Published 2022-11-30 · Federal Register document 2022-26083
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model BAe 146 series airplanes. This AD was prompted by a finding that when the autopilot is engaged, the architecture of the autopilot system does not automatically disconnect the autopilot in response to pilot application of a pitch input or when the electric pitch trim switch on either pilot control wheel is operated. This AD requires modifying the autopilot engagement circuit. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:11.345539+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2022-c0cc5a172b1306fa
- Source row
- results[373]
- Raw source SHA-256
- c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2022-23-07
- Effective date printed in this edition
- 2023-01-04
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective January 4, 2023.
Exact source excerpt. Text positions 8787–8876, end exclusive, in the original decoded publication. SHA-256: 145e94105b394800bd8f0b4753f5a602c487af745f6350c104dc934777652c22
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 8876–8905, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to all BAE Systems (Operations) Limited Model
BAe 146-100A, -200A, and -300A airplanes, certificated in any
category.
Exact source excerpt. Text positions 8905–9065, end exclusive, in the original decoded publication. SHA-256: 931053fa79db266a1ebea4babf2ee2669d7fdafbbe14557b3b9c3db89a8b8dd3
Subject
(d) Subject
Air Transport Association (ATA) of America Code 22, Auto-Flight.
Exact source excerpt. Text positions 9065–9148, end exclusive, in the original decoded publication. SHA-256: 73cb408cb74d410d52ee9815649c6fa70ef3a6d209da8a295e631da87fe85e8d
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a finding that when the autopilot is
engaged, the architecture of the autopilot system does not
automatically disconnect the autopilot in response to pilot
application of a pitch input or when the electric pitch trim switch
on either pilot control wheel is operated. The FAA is issuing this
AD to address continued autopilot engagement after flightcrew input
to disengage the autopilot, which could lead to reduced
controllability of the airplane.
Exact source excerpt. Text positions 9148–9654, end exclusive, in the original decoded publication. SHA-256: c2054784f7536420ffa9e4fedac297ede31df2cf3037294a2c33bd032cf97f14
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 9654–9756, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Modification
(g) Modification
Within 12 months after the effective date of this AD, modify the
autopilot engagement circuit in accordance with the Accomplishment
Instructions of BAE Systems (Operations) Limited Modification
Service Bulletin SB.22-072-36262A, dated September 14, 2021.
Exact source excerpt. Text positions 9756–10037, end exclusive, in the original decoded publication. SHA-256: 23c1de6129ca9b007b1d1da028052216f9de35215dd510e12ce099518a9b0102
No Reporting Requirement
(h) No Reporting Requirement
Although BAE Systems (Operations) Limited Modification Service
Bulletin SB.22-072-36262A, dated September 14, 2021, specifies to
submit certain information to the manufacturer, this AD does not
include that requirement.
Exact source excerpt. Text positions 10037–10295, end exclusive, in the original decoded publication. SHA-256: 5e1c0b3d217f160f93052c105a0324f8569b680cc8dcdd99a8855011438e45e9
Other AD Provisions
(i) Other AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
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 International
Validation Branch, send it to the attention of the person identified
in paragraph (j)(2) of this AD. Information may be emailed to: [email protected]. 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, International
Validation Branch, FAA; or the United Kingdom Civil Aviation
Authority (U.K. CAA); or BAE Systems (Operations) Limited's U.K. CAA
Design Organization Approval (DOA). If approved by the DOA, the
approval must include the DOA-authorized signature.
Exact source excerpt. Text positions 10295–11551, end exclusive, in the original decoded publication. SHA-256: ddc9efca6f05f0a4add425d6b2c093a77fae708ba2e0097f281e384bc829d1ff
Additional Information
(j) Additional Information
(1) Refer to U.K. CAA AD G-2022-0002, dated February 11, 2022,
for related information. This U.K. CAA AD may be found in the AD
docket at regulations.gov under Docket No. FAA-2022-1053.
(2) For more information about this AD, contact Todd Thompson,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3228; email [email protected].
Exact source excerpt. Text positions 11551–12017, end exclusive, in the original decoded publication. SHA-256: a2b4761fb43a69ff4591e0f694f98fb42ee33859b3539d4782990c9e6d9f6f23
Material Incorporated by Reference
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) BAE Systems (Operations) Limited Modification Service
Bulletin SB.22-072-36262A, dated September 14, 2021.
(ii) [Reserved]
(3) 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
[email protected]; website baesystems.com/Businesses/RegionalAircraft/index.htm.
(4) 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 12017–13397, end exclusive, in the original decoded publication. SHA-256: 73e9fcbb240392a3004ba0733d57cc32ed5b845f34b609f605a5c211a4fec73f
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2022-23-07 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: dbac88fab7eaae57874c4e7128900cdd629411eb02d5b36327675c94e407cbd8. Source manifest: 20eb04732cccce717e318ddf81e12588e636beef5746746b957c339bdf19b0ab.
Official source · 2022-11-30
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 87, Number 229 (Wednesday, November 30, 2022)]
[Rules and Regulations]
[Pages 73446-73448]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-26083]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1053; Project Identifier MCAI-2022-00200-T;
Amendment 39-22234; AD 2022-23-07]
RIN 2120-AA64
Airworthiness Directives; BAE Systems (Operations) Limited
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
BAE Systems (Operations) Limited Model BAe 146 series airplanes. This
AD was prompted by a finding that when the autopilot is engaged, the
architecture of the autopilot system does not automatically disconnect
the autopilot in response to pilot application of a pitch input or when
the electric pitch trim switch on either pilot control wheel is
operated. This AD requires modifying the autopilot engagement circuit.
The FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective January 4, 2023.
[[Page 73447]]
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 4,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1053; 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 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 [email protected]; website baesystems.com/Businesses/RegionalAircraft/index.htm.
<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
regulations.gov under Docket No. FAA-2022-1053.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone 206-231-3228; email
[email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all BAE Systems
(Operations) Limited Model BAe 146 series airplanes. The NPRM published
in the Federal Register on August 22, 2022 (87 FR 51271). The NPRM was
prompted by AD G-2022-0002, dated February 11, 2022, issued by United
Kingdom Civil Aviation Authority (U.K. CAA), which is the aviation
authority for the United Kingdom (referred to after this as the MCAI).
The MCAI states that when the autopilot is engaged, the architecture of
the autopilot system does not automatically disconnect the autopilot in
response to pilot application of a pitch input or when the electric
pitch trim switch on either pilot control wheel is operated.
In the NPRM, the FAA proposed to require modifying the autopilot
engagement circuit. The FAA is issuing this AD to address continued
autopilot engagement after flightcrew input to disengage the autopilot,
which could lead to reduced controllability of the airplane.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-1053.
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
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 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 minor editorial changes, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.
Related Service Information Under 1 CFR Part 51
BAE Systems (Operations) Limited has issued Modification Service
Bulletin SB.22-072-36262A, dated September 14, 2021. This service
information describes procedures for modifying the autopilot engagement
circuit, including the wiring, relay, and certain module blocks. 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
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
130 work-hours x $85 per hour = $11,050...................... $2,124 $13,174 $263,480
----------------------------------------------------------------------------------------------------------------
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
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
[[Page 73448]]
under the criteria of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2022-23-07 BAE Systems (Operations) Limited Amendment 39-22234;
Docket No. FAA-2022-1053; Project Identifier MCAI-2022-00200-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 4, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all BAE Systems (Operations) Limited Model
BAe 146-100A, -200A, and -300A 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 a finding that when the autopilot is
engaged, the architecture of the autopilot system does not
automatically disconnect the autopilot in response to pilot
application of a pitch input or when the electric pitch trim switch
on either pilot control wheel is operated. The FAA is issuing this
AD to address continued autopilot engagement after flightcrew input
to disengage the autopilot, which could lead to reduced
controllability of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Modification
Within 12 months after the effective date of this AD, modify the
autopilot engagement circuit in accordance with the Accomplishment
Instructions of BAE Systems (Operations) Limited Modification
Service Bulletin SB.22-072-36262A, dated September 14, 2021.
(h) No Reporting Requirement
Although BAE Systems (Operations) Limited Modification Service
Bulletin SB.22-072-36262A, dated September 14, 2021, specifies to
submit certain information to the manufacturer, this AD does not
include that requirement.
(i) Other AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
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 International
Validation Branch, send it to the attention of the person identified
in paragraph (j)(2) of this AD. Information may be emailed to: [email protected]. 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, International
Validation Branch, FAA; or the United Kingdom Civil Aviation
Authority (U.K. CAA); or BAE Systems (Operations) Limited's U.K. CAA
Design Organization Approval (DOA). If approved by the DOA, the
approval must include the DOA-authorized signature.
(j) Additional Information
(1) Refer to U.K. CAA AD G-2022-0002, dated February 11, 2022,
for related information. This U.K. CAA AD may be found in the AD
docket at regulations.gov under Docket No. FAA-2022-1053.
(2) For more information about this AD, contact Todd Thompson,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3228; email [email protected].
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) BAE Systems (Operations) Limited Modification Service
Bulletin SB.22-072-36262A, dated September 14, 2021.
(ii) [Reserved]
(3) 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
[email protected]; website baesystems.com/Businesses/RegionalAircraft/index.htm.
(4) 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on November 1, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-26083 Filed 11-29-22; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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