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2021-24-13 DAHER AEROSPACE (TYPE CERTIFICATE PREVIOUSLY HELD BY SOCATA):
Amendment 39-21834; Docket No. FAA-2021-0778; Project Identifier 2019-CE-062-AD.

(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective January 12, 2022.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to  Daher Aerospace (type certificate  previously held
    by SOCATA) Model  TBM 700 airplanes,  serial numbers 1106  and larger,
    certificated in any category.

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 2130,  Cabin Pressure Con-
    trol System.

(e) UNSAFE CONDITION

    This AD was prompted by mandatory continuing airworthiness information
    (MCAI)  originated  by an  aviation  authority of  another  country to
    identify and correct an unsafe  condition on an aviation product.  The
    MCAI describes the  unsafe condition as  a non-conforming dump  switch
    ejecting from its  slot. The FAA  is issuing this  AD to prevent  dump
    switches ejecting from their slots,  which, in case of smoke/fumes  in
    the cabin,  could prevent  evacuation of  the smoke/fumes.  The unsafe
    condition, if  not addressed,  could result  in excessive  flight crew
    workload and injury to airplane occupants.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REQUIRED ACTIONS

    Within 12  months after  the effective  date of  this AD, inspect each
    dump switch  part number  (P/N) 7388475012  to determine  if a seal is
    installed, as depicted in Figure 3 of Daher Aerospace Service Bulletin
    SB 70-271-21, Revision 1, dated November 2019.

(1) If a seal is installed,  no further action  is required  by this para-
    graph.

(2) If a seal is not installed,  within 12 months after the effective date
    of  this AD,  modify  the  dump switch  in accordance  with steps  (2)
    through (5) of the Description of Accomplishment Instructions in Daher
    Aerospace Service  Bulletin SB  70-271-21, Revision  1, dated November
    2019.

(h) PARTS INSTALLATION PROVISION

    As of the effective date of this AD,  do not install a dump switch P/N
    7388475012 on any airplane  unless the switch has been modified as de-
    scribed in Daher Aerospace Service Bulletin SB 70-271-21,  Revision 1,
    dated November 2019. Removal of a dump switch from an airplane and re-
    installation of that dump switch on the same airplane  within the same
    maintenance visit is not an installation  for  purposes  of this para-
    graph.

(i) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) 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 local Flight Standards District Office, as
    appropriate. If  sending information  directly to  the manager  of the
    International  Validation  Branch, send  it  to the  attention  of the
    person identified in paragraph (j)(1) of this AD or email:  9-AVS-AIR-
    730-AMOC@faa.gov.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking  a principal inspector,  the manager of  the local
    flight standards district office/certificate holding district office.

(j) RELATED INFORMATION

(1) For more information about this AD,  contact Gregory Johnson, Aviation
    Safety Engineer,  FAA,  General Aviation & Rotorcraft Section,  Inter-
    national Validation Branch,  901  Locust,  Room  301,  Kansas City, MO
    64106;  phone: (720) 626-5462;  fax: (816) 329-4090;  email:  gregory.
    johnson@faa.gov.

(2) Refer to European Union Aviation Safety Agency  (EASA)  AD  2019-0306,
    dated December  18, 2019,  for more  information. You  may examine the
    EASA AD in the  AD docket at https://www.regulations.gov  by searching
    for and locating it in Docket No. FAA-2021-0778.

(k) 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 the AD specifies otherwise.

(i) Daher Aerospace Service Bulletin SB 70-271-21 Revision 1, dated Novem-
    ber 2019.

(ii) [Reserved]

(3) For service information identified in this AD, contact Daher Aerospace
    Inc., Pompano Beach Airpark, 601 NE 10 Street, Pompano Beach, FL 33060
    phone: (954) 893-1400; website: https://www.tbm.aero.

(4) You may view this service information at the FAA,  Airworthiness Prod-
    ucts Section, Operational Safety  Branch, 901 Locust, Kansas  City, MO
    64106. For  information on  the availability  of this  material at the
    FAA, call (816) 329-4148.

(5) You may view this service information  that is incorporated  by refer-
    ence 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.

Issued on November 17, 2021.  Gaetano A. Sciortino,  Deputy  Director  for
Strategic Initiatives,  Compliance & Airworthiness Division, Aircraft Cer-
tification Service.

FOR FURTHER INFORMATION CONTACT: Gregory Johnson, Aviation Safety Engineer
FAA,  General  Aviation  &  Rotorcraft  Section,  International Validation
Branch, 901 Locust, Room 301, Kansas City, MO 64106; phone (720) 626-5462;
fax: (816) 329-4090; email: gregory.johnson@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0778; Project Identifier 2019-CE-062-AD; Amendment
39-21834; AD 2021-24-13]
RIN 2120-AA64

Airworthiness Directives; Daher Aerospace (Type Certificate
Previously Held by SOCATA) Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Daher Aerospace (type certificate previously held by SOCATA)
Model TBM 700 airplanes. This AD was prompted by mandatory continuing
airworthiness information (MCAI) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as a non-
conforming dump switch ejecting from its slot. This AD requires
modifying certain dump switches. The FAA is issuing this AD to address
the unsafe condition on these products.

DATES: This AD is effective January 12, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 12,
2022.

ADDRESSES: For service information identified in this final rule,
contact Daher Aerospace Inc., Pompano Beach Airpark, 601 NE 10 Street,
Pompano Beach, FL 33060; phone: (954) 893-1400; website: https://
www.tbm.aero. You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 901 Locust,
Kansas City, MO 64106. For information on the availability of this
material at the FAA, call (816) 329-4148. It is also available at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2021-0778.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0778; 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
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: Gregory Johnson, Aviation Safety
Engineer, FAA, General Aviation & Rotorcraft Section, International
Validation Branch, 901 Locust, Room 301, Kansas City, MO 64106; phone:
(720) 626-5462; fax: (816) 329-4090; email: gregory.johnson@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain serial-numbered
Daher Aerospace (type certificate previously held by SOCATA) Model TBM
700 airplanes. The NPRM published in the Federal Register on September
14, 2021 (86 FR 51033). The NPRM was prompted by MCAI originated by the
European Union Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union. EASA issued AD 2019-
0306, dated December 18, 2019 (referred to after this as ``the MCAI''),
to address the unsafe condition on certain serial-numbered Daher
Aerospace (formerly SOCATA) Model TBM 700 airplanes. The MCAI states:

It has been determined that, in certain conditions, an affected
switch [dump switch part number 7388475012 without a seal] may eject
from its slot. Investigations identified the root cause in a non-
conformity of the affected switch.
This condition, if not corrected, could, in case of smoke/fumes
in the cabin, prevent evacuation of the smoke/fumes, possibly
resulting in excessive flight crew workload and/or injury to
aeroplane occupants.
To address this potential unsafe condition, DAHER AEROSPACE
issued the [service bulletin] SB to provide modification
instructions.
For the reasons described above, this [EASA] AD requires
modification of the affected parts by installation of a seal, and
introduces requirements for installation of a dump switch.

You may examine the MCAI in the AD docket at https://www.regulations.
gov by searching for and locating Docket No. FAA-2021-0778.

Discussion of Final Airworthiness Directive

Comments

The FAA received no comments on the NPRM or on the determination of
the costs.

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 and
service information 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 these products. This AD is adopted as proposed in the
NPRM.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Daher Aerospace Service Bulletin SB 70-271-21,
Revision 1, dated November 2019. The service information contains
procedures for modifying each dump switch part number 7388475012 by
removing the two indicator light units, installing a seal, installing a
thin layer of grease, and installing the two indicator lights. 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 150 airplanes of U.S.
registry. The FAA also estimates that it would take about 1 work-hour
per airplane and require parts costing $800 to comply with the
modification required by this AD. The average labor rate is $85 per
work-hour.
Based on these figures, the FAA estimates the inspection cost of
this AD on U.S. operators to be $132,750 or $885 per airplane.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some 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 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 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

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: