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2021-03-18 DASSAULT AVIATION: Amendment 39-21421; Docket No. FAA-2021-0024; Project Identifier MCAI-2021-00105-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective February 22, 2021.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies  to all Dassault  Aviation Model FALCON  7X airplanes,
    certificated in any category.

    NOTE 1 TO PARAGRAPH (C): Model FALCON 7X airplanes include those  that
    have embodied Dassault  modification (mod)  M1000  (commercially known
    as  Falcon 8X) in production.

(d) SUBJECT

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

(e) REASON

    This AD was prompted by a report of deviations concerning the assembly
    and  overhaul of  certain crew  oxygen mask  stowage boxes,  including
    incorrect  application of  Loctite 222  thread-locker on  the  fitting
    sensor screws. The FAA is issuing this AD to address such  deviations,
    which could  lead to  blocked oxygen  supply flow  to flight deck crew
    oxygen masks, which,  in combination with  in-flight depressurization,
    flight  deck  smoke, or  a  smoke evacuation  procedure,  may lead  to
    flightcrew hypoxia  and loss  of useful  consciousness and  consequent
    loss of control of the airplane.

(f) COMPLIANCE

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

(g) REQUIREMENTS

    Except  as specified  in paragraph  (h) of  this AD:  Comply with  all
    required actions and compliance times specified in, and in  accordance
    with, European Union Aviation  Safety Agency (EASA) Emergency  AD 2021
    -0036-E, dated January 25, 2021 (EASA Emergency AD 2021-0036-E).

(h) EXCEPTIONS TO EASA EMERGENCY AD 2021-0036-E

(1) Where EASA Emergency AD 2021-0036-E refers to its effective date, this
    AD requires using the effective date of this AD.

(2) Where paragraph (2) of EASA Emergency AD 2021-0036-E specifies actions
    if  "any  discrepancy  is detected,"  for this  AD a  "discrepancy" is
    defined as an inability to clearly hear oxygen flowing out of the mask
    during a functional test or see that the yellow blinker on the stowage
    box does not illuminate.

(3) Although the service information referenced in EASA Emergency AD 2021-
    0036-E specifies that certain actions may be accomplished by a  pilot,
    this AD does not allow that provision.

(4) The "Remarks" section of EASA Emergency AD 2021-0036-E does not  apply
    to this AD.

(i) NO REPORTING REQUIREMENT

    Although the service information referenced in EASA Emergency AD 2021-
    0036-E specifies to submit  certain  information to the  manufacturer,
    this AD does not include that requirement.

(j) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS): The Manager, Large Aircraft
    Section, 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 Large  Aircraft
    Section, International Validation Branch, send it to the attention  of
    the person identified in paragraph (k) of this AD. Information may  be
    emailed  to:  9-AVS-AIR-730-AMOC@faa.gov.  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, Large  Aircraft
    Section, International  Validation Branch,  FAA; or  EASA; or Dassault
    Aviation's EASA Design Organization Approval (DOA). If approved by the
    DOA, the approval must include the DOA-authorized signature.

(k) RELATED INFORMATION

    For more information about  this AD, contact Tom  Rodriguez, Aerospace
    Engineer,  Large  Aircraft Section,  International  Validation Branch,
    FAA, 2200  South 216th  St., Des  Moines, WA  98198; telephone and fax
    206-231-3226; email tom.rodriguez@faa.gov.

(l) MATERIAL INCORPORATED BY REFERENCE

(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) European Union Aviation Safety Agency (EASA) Emergency AD 2021-0036-E,
    dated January 25, 2021.

(ii) [Reserved]

(3) For EASA Emergency AD 2021-0036-E, contact the  EASA, Konrad-Adenauer-
    Ufer 3,  50668 Cologne,  Germany; telephone  +49 221  8999 000;  email
    ADs@easa.europa.eu;  Internet  www.easa.europa.eu. You  may  find this
    EASA AD on the EASA website at https://ad.easa.europa.eu.

(4) You may view this material 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. This material may be found in the AD docket on the internet
    at https://www.regulations.gov  by searching  for and  locating Docket
    No. FAA-2021-0024.

(5) You may view  this material that is  incorporated by reference at  the
    National Archives and  Records Administration (NARA).  For information
    on   the    availability   of    this   material    at   NARA,   email
    fedreg.legal@nara.gov,  or  go  to:   https://www.archives.gov/federal
    -register/cfr/ibr-locations.html.

Issued  on  February  1,  2021.  Lance  T.  Gant,  Director,  Compliance &
Airworthiness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,  Large
Aircraft Section, International Validation  Branch, FAA, 2200 South  216th
St.,  Des  Moines,  WA  98198;  telephone  and  fax  206-231-3226;   email
tom.rodriguez@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2021-0024; Project Identifier MCAI-2021-00105-T;
Amendment 39-21421; AD 2021-03-18]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Dassault Aviation Model FALCON 7X airplanes. This AD was prompted by a
report of deviations concerning the assembly and overhaul of certain
crew oxygen mask stowage boxes, including incorrect application of a
certain thread-locker on the fitting sensor screws. This AD requires an
inspection of certain crew oxygen mask stowage boxes for discrepancies,
and replacement if necessary, as specified in a European Union Aviation
Safety Agency (EASA) AD, which is incorporated by reference. The FAA is
issuing this AD to address the unsafe condition on these products.

DATES: This AD becomes effective February 22, 2021.

The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of February 22,
2021.

The FAA must receive comments on this AD by March 22, 2021.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:

Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow
the instructions for submitting comments.

Fax: 202-493-2251.

Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.

Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.

For material incorporated by reference (IBR) in this AD, contact
the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49
221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu.
You may find this IBR material on the EASA website at https://ad.easa.europa.eu. You
may view this IBR material 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 in the AD
docket on the internet at https://www.regulations.gov by searching for
and locating Docket No. FAA-2021-0024.

Examining the AD Docket


You may examine the AD docket on the internet at https://www.regulations.gov
by searching for and locating Docket No. FAA-2021-
0024; 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 AD, any comments received, and other information. The street
address for Docket Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226;
email tom.rodriguez@faa.gov.

SUPPLEMENTARY INFORMATION:

Background


The EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA Emergency AD 2021-0036-E, dated January
25, 2021 (EASA Emergency AD 2021-0036-E) (also referred to as the
Mandatory Continuing Airworthiness Information, or the MCAI), to
correct an unsafe condition for all Dassault Aviation Model FALCON 7X
airplanes.

This AD was prompted by a report of deviations concerning the
assembly and overhaul of certain crew oxygen mask stowage boxes,
including incorrect application of Loctite 222 thread-locker on the
fitting sensor screws. The FAA is issuing this AD to address such
deviations, which could lead to blocked oxygen supply flow to flight
deck crew oxygen masks. In combination with in-flight depressurization,
flight deck smoke, or a smoke evacuation procedure, this lack of oxygen
may lead to flightcrew hypoxia and loss of useful consciousness and
consequent loss of control of the airplane. See the MCAI for additional
background information.

Related Service Information Under 1 CFR Part 51


EASA Emergency AD 2021-0036-E describes procedures for an
inspection (test) of crew oxygen mask stowage boxes having part number
CSD30-005-X-X (`X' can represent any alphanumeric value) for
discrepancies (an inability to clearly hear oxygen flowing out of the
mask during a functional test or see that the yellow blinker on the
stowage box does not illuminate), and replacement.

This material 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.

FAA's Determination


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 the State of Design Authority,
the FAA has been notified of the unsafe condition described in the MCAI
referenced above. The FAA is issuing this AD because the FAA evaluated all
pertinent information and determined the unsafe condition exists and is
likely to exist or develop on other products of the same type design.

Requirements of This AD


This AD requires accomplishing the actions specified in EASA
Emergency AD 2021-0036-E described previously, as incorporated by
reference, except for any differences identified as exceptions in the
regulatory text of this AD.

Explanation of Required Compliance Information


In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA initially worked with Airbus and EASA to develop a
process to use certain EASA ADs as the primary source of information
for compliance with requirements for corresponding FAA ADs. The FAA has
since coordinated with other manufacturers and civil aviation
authorities (CAAs) to use this process. As a result, EASA Emergency AD
2021-0036-E is incorporated by reference in this final rule. This AD,
therefore, requires compliance with EASA Emergency AD 2021-0036-E in
its entirety, through that incorporation, except for any differences
identified as exceptions in the regulatory text of this AD. Using
common terms that are the same as the heading of a particular section
in the EASA AD does not mean that operators need comply only with that
section. For example, where the AD requirement refers to "all required
actions and compliance times," compliance with this AD requirement is
not limited to the section titled "Required Action(s) and Compliance
Time(s)" in the EASA AD. Service information specified in EASA
Emergency AD 2021-0036-E that is required for compliance with EASA
Emergency AD 2021-0036-E is available on the internet at
https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0024.

FAA's Justification and Determination of the Effective Date


An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies waiving notice and comment prior to adoption of this rule
because deviations during the assembly and overhaul of certain crew
oxygen mask stowage boxes could lead to blocked oxygen supply flow to
flight deck crew oxygen masks, which, in combination with in-flight
depressurization, flight deck smoke, or a smoke evacuation procedure,
may lead to flightcrew hypoxia and loss of useful consciousness and
consequent loss of control of the airplane. In addition, the compliance
time for the required action is shorter than the time necessary for the
public to comment and for publication of the final rule. Therefore, the
FAA finds good cause that notice and opportunity for prior public
comment are impracticable. In addition, for the reasons stated above,
the FAA finds that good cause exists for making this amendment
effective in less than 30 days.

Comments Invited


The FAA invites you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
ADDRESSES. Include "Docket No. FAA-2021-0024; Project Identifier MCAI-
2021-01005-T" at the beginning of your comments. The most helpful
comments reference a specific portion of the final rule, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this final rule because of those comments.

Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this final rule.

Confidential Business Information


CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this AD contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this AD, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as "PROPIN." The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this AD. Submissions containing CBI should be sent to Tom
Rodriguez, Aerospace Engineer, Large Aircraft Section, International
Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax 206-231-3226; email tom.rodriguez@faa.gov. Any
commentary that the FAA receives which is not specifically designated
as CBI will be placed in the public docket for this rulemaking.

Regulatory Flexibility Act (RFA)


The requirements of the RFA do not apply when an agency finds good
cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and
comment. Because the FAA has determined that it has good cause to adopt
this rule without notice and comment, RFA analysis is not required.

Costs of Compliance


The FAA estimates that this AD affects 133 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs for Required Actions

LABOR COST
PARTS COST
COST PER PRODUCT
COST ON U.S. OPERATORS
1 work-hours x $85 per hour = $85
$0
$85
$11,305

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

LABOR COST
PARTS COST
COST PER PRODUCT
Up to 3 work-hours x $85 per hour = Up to $255 (per mask stowage box).
$8,427
Up to $8,682.

According to the manufacturer, some or all of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected operators. The FAA does not control warranty coverage for
affected operators. As a result, the FAA has included all known costs
in the cost estimate.

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


The FAA determined that 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, and

(2) Will not affect intrastate aviation in Alaska.

List of Subjects in 14 CFR Part 39


Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of 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


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]


2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive: