- Effective
- August 19, 2022
- Published
- July 15, 2022 · 87 FR 42312–42315
- Issued
- June 27, 2022
- Models
- BD-700-1A10, BD-700-1A11
- Data sheet
- TCDST00003NY
- Registered aircraft
- 522 matched by model
- Product
- Aircraft · Large airplane
- ATA chapter
- 35 · Oxygen
- Amendment
- 39-22112
- Docket
- FAA-2022-0470
- Project
- MCAI-2021-01002-T
- Issued as
- Final rule
Unofficial copy from the Federal Register XML, document 2022-15190. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 359 KB | 5f32070b…bdc5167 | 2022-15190.pdf on govinfo.gov |
| Federal Register XML | 23 KB | 09e83c6b…1595560 | 2022-15190.xml on federalregister.gov |
| FAA DRS HTML | 50 KB | 66ffc31f…8412387 | FAA DRS (API key needed) |
On this page
Summary
The FAA is adopting a new airworthiness directive (AD) for all Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This AD was prompted by reports that some oxygen box assemblies had their piston ejected during the mask deployment test. This AD requires a one-time inspection of each passenger oxygen box dual manifold assembly to find and replace affected parts. This AD also prohibits installing affected parts. The FAA is issuing this AD to address the unsafe condition on these products.
The airworthiness directive
2022-14-07 Bombardier, Inc.: Amendment 39-22112; Docket No. FAA-2022-0470; Project Identifier MCAI-2021-01002-T.
(a) Effective Date
PDF page 2This airworthiness directive (AD) is effective August 19, 2022.
(b) Affected ADs
PDF page 2None.
(c) Applicability
PDF page 2This AD applies to all Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes, certificated in any category.
(d) Subject
PDF page 2Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Unsafe Condition
PDF page 2This AD was prompted by reports that some passenger oxygen box dual manifold had their piston ejected during the mask deployment test due to a non-conformity in manufacturing. The FAA is issuing this AD to address a possible in-service piston ejection when used for emergency descent, smoke, or fire that may result in a high rate of oxygen leakage, which could prematurely deplete the oxygen for all passengers.
(f) Compliance
PDF page 2Comply with this AD within the compliance times specified, unless already done.
(g) Definition
PDF page 2An affected part is a passenger oxygen box assembly having a dual manifold assembly having part number 100-009-39 and a lot and serial number specified in figure 1 to paragraph (g) of this AD.
[graphic omitted; see the official PDF]
(h) Required Actions
PDF page 2Within the applicable compliance time specified in paragraph (h)(1) or (2) of this AD: Inspect each passenger oxygen box dual manifold assembly to determine if it is an affected part, as defined in paragraph (g) of this AD, and replace any affected part in accordance with paragraph 2.B. of the Accomplishment Instructions of the applicable Bombardier service bulletin specified in figure 2 to paragraph (h) of this AD. Replace any affected part before further flight.
(1) For airplanes having serial numbers 9771, 9779, 9784, 9788 through 9824 inclusive, 9853 through 9857 inclusive, and 9859 through 9876 inclusive, within 4 months after the effective date of this AD.
(2) For airplane having serial numbers 9877 through 9879 inclusive, and 60001 through 60042 inclusive, within 30 months after the effective date of this AD.
[graphic omitted; see the official PDF]
(i) Parts Installation Prohibition
PDF page 2As of the effective date of this AD, no person may install an affected part as defined in paragraph (g) of this AD, on any airplane.
(j) Credit for Previous Actions
PDF page 2This paragraph provides credit for actions required by paragraph (h) of this AD, if those actions were performed before the effective date of this AD using the service information specified in paragraphs (j)(1) through (7) of this AD, as applicable.
(1) Bombardier Service Bulletin 700-35-5004, dated December 10, 2018.
(2) Bombardier Service Bulletin 700-35-5004, Revision 01, dated November 29, 2019.
(3) Bombardier Service Bulletin 700-35-6004, dated December 10, 2018.
(4) Bombardier Service Bulletin 700-35-6004, Revision 01, dated January 16, 2019.
(5) Bombardier Service Bulletin 700-35-6004, Revision 02, dated April 5, 2019.
(6) Bombardier Service Bulletin 700-35-6004, Revision 03, dated May 31, 2019.
(7) Bombardier Service Bulletin 700-35-6004, Revision 04, dated November 29, 2019.
(k) Other FAA AD Provisions
PDF page 2The 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.
(l) Related Information
PDF page 4(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) TCCA AD CF-2021-30, dated September 7, 2021, for related information. This MCAI may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0470.
(2) For more information about this AD, contact Elizabeth Dowling, 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 9-avs-nyaco-cos@faa.gov.
(3) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (m)(4) and (5) of this AD.
(m) Material Incorporated by Reference
PDF page 4(1) The Director of the Federal Register approved the incorporation by reference (IBR) 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 700-35-5004, Revision 02, dated August 27, 2021.
(ii) Bombardier Service Bulletin 700-35-5502, dated August 27, 2021.
(iii) Bombardier Service Bulletin 700-35-6004, Revision 05, dated August 27, 2021.
(iv) Bombardier Service Bulletin 700-35-6502, dated August 27, 2021.
(3) For service information identified in this AD, contact Bombardier Business Aircraft Customer Response Center, 400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada; telephone 514-855-2999; email ac.yul@aero.bombardier.com; 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 fr.inspection@nara.gov, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
This AD is effective August 19, 2022.
The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 19, 2022.
AddressesPage 1
For service information identified in this final rule, contact Bombardier Business Aircraft Customer Response Center, 400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada; telephone 514-855-2999; email ac.yul@aero.bombardier.com; internet https://www.bombardier.com. 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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0470.
For further information contactPage 1
Elizabeth Dowling, 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 9-avs-nyaco-cos@faa.gov.
BackgroundPage 1
Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued TCCA AD CF-2021-30, dated September 7, 2021 (TCCA AD CF-2021-30) (also referred to after this as the Mandatory Continuing Airworthiness Information, or the MCAI), to correct an unsafe condition for all Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. You may examine the MCAI in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0470.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. The NPRM published in the Federal Register on April 26, 2022 (87 FR 24476). The NPRM was prompted by reports that some oxygen box assemblies had their piston ejected during the mask deployment test. The NPRM proposed to require a one-time inspection of each passenger oxygen box dual manifold assembly to find and replace affected parts. The NPRM also proposed to prohibit installing affected parts. The FAA is issuing this AD to address a possible in-service piston ejection when used for emergency descent, smoke, or fire that may result in a high rate of oxygen leakage, which could prematurely deplete the oxygen for all passengers. See the MCAI for additional background information.
CommentsPage 1
The FAA received no comments on the NPRM or on the determination of the cost to the public.
ConclusionPage 1
The FAA reviewed the relevant data and determined that air safety requires adopting this AD as proposed. 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. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products.
Related Service Information Under 1 CFR Part 51Page 1
Bombardier, Inc., has issued the following service information.
• Service Bulletin 700-35-5004, Revision 02, dated August 27, 2021.
• Service Bulletin 700-35-5502, dated August 27, 2021.
• Service Bulletin 700-35-6004, Revision 05, dated August 27, 2021.
• Service Bulletin 700-35-6502, dated August 27, 2021.
This service information describes procedures for inspecting each passenger oxygen box dual manifold assembly to find affected parts, and replacing affected parts. These documents are distinct because they apply to different airplane configurations.
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 CompliancePage 2
The FAA estimates that this AD affects 308 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:
| Labor cost | Parts cost | Cost per product | Cost on U.S. operators |
|---|---|---|---|
| 1 work-hour × $85 per hour = $85 | $0 | $85 | $26,180 |
The FAA estimates the following costs to do any necessary on-condition actions 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:
| Labor cost | Parts cost | Cost per product |
|---|---|---|
| Up to 34 work-hours × $85 per hour = $2,890 | Up to $1,700 | Up to $4,590 |
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 RulemakingPage 2
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 findingsPage 2
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.
The amendmentPage 2
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
Adoption of the amendmentPage 2
1. The authority citation for part 39 continues to read as follows:
2. The FAA amends § 39.13 by adding the following new airworthiness directive:
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 522
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1997 | 1 |
|---|---|
| 1998 | 2 |
| 1999 | 16 |
| 2000 | 19 |
| 2001 | 13 |
| 2002 | 8 |
| 2003 | 5 |
| 2004 | 13 |
| 2005 | 7 |
| 2006 | 19 |
| 2007 | 19 |
| 2008 | 20 |
| 2009 | 19 |
| 2010 | 13 |
| 2011 | 21 |
| 2012 | 30 |
| 2013 | 31 |
| 2014 | 37 |
| 2015 | 24 |
| 2016 | 13 |
| 2017 | 15 |
| 2018 | 15 |
| 2019 | 6 |
| 2020 | 9 |
| 2021 | 6 |
| 2022 | 18 |
| 2023 | 25 |
| 2024 | 22 |
| 2025 | 22 |
| 2026 | 7 |
47 with no year recorded