AD 2020-24-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | Various | Airworthiness Directives; The Boeing Company Airplanes |
Unsafe Condition
The autopilot flight director system (AFDS) failed to transition to the instrument landing system localizer (LOC) beam after the consistent localizer capture function in the flight control modules initiated a transition to capture LOC during approach.
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Required Actions
Revising the Operating Procedures chapter of the existing Airplane Flight Manual (AFM) to incorporate the procedures specified in figure 1 to paragraph (g) of this AD.
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Compliance Time
Within 14 days after the effective date of this AD
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Affected Aircraft
All The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in any category.
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Federal Register Abstract
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. As published, the regulatory text of the AD included errors in certain references to the airplane flight manual (AFM) that is required to be revised. This document corrects those errors. In all other respects, the original document remains the same.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to all The Boeing Company Model 787-8, 787-9,
and 787-10 airplanes, certificated in any category.
Document Text
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[Federal Register Volume 85, Number 240 (Monday, December 14, 2020)]
[Rules and Regulations]
[Pages 80589-80590]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2020-27507]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-1031; Project Identifier AD-2020-00846-T;
Amendment 39-21334; AD 2020-24-04]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to all The Boeing
Company Model 787-8, 787-9, and 787-10 airplanes. As published, the
regulatory text of the AD included errors in certain references to the
airplane flight manual (AFM) that is required to be revised. This
document corrects those errors. In all other respects, the original
document remains the same.
DATES: This correction is effective December 18, 2020. The effective
date of AD 2020-24-04 remains December 18, 2020.
ADDRESSES: You may examine the AD docket at <a href="https://www.regulations.gov">https://www.regulations.gov</a>; or in person at the Docket Management Facility
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: Frank Carreras, Aerospace Engineer,
Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South
216th St., Des Moines, WA 98198; phone and fax: 206-231-3539; email:
<a href="/cdn-cgi/l/email-protection#c8aebaa9a6a3e6aba9babaadbaa9bb88aea9a9e6afa7be"><span class="__cf_email__" data-cfemail="4f293d2e2124612c2e3d3d2a3d2e3c0f292e2e61282039">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION: As published, Airworthiness Directive 2020-
24-04, Amendment 39-21334 (85 FR 77991, December 3, 2020), requires
revising the existing AFM to incorporate procedures for conducting an
approach with a localizer-based navigation aid, monitoring localizer
raw data, calling out any significant deviations, and performing an
immediate go around if the airplane has not intercepted the final
approach course as shown by the localizer deviation. AD 2020-24-04
applies to all The Boeing Company Model 787-8, 787-9, and 787-10
airplanes.
As published, the regulatory text included errors in certain
references to the AFM that is required to be revised. The location of
the AFM text to be revised is incorrectly identified as the
``Limitations section''; the correct location is the ``Operating
Procedures chapter.'' In addition, the figure incorrectly identified
the heading of the AFM text as ``Operating Instructions''; the correct
heading is ``Autopilot Flight Director System--Operating
Instructions.''
Correction of Publication
This document corrects an error and correctly adds the AD as an
amendment to 14 CFR 39.13. Although no other part of the preamble or
regulatory information has been corrected, the FAA is publishing the
entire rule in the Federal Register.
The effective date of this AD remains December 18, 2020.
Since this action only corrects errors in certain AFM references,
it has no adverse economic impact and imposes no additional burden on
any person. Therefore, the FAA has determined that notice and public
comment procedures are unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Correction
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (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 [Corrected]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2020-24-04 The Boeing Company: Amendment 39-21334; Docket No. FAA-
2020-1031; Project Identifier AD-2020-00846-T.
(a) Effective Date
This AD is effective December 18, 2020.
(b) Affected ADs
None.
[[Page 80590]]
(c) Applicability
This AD applies to all The Boeing Company Model 787-8, 787-9,
and 787-10 airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 22, Auto flight.
(e) Unsafe Condition
This AD was prompted by reports indicating that the autopilot
flight director system (AFDS) failed to transition to the instrument
landing system localizer (LOC) beam after the consistent localizer
capture function in the flight control modules initiated a
transition to capture LOC during approach. The FAA is issuing this
AD to address the AFDS failing to transition, which could result in
localizer overshoot leading to glideslope descent on the wrong
heading. Combined with a lack of flight deck effects for a
consistent localizer capture mode failure, this condition could
result in a controlled flight into terrain.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Revise the Airplane Flight Manual (AFM)
Within 14 days after the effective date of this AD, revise the
Operating Procedures chapter of the existing AFM and applicable
corresponding operational procedures to incorporate the procedures
specified in figure 1 to paragraph (g) of this AD. Revising the
existing AFM to include the changes specified in paragraph (g) of
this AD may be done by inserting a copy of figure 1 to paragraph (g)
of this AD into the existing AFM.
[GRAPHIC] [TIFF OMITTED] TR14DE20.092
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Seattle 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 certification office, send it to the attention of the person
identified in paragraph (i) of this AD. Information may be emailed
to: <a href="/cdn-cgi/l/email-protection#1d24305c5350304e787c69697178305c5e52305c50525e304f786c68786e696e5d7b7c7c337a726b"><span class="__cf_email__" data-cfemail="ad9480ece3e080fec8ccd9d9c1c880eceee280ece0e2ee80ffc8dcd8c8ded9deedcbcccc83cac2db">[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, Seattle
ACO 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.
(i) Related Information
For more information about this AD, contact Frank Carreras,
Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO
Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax:
206-231-3539; email: <a href="/cdn-cgi/l/email-protection#107662717e7b3e7371626275627163507671713e777f66"><span class="__cf_email__" data-cfemail="345246555a5f1a5755464651465547745255551a535b42">[email protected]</span></a>.
(j) Material Incorporated by Reference
None.
Issued on December 9, 2020.
Ross Landes,
Deputy Director for Regulatory Operations, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-27507 Filed 12-10-20; 11:15 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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