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Published 2022-09-22 · Federal Register document 2022-20490

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 reports that significant water accumulation was discovered in the oxygen service compartment access panels of multiple airplanes. This AD requires modifying the oxygen service compartment door to introduce a means of water drainage. 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[306]
Raw source SHA-256
c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2022-17-11
Effective date printed in this edition
2022-10-27
Read 11 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) is effective October 27, 2022.

Exact source excerpt. Text positions 9631–9721, end exclusive, in the original decoded publication. SHA-256: 4c4a06c03ccb9bc0e2040b28ff949ed620a7cc6e19f6d3790e49fb1a2597ee1e

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 9721–9750, 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, certificated in any category, as identified in Bombardier 
Service Bulletin 700-52-7508, Revision 01, dated January 13, 2021.

Exact source excerpt. Text positions 9750–9967, end exclusive, in the original decoded publication. SHA-256: 46b442cc0d52b3ba58ae630f22231655b9ac223714769d77380b65fb7927697a

Subject
(d) Subject

    Air Transport Association (ATA) of America Code 35, Oxygen.

Exact source excerpt. Text positions 9967–10045, end exclusive, in the original decoded publication. SHA-256: beebdc11ca55a698e6bba23e8dc2d9b64bbafa16f2e35342201f0a7331ad0a62

Unsafe Condition
(e) Unsafe Condition

    This AD was prompted by reports that significant water 
accumulation was discovered in the oxygen service compartment of 
multiple airplanes. The FAA is issuing this AD to address water 
ingress through oxygen service compartment access panels. If not 
addressed, the freeze/thaw cycle of accumulated water may damage 
oxygen connections inside the compartment, leading to oxygen leakage 
and risk of fire in the presence of an ignition source.

Exact source excerpt. Text positions 10045–10517, end exclusive, in the original decoded publication. SHA-256: 07623f1f5dd5c2c8ed82a1cd2059ed116ee6a6853846d4e9c64bfb842e818117

Compliance
(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

Exact source excerpt. Text positions 10517–10619, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Required Actions
(g) Required Actions

    Within 25 months after the effective date of this AD: Modify the 
oxygen service compartment door in accordance with Part A of the 
Accomplishment Instructions of Bombardier Service Bulletin 700-52-
7508, Revision 1, dated January 13, 2021.

Exact source excerpt. Text positions 10619–10887, end exclusive, in the original decoded publication. SHA-256: ae4f1e528b0950f50b82bba83a5d86c521270949742935c0902f51e1a96c096e

Credit for Previous Actions
(h) 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 Bombardier Service Bulletin 700-52-7508, dated 
September 4, 2020.

Exact source excerpt. Text positions 10887–11150, end exclusive, in the original decoded publication. SHA-256: 28b9ad2d3269f3a8e95bad8b214df7f19c9dea97a43aa7dcd3cca1033834cefb

Other FAA AD Provisions
(i) 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; fax 516-794-5531. 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 11150–12409, end exclusive, in the original decoded publication. SHA-256: 8f3843fe94f632132b99220d3cb0585cffbb1bcc5e6ae9ee368f70cb95e164d2

Additional Information
(j) Additional Information

    (1) Refer to TCCA AD CF-2021-40, dated November 19, 2021, for 
related information. This TCCA AD may be found in the AD docket at 
www.regulations.gov under Docket No. FAA-2022-0681.
    (2) For more information about this AD, contact Gabriel Kim, 
Aerospace Engineer, Mechanical Systems and Administrative Services 
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; telephone 516-228-7300; email [email protected].

Exact source excerpt. Text positions 12409–12896, end exclusive, in the original decoded publication. SHA-256: f302bb2f442a52f7609642a8dcd1363d2b01b06d7014425590d68b5ed4fb37c3

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) Bombardier Service Bulletin 700-52-7508, Revision 1, dated 
January 13, 2021.
    (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 514-855-2999; email [email protected]; internet 
https://www.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.

Exact source excerpt. Text positions 12896–14178, end exclusive, in the original decoded publication. SHA-256: 92a52c6f90e5698f387ac27575e6e0029659bda4f5a895e34dec823daa5157d3

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 2022-17-11 · 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: c31b681f6d4e2f1e176c5e23ca23939b86cd588be0120a4bcb13a16c4a75d4b4. Source manifest: 6b5c87d8f674234572b2b95415d628723bc50bd59925fb62830cce5eb42aec9d.

Official source · 2022-09-22

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 183 (Thursday, September 22, 2022)]
[Rules and Regulations]
[Pages 57812-57814]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-20490]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0681; Project Identifier MCAI-2021-01292-T; 
Amendment 39-22149; AD 2022-17-11]
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 reports that significant water accumulation was discovered 
in the oxygen service compartment access panels of multiple airplanes. 
This AD requires modifying the oxygen service compartment door to 
introduce a means of water drainage. The FAA is issuing this AD to 
address the unsafe condition on these products.

DATES: This AD is effective October 27, 2022.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of October 27, 
2022.

ADDRESSES: 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 514-855-2999; email [email protected]; internet 
https://www.bombardier.com. You may view this service information at 
the FAA, Airworthiness Products Section,

[[Page 57813]]

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 www.regulations.gov under Docket No. 
FAA-2022-0681.

Examining the AD Docket

    You may examine the AD docket at www.regulations.gov under Docket 
No. FAA-2022-0681; 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.

FOR FURTHER INFORMATION CONTACT: Gabriel Kim, Aerospace Engineer, 
Mechanical Systems and Administrative Services Section, FAA, New York 
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
telephone 516-228-7300; 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 16, 2022 (87 FR 36272). The NPRM was prompted by AD 
CF-2021-40, dated November 19, 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 significant water 
accumulation was discovered in the oxygen service compartment access 
panels during production activities on multiple airplanes and that, if 
not corrected, the freeze/thaw cycle of accumulated water may damage 
oxygen connections inside the compartment, leading to oxygen leakage 
and risk of fire in the presence of an ignition source.
    In the NPRM, the FAA proposed to require modifying the oxygen 
service compartment door to introduce a means of water drainage. The 
FAA is issuing this AD to address the unsafe condition on these 
products.
    You may examine the MCAI in the AD docket at https://www.regulations.gov under Docket No. FAA-2022-0681.

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

    The FAA reviewed Bombardier Service Bulletin 700-52-7508, Revision 
1, dated January 13, 2021. This service information specifies 
procedures for, among other actions not specified in this AD, modifying 
the oxygen service compartment door to introduce a means of water 
drainage. The modification also includes a general visual inspection 
for damage of the oxygen access panel placard, and replacement of a 
damaged placard.
    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 40 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
----------------------------------------------------------------------------------------------------------------
4 work-hours x $85 per hour = $340...........................              $0             $340          $13,600
----------------------------------------------------------------------------------------------------------------

    The FAA estimates the following costs to do any necessary on-
condition action that would be required based on the results of any 
required actions. The FAA has no way of determining the number of 
aircraft that might need this on-condition action:

                 Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
                                                             Cost per
              Labor cost                   Parts cost        product
------------------------------------------------------------------------
1 work-hour x $85 per hour = $85......             $40             $125
------------------------------------------------------------------------

    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.

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

[[Page 57814]]

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:

2022-17-11 Bombardier, Inc.: Amendment 39-22149; Docket No. FAA-
2022-0681; Project Identifier MCAI-2021-01292-T.

(a) Effective Date

    This airworthiness directive (AD) is effective October 27, 2022.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Bombardier, Inc., Model BD-700-2A12 
airplanes, certificated in any category, as identified in Bombardier 
Service Bulletin 700-52-7508, Revision 01, dated January 13, 2021.

(d) Subject

    Air Transport Association (ATA) of America Code 35, Oxygen.

(e) Unsafe Condition

    This AD was prompted by reports that significant water 
accumulation was discovered in the oxygen service compartment of 
multiple airplanes. The FAA is issuing this AD to address water 
ingress through oxygen service compartment access panels. If not 
addressed, the freeze/thaw cycle of accumulated water may damage 
oxygen connections inside the compartment, leading to oxygen leakage 
and risk of fire in the presence of an ignition source.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Required Actions

    Within 25 months after the effective date of this AD: Modify the 
oxygen service compartment door in accordance with Part A of the 
Accomplishment Instructions of Bombardier Service Bulletin 700-52-
7508, Revision 1, dated January 13, 2021.

(h) 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 Bombardier Service Bulletin 700-52-7508, dated 
September 4, 2020.

(i) 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; fax 516-794-5531. 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.

(j) Additional Information

    (1) Refer to TCCA AD CF-2021-40, dated November 19, 2021, for 
related information. This TCCA AD may be found in the AD docket at 
www.regulations.gov under Docket No. FAA-2022-0681.
    (2) For more information about this AD, contact Gabriel Kim, 
Aerospace Engineer, Mechanical Systems and Administrative Services 
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; telephone 516-228-7300; 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) Bombardier Service Bulletin 700-52-7508, Revision 1, dated 
January 13, 2021.
    (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 514-855-2999; email [email protected]; internet 
https://www.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.

    Issued on August 10, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2022-20490 Filed 9-21-22; 8:45 am]
BILLING CODE 4910-13-P


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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T01:40:06.788729+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
287fbb8e11a7576019f6e8c597d77ef4edc0e87b07d012927d697fd01ce0529c
Text SHA-256
c31b681f6d4e2f1e176c5e23ca23939b86cd588be0120a4bcb13a16c4a75d4b4

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Coverage and limits

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.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.