Published 2022-12-05 · Federal Register document 2022-26354
Airworthiness Directives; Bombardier, Inc., Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-2A12 airplanes. This AD was prompted by the investigation of erroneous radio altimeter data that was displayed on an in-service airplane. It was revealed that certain radio altimeter coaxial cables used by the radio altimeter systems, in the aft fuselage equipment bay, were damaged. This AD requires replacing affected radio altimeter coaxial cables. 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[379]
- Raw source SHA-256
- c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2022-23-03
- Effective date printed in this edition
- 2023-01-09
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective January 9, 2023.
Exact source excerpt. Text positions 10497–10586, end exclusive, in the original decoded publication. SHA-256: 24193d2c188d2a5d3e0bc37ec6edc306265ee96cf217183a37b61cf722c7d3e8
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10586–10615, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-700-2A12
airplanes, serial numbers 70006 through 70053 inclusive,
certificated in any category.
Exact source excerpt. Text positions 10615–10783, end exclusive, in the original decoded publication. SHA-256: 2d1bebdf4a6e7ee2083b3f34a2af84e1cc76941cb008106577e638157fba4e3d
Subject
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
Exact source excerpt. Text positions 10783–10865, end exclusive, in the original decoded publication. SHA-256: 0542bcd80d4296f1663f9c1a9ee6733c7599b54c556ebcd2abd87a0d6015adff
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by the investigation of erroneous radio
altimeter data that was displayed on an in-service airplane. It was
revealed that certain radio altimeter coaxial cables in the aft
fuselage equipment bay were damaged. The FAA is issuing this AD to
address damage to or kinks in the radio altimeter coaxial cables,
which could lead to signal loss or degradation, and possibly un-
annunciated loss of terrain awareness warning system aural cues
during approach.
Exact source excerpt. Text positions 10865–11370, end exclusive, in the original decoded publication. SHA-256: f909a5ed475f04b0b951c360cb768c53c16dae338294532b12fef1b3603d4f36
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11370–11472, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Replacement of Radio Altimeter Coaxial Cables
(g) Replacement of Radio Altimeter Coaxial Cables
Within 12 months after the effective date of this AD, replace
affected radio altimeter coaxial cables, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 700-91-
7502, Revision 02, dated April 5, 2022, except as specified in
paragraph (h) of this AD.
Exact source excerpt. Text positions 11472–11813, end exclusive, in the original decoded publication. SHA-256: 9cebbb13e0c9fa5aa014c8391cdfa23a6ce2da40e723477458c064548b70a80a
No Reporting Requirement
(h) No Reporting Requirement
Although Bombardier Service Bulletin 700-91-7502, Revision 02,
dated April 5, 2022, specifies to submit certain information to the
manufacturer, this AD does not include that requirement.
Exact source excerpt. Text positions 11813–12039, end exclusive, in the original decoded publication. SHA-256: 16fc681a83dc6606e3e7398a6f5576644bb55a1c874e3c6221e57683fcbd9c38
Credit for Previous Actions
(i) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using the service information identified in
Bombardier Service Bulletin 700-91-7502, dated February 6, 2020; or
Bombardier Service Bulletin 700-91-7502, Revision 01, dated August
31, 2020.
Exact source excerpt. Text positions 12039–12421, end exclusive, in the original decoded publication. SHA-256: 4435fa42b161bd93539c4679b6e999200f37af55e82b04ebf3ba4ea202e549a0
Other FAA AD Provisions
(j) Other FAA 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 certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300. 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
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
Exact source excerpt. Text positions 12421–13662, end exclusive, in the original decoded publication. SHA-256: 3e7bdfd994a7359db6c6f10111acf325abc2226ab1254ef079b265d35cebcb3f
Additional Information
(k) Additional Information
(1) Refer to TCCA AD CF-2021-45, dated December 7, 2021, for
related information. This TCCA AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2022-0677.
(2) For more information about this AD, contact Thomas Niczky,
Aerospace Engineer, Avionics and Electrical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7347; email [email protected].
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (l)(3) and (4) of this AD.
Exact source excerpt. Text positions 13662–14302, end exclusive, in the original decoded publication. SHA-256: 678771e7ed7eea5d6cdac65bdd96ce4437b3cff797469a9b442729372fb6c449
Material Incorporated by Reference
(l) 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) Bombardier Service Bulletin 700-91-7502, Revision 02, dated
April 5, 2022.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 1-514-855-2999; email bombardier.com">ac.yul@aero.bombardier.com; internet
bombardier.com.
(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.
[[Page 74301]]
Exact source excerpt. Text positions 14302–15614, end exclusive, in the original decoded publication. SHA-256: 701d9c343efdd4565f169f58c27be42eb480c3e3597bac34b8aabdf805ee34dd
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 2022-23-03 · 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: ee37808d509eeaad0fe48905dc21244fd56d8b046239a5316417ed3096f227b6. Source manifest: 42c97c38f8ae8f8d37ba2b2877c7150365860a51d2b1e9b02d675f0d62f6efe0.
Official source · 2022-12-05
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 232 (Monday, December 5, 2022)]
[Rules and Regulations]
[Pages 74298-74301]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-26354]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0677; Project Identifier MCAI-2021-01378-T;
Amendment 39-22230; AD 2022-23-03]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD-700-2A12 airplanes. This AD was
prompted by the investigation of erroneous radio altimeter data that
was displayed on an in-service airplane. It was revealed that certain
radio altimeter coaxial cables used by the radio altimeter systems, in
the aft fuselage equipment bay, were damaged. This AD requires
replacing affected radio altimeter coaxial cables. The FAA is issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective January 9, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 9,
2023.
[[Page 74299]]
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-0677; 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 Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 1-514-855-2999; email bombardier.com">ac.yul@aero.bombardier.com; internet
bombardier.com.
<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-2022-0677.
FOR FURTHER INFORMATION CONTACT: Thomas Niczky, Aerospace Engineer,
Avionics and Electrical Systems Section, FAA, New York ACO Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7347;
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 certain Bombardier,
Inc., Model BD-700-2A12 airplanes. The NPRM published in the Federal
Register on June 13, 2022 (87 FR 35686). The NPRM was prompted by AD
CF-2021-45, dated December 7, 2021, 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 the erroneous radio
altimeter data was displayed on an in-service airplane. It was revealed
that certain radio altimeter coaxial cables in the aft fuselage
equipment bay had been reported damaged (from radio altimeters A28 and
A29 to antennas), due their light weight construction, and their
proximity to the access door on the eBay. The damage to or kinks in the
radio altimeter coaxial cables, if not corrected, could lead to signal
loss or degradation, and possibly un-annunciated loss of terrain
awareness warning system aural cues during approach.
In the NPRM, the FAA proposed to require replacing affected radio
altimeter coaxial cables. The FAA is issuing this AD to address the
unsafe condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-0677.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from Netjets. The following presents the
comment received on the NPRM and the FAA's response to the comment.
Request To Refer to Updated Bombardier Service Bulletin
Netjets stated Bombardier Service Bulletin 700-91-7502, Revision
02, dated April 5, 2022, has been released. The FAA infers that Netjets
is requesting that the proposed AD be revised to refer to Bombardier
Service Bulletin 700-91-7502, Revision 02, dated April 5, 2022 (the
proposed AD refers to Bombardier Service Bulletin 700-91-7502, Revision
01, dated August 31, 2020, as the appropriate source of service
information).
The FAA agrees with the request. Bombardier Service Bulletin 700-
91-7502, Revision 02, dated April 5, 2022, adds minor changes that do
not affect the substantive requirements proposed in the NPRM, including
adding references to an advisory document and the MCAI AD. The FAA has
revised this final rule to refer to Bombardier Service Bulletin 700-91-
7502, Revision 02, dated April 5, 2022. The FAA has also revised
paragraph (i) of this AD to provide credit for actions done in
accordance with Bombardier Service Bulletin 700-91-7502, Revision 01,
dated August 31, 2020.
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 minor editorial changes,
and any other changes described previously, 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
The FAA reviewed Bombardier Service Bulletin 700-91-7502, Revision
02, dated April 5, 2022. This service information specifies procedures
for replacing affected radio altimeter coaxial cables. The replacement
includes removing the existing radio altimeter coaxial cables,
replacing with new coaxial cables, installing new clamps to accommodate
the coaxial bend radius along the coaxial routing, and re-routing new
radio altimeter coaxial cables from the wing to fuselage fairing, in
the left and right aft fuselage, and in the aft fuselage belly fairing.
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 27 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
----------------------------------------------------------------------------------------------------------------
70 work-hours x $85 per hour = $5,950........................ $13,808 $19,758 $533,466
----------------------------------------------------------------------------------------------------------------
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this AD may be covered under warranty, thereby reducing the cost impact
on affected operators.
[[Page 74300]]
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 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:
2022-23-03 Bombardier, Inc.: Amendment 39-22230; Docket No. FAA-
2022-0677; Project Identifier MCAI-2021-01378-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 9, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-700-2A12
airplanes, serial numbers 70006 through 70053 inclusive,
certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
(e) Unsafe Condition
This AD was prompted by the investigation of erroneous radio
altimeter data that was displayed on an in-service airplane. It was
revealed that certain radio altimeter coaxial cables in the aft
fuselage equipment bay were damaged. The FAA is issuing this AD to
address damage to or kinks in the radio altimeter coaxial cables,
which could lead to signal loss or degradation, and possibly un-
annunciated loss of terrain awareness warning system aural cues
during approach.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Replacement of Radio Altimeter Coaxial Cables
Within 12 months after the effective date of this AD, replace
affected radio altimeter coaxial cables, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 700-91-
7502, Revision 02, dated April 5, 2022, except as specified in
paragraph (h) of this AD.
(h) No Reporting Requirement
Although Bombardier Service Bulletin 700-91-7502, Revision 02,
dated April 5, 2022, specifies to submit certain information to the
manufacturer, this AD does not include that requirement.
(i) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using the service information identified in
Bombardier Service Bulletin 700-91-7502, dated February 6, 2020; or
Bombardier Service Bulletin 700-91-7502, Revision 01, dated August
31, 2020.
(j) Other FAA 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 certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300. 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
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(k) Additional Information
(1) Refer to TCCA AD CF-2021-45, dated December 7, 2021, for
related information. This TCCA AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2022-0677.
(2) For more information about this AD, contact Thomas Niczky,
Aerospace Engineer, Avionics and Electrical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7347; email [email protected].
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (l)(3) and (4) of this AD.
(l) 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) Bombardier Service Bulletin 700-91-7502, Revision 02, dated
April 5, 2022.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 1-514-855-2999; email bombardier.com">ac.yul@aero.bombardier.com; internet
bombardier.com.
(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.
[[Page 74301]]
Issued on October 27, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-26354 Filed 12-2-22; 8:45 am]
BILLING CODE 4910-13-P
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