeing Special Attention Service Bulletin 747-25-
3644, Revision 2, dated January 27, 2023. The material describes
procedures for identification of the part number, and the serial number
if applicable, of the Captain's and First Officer's seats, and
applicable on-condition actions. On-condition actions include an
inspection of each seat's fore and aft and vertical manual control
levers for looseness, installation of serviceable seats, and a seat
operational test after any cable adjustment. This material also adds
Ipeco seat part numbers 3A258-0041-01-1Z and 3A258-0042-01-1Z.
The FAA also reviewed Boeing Special Attention Service Bulletin
747-25-3653, Revision 2, dated January 27, 2023. This material
describes procedures for a detailed inspection and repetitive checks of
the HMS (including for any Artus part and amendment numbers of the
horizontal actuator of the HMS) for the Captain's and First Officer's
seats for findings (e.g., evidence of cracks, scores, corrosion, dents,
deformation, or visible wear; and incorrectly assembled microswitch
assemblies, actuators, and limit switches), and applicable on-condition
actions. The on-condition actions include clearing the seat tracks of
foreign object debris (FOD), overhauling the HMS, and replacing the
horizontal actuator. This material also describes procedures for an
optional terminating action for the repetitive checks by installing a
serviceable Captain's or First Officer's seat.
This material is reasonably available because the interested
parties have access to it through their normal course of business or by
the means identified in ADDRESSES section.
Proposed AD Requirements in This NPRM
Although this proposed AD does not explicitly restate the
requirements of AD 2019-22-02, this proposed AD would retain all of the
requirements of AD 2019-22-02. Those requirements are referenced in the
service information identified previously, which, in turn, is
referenced in paragraphs (g) and (h) of this proposed AD.
This proposed AD would require accomplishing the actions specified
in the service information already described, except for any
differences identified as exceptions in the regulatory text of this
proposed AD. For information on the procedures and compliance times,
see this service information at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-
2024-2137.
Acceptable Methods of Compliance
The FAA has determined that the actions required by paragraphs (g)
and (h) of this AD are not required under specific conditions, e.g., if
it can be shown through maintenance records that the required actions
have already been accomplished by the previous revision of the service
information and specific conditions have been met. Paragraph (j) of
this AD identifies these conditions. Complying with these conditions
adequately addresses the unsafe condition identified in this proposed
AD.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 162 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
[[Page 73016]]
Estimated Costs for Required Actions per Seat
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Cost on U.S.
Action Labor cost Parts cost Cost per product operators
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Identification, seat (retained 1 work-hour x $85 $0 $85................ $27,540.
actions from AD 2019[dash]22-02). per hour = $85.
Detailed inspection, HMS 1 work-hour x $85 0 $85................ $27,540.
(retained actions from AD per hour = $85.
2019[dash]22-02).
Checks, HMS (retained actions 2 work-hours x $85 0 $170 per check $55,080 per check
from AD 2019-22-02). per hour = $170 cycle. cycle.
per check cycle.
Identification, seat (new 1 work-hour x $85 0 $85................ Up to $117,980.
proposed actions). per hour = $85.
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The FAA estimates the following costs to do any necessary on-
condition actions that will be required. The FAA has no way of
determining the number of aircraft that might need these on-condition
actions:
Estimated Costs of On-Condition Actions *
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Action Labor cost Parts cost Cost per product
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Adjustment, control lever cable...... 1 work-hour x $85 per $0..................... $85.
hour = $85.
Overhaul, HMS........................ 11 work-hours x $85 per Up to $5,824........... Up to $6,759.
hour = $935.
Inspection of each seat's fore/aft 1 work-hour x $85 per $0..................... $85 per seat.
and vertical manual control levers. hour = $85 per seat.
Installation of serviceable seats.... 1 work-hour x $85 per $0..................... $85 per seat.
hour = $85 per seat.
Clearing FOD......................... 1 work-hour x $85 per $0..................... $85 per seat.
hour = $85 per seat.
Replacement of the horizontal 1 work-hour x $85 per $7,937 per actuator.... $8,022 per actuator.
actuator. hour = $85 per
actuator.
Operational test, adjusted control 1 work-hour x $85 per $0..................... $85 per seat.
lever cable. hour = $85 per seat.
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* The estimated cost for tooling to align an affected seat for adjustment of the control lever cable is up to
$46,064.
The FAA has received no definitive data that would enable the FAA
to provide cost estimates for the optional terminating action for the
repetitive checks specified in this proposed 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 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:
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 2019-22-02, Amendment 39-19781 (84
FR 67854, December 12, 2019), and
0
b. Adding the following new Airworthiness Directive:
The Boeing Company: Docket No. FAA-2024-2137; Project Identifier AD-
2023-00297-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by October 24, 2024.
(b) Affected ADs
This AD replaces AD 2019-22-02, Amendment 39-19781 (84 FR 67854,
December 12, 2019) (AD 2019-22-02).
(c) Applicability
This AD applies to all The Boeing Company Model 747-200B, 747-
200C, 747-
[[Page 73017]]
200F, 747-300, 747-400, 747-400D, 747-400F, 747-8F, and 747-8 series
airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Unsafe Condition
This AD was prompted by reports of uncommanded fore and aft
movement of the Captain's and First Officer's seats. The FAA is
issuing this AD to address uncommanded fore and aft movement of the
Captain's and First Officer's seats. The unsafe condition, if not
addressed, could result in an uncommanded fore or aft seat movement
during a critical part of a flight, such as takeoff or landing, and
could cause a flight control obstruction or unintended flight
control input, which could result in the loss of the ability to
control the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Seat Part Number Identification and On-Condition Actions
Except as specified by paragraphs (i) and (j) of this AD: At the
applicable times specified in the ``Compliance'' paragraph of Boeing
Special Attention Service Bulletin 747-25-3644, Revision 2, dated
January 27, 2023, do an inspection to determine the part number, and
serial number as applicable, of the Captain's and First Officer's
seats, and all applicable on-condition actions identified in, and in
accordance with the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 747-25-3644, Revision 2, dated January
27, 2023. A review of airplane maintenance records is acceptable in
lieu of this inspection if the part number and serial number of the
Captain's and First Officer's seats can be conclusively determined
from that review.
(h) Detailed Inspection, and Repetitive Checks of Horizontal Movement
System and On-Condition Actions
Except as specified by paragraph (i) and (j) of this AD: At the
applicable times specified in the ``Compliance'' paragraph of Boeing
Special Attention Bulletin 747-25-3653, Revision 2, dated January
27, 2023, do all applicable actions identified as ``RC'' (required
for compliance) in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Bulletin 747-25-3653,
Revision 2, dated January 27, 2023. Actions identified as
terminating action in Boeing Special Attention Service Bulletin 747-
25-3653, Revision 2, dated January 27, 2023, terminate the
applicable required actions of this AD, provided the terminating
action is done in accordance with the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 747-25-3653, Revision 2,
dated January 27, 2023.
(i) Exceptions to Service Information Specifications
(1) Where the ``Compliance'' paragraph of Boeing Special
Attention Bulletin 747-25-3653, Revision 2, dated January 27, 2023,
refers to the original issue date of this bulletin, this AD requires
using January 16, 2020 (the effective date of AD 2019-22-02).
(2) Where the ``Compliance'' paragraph of Boeing Special
Attention Bulletin 747-25-3644, Revision 2, dated January 27, 2023,
refers to 72 months after the original issue date of this service
bulletin, this AD requires using 36 months after January 16, 2020
(the effective date of AD 2019-22-02).
(3) Where the ``Compliance'' paragraph of Boeing Special
Attention Bulletin 747-25-3644, Revision 2, dated January 27, 2023,
refers to the Revision 2 date of this service bulletin, this AD
requires using the effective date of the AD.
(j) Acceptable Conditions for Compliance
If the airplane records show that an Ipeco Captain's or First
Officer's seat meets all criteria specified in any row in figure 1
to paragraph (j) of this AD, the actions specified in paragraphs (g)
and (h) of this AD are not required for that seat.
Figure 1 to Paragraph (j)--Alternative Acceptable Seats
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[[Page 73019]]
[GRAPHIC] [TIFF OMITTED] TP09SE24.001
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(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, AIR-520, Continued Operational Safety 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 certification office,
send it to the attention of the person identified in paragraph (m)
of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#ffbeb2b0bcbf999e9ed1989089"><span class="__cf_email__" data-cfemail="ffbeb2b0bcbf999e9ed1989089">[email protected]</span></a>.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by The Boeing Company Organization Designation
Authorization (ODA) that has been authorized by the Manager, AIR-
520, Continued Operational Safety Branch, FAA, to make those
findings. To be approved, the repair method, modification deviation,
or alteration deviation must meet the certification basis of the
airplane, and the approval must specifically refer to this AD.
[[Page 73020]]
(4) AMOCs approved for AD 2019-22-02 are approved as AMOCs for
the corresponding provisions of Boeing Special Attention Service
Bulletin 747-25-3644, Revision 2, dated January 27, 2023, and Boeing
Special Attention Service Bulletin 747-25-3653, Revision 2, dated
January 27, 2023, that are required by paragraphs (g) and (h) of
this AD.
(5) For service information that contains steps that are labeled
as Required for Compliance (RC), the provisions of paragraphs
(k)(5)(i) and (ii) of this AD apply.
(i) The steps labeled as RC, including substeps under an RC step
and any figures identified in an RC step, must be done to comply
with the AD. If a step or substep is labeled ``RC Exempt,'' then the
RC requirement is removed from that step or substep. An AMOC is
required for any deviations to RC steps, including substeps and
identified figures.
(ii) Steps not labeled as RC may be deviated from using accepted
methods in accordance with the operator's maintenance or inspection
program without obtaining approval of an AMOC, provided the RC
steps, including substeps and identified figures, can still be done
as specified, and the airplane can be put back in an airworthy
condition.
(l) Related Information
For more information about this AD, contact Courtney Tuck,
Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines,
WA 98198; phone 206-231-3986; email <a href="/cdn-cgi/l/email-protection#afecc0dadddbc1cad681e481fbdaccc4efc9cece81c8c0d9"><span class="__cf_email__" data-cfemail="9eddf1ebeceaf0fbe7b0d5b0caebfdf5def8ffffb0f9f1e8">[email protected]</span></a>.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the material listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless the AD specifies otherwise.
(i) Boeing Special Attention Service Bulletin 747-25-3644,
Revision 2, dated January 27, 2023.
(ii) Boeing Special Attention Service Bulletin 747-25-3653,
Revision 2, dated January 27, 2023.
(3) For Boeing material identified in this AD, contact Boeing
Commercial Airplanes, Attention: Contractual & Data Services (C&DS),
2600 Westminster Boulevard, MC 110-SK57, Seal Beach, CA 90740-5600;
phone 562-797-1717; website <a href="http://myboeingfleet.com">myboeingfleet.com</a>.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th
Street, Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195.
(5) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit <a href="http://www.archives.gov/federal-register/cfr/ibr-locations">www.archives.gov/federal-register/cfr/ibr-locations</a> or email <a href="/cdn-cgi/l/email-protection#8bedf9a5e2e5f8fbeee8ffe2e4e5cbe5eaf9eaa5ece4fd"><span class="__cf_email__" data-cfemail="e78195c98e8994978284938e8889a789869586c9808891">[email protected]</span></a>.
Issued on August 26, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-20159 Filed 9-6-24; 8:45 am]
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