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2021-22-07 UMLAUT ENGINEERING GMBH (PREVIOUSLY P3 ENGINEERING GMBH) HAFEX (HALON-FREE) HAND-HELD FIRE EXTINGUISHERS: Amendment 39-21780; Docket No. FAA-2021-0882; Project Identifier MCAI-2021-00929-Q.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective November 18, 2021.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Umlaut Engineering GmbH (previously P3  Engineering
    GmbH)   HAFEX   (Halon-free)   hand-held   fire   extinguisher   (fire
    extinguisher)  part  numbers  (P/Ns)  P3APP003010A,  P3APP003010B, and
    P3APP003010C. An affected fire  extinguisher may be installed  on, but
    not limited to, the following aircraft, certificated in any category:

Note 1  to the  introductory text  of paragraph  (c): According  to Umlaut
service  information,  the fire  extinguisher  P/N is  on  the RFID  label
located on the lever of the fire extinguisher.

(1) Airbus SAS Model A318 series, A319 series,  A320 series,  A321 series,
    A330-200 series, A330-200 freighter series,  A330-300 series, A330-800
    series, A330-900 series,  A340-200 series,  A340-300 series,  A340-500
    series, A340-600 series, and A350-941, AS350-1041, A380-841, A380-842,
    and A380-861 airplanes;

(2) Airbus Helicopters Model AS332C, AS332C1,  AS332L,  AS332L1,  AS332L2,
    AS-365N2, AS 365 N3, EC 155B, EC155B1,  EC225LP,  SA330J, SA-365C, SA-
    365C1, SA-365C2, SA-365N, SA-365N1, and SA-366G1 helicopters;

(3) Airbus Helicopters Deutschland  GmbH  (AHD)  Model  EC135P1,  EC135P2,
    EC135P2+, EC135P3, EC135T1 EC135T2, EC135T2+, EC135T3, MBB-BK 117 A-1,
    MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2, MBB-BK
    117 C-1, MBB-BK 117 C-2, MBB-BK 117 D-2 and MBB-BK 117 D-3 helicopters

Note 2 to paragraph (c)(3):  Helicopters with an EC135P3H designation  are
Model EC135P3 helicopters; and helicopters with an MBB-BK 117C-2e designa-
tion are Model MBB-BK 117C-2 helicopters.

(4) ATR-GIE Avions de Transport Regional Model ATR42-200, ATR42-300, ATR42
    -320, ATR42-500, ATR72-101, ATR72-102,  ATR72-201,  ATR72-202,  ATR72-
    211, ATR72-212, and ATR72-212A airplanes;

(5) Leonardo S.p.a.  Model AB139, AB412, AB412 EP, AW139, AW169, and AW189
    helicopters; and

(6) PZL Swidnik S.A. Model PZL W-3A helicopters.

(d) SUBJECT

    Joint Aircraft Service Component (JASC) Code: 2622, Fire Bottle, Port-
    able.

(e) UNSAFE CONDITION

    This AD defines the unsafe condition as an impaired fire extinguisher,
    which could prevent proper extinguishing  of  a  fire  in the cabin or
    cockpit, and result in subsequent damage to the aircraft and injury to
    the occupants.

(f) COMPLIANCE

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

(g) REQUIRED ACTIONS

(1) Within 30 days after the effective date of this AD  and  thereafter at
    intervals not to exceed 6 months:

(i) Inspect each fire extinguisher identified  in  the  introductory para-
    graph of paragraph (c) of this AD  by following the Accomplishment In-
    structions,  paragraph 3.2.C., steps 1. through 5. (but not steps 5.a.
    and b.), of Umlaut Vender Service Bulletin (VSB) Doc. No. P3VSB000003,
    Issue C, dated August 3, 2021 (P3VSB000003, Issue C).

(ii) If the safety pin  does  not  touch  the valve head (there is a gap),
     continue to inspect the fire extinguisher by following the Accomplish
     -ment Instructions,  paragraph 3.2.C.,  steps 6. through 8.  (but not
     steps 8.a. and b.), of P3VSB000003, Issue C.

(iii) If the lever moves back up  into  its  previous position  on its own
      (there is a gap), before further flight, remove the fire extinguish-
      er from service.

(2) As of the effective date of this AD,  for  a fire extinguisher identi-
    fied in the introductory text  of paragraph (c) of this  AD, installed
    on  any  aircraft  that has  not  been  in operation  for  30  or more
    consecutive days, or if it  cannot be determined how long  an aircraft
    has not been  in operation, before  further flight, and  thereafter at
    intervals not to exceed 6  months, accomplish the actions required  by
    paragraphs (g)(1)(i) through  (iii) of this  AD. For purposes  of this
    AD, an engine run-up does not count as aircraft operation.

(3) As of the effective date of this AD,  do not install  as a replacement
    part or as an original installation  a fire extinguisher identified in
    the introductory text of paragraph (c) of this AD on any aircraft, un-
    less the actions required  by  paragraphs  (g)(1)(i)  through (iii) of
    this AD have been accomplished.

(h) CREDIT FOR PREVIOUS ACTIONS

    This paragraph provides credit for the initial instance of the actions
    required by paragraph (g)(1) of this AD  if those actions  were accom-
    plished before the effective date of this AD using Umlaut VSB Doc. No.
    P3VSB000003,  Issue  A,  dated  May 10, 2021,  or  Umlaut VSB Doc. No.
    P3VSB000003, Issue B, dated July 14, 2021.

(i) SPECIAL FLIGHT PERMITS

    A special flight permit  may  be  permitted provided that there are no
    passengers onboard.

(j) 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 (k)(1)  of this AD. Information may  be
    emailed to: 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.

(k) RELATED INFORMATION

(1) For more information about this AD, contact Hal Jensen, Aerospace Eng-
    ineer, Operational Safety Branch, Compliance & Airworthiness Division,
    FAA,  950 L'Enfant Plaza N SW,  Washington, DC 20024;  telephone (202)
    267-9167; email hal.jensen@faa.gov.

(2) Umlaut VSB Doc. No. P3VSB000003, Issue A, dated May 10, 2021 and Issue
    B, dated July 14, 2021,  which are not incorporated by reference, con-
    tain additional information about the subject of this AD. This service
    information is available at the contact information specified in para-
    graphs (l)(3) and (4) of this AD.

(3) The subject of this AD  is addressed in European Union Aviation Safety
    Agency (EASA) AD 2021-0185R1, dated August 11, 2021.  You may view the
    EASA AD  at https://www.regulations.gov  in  Docket No. FAA-2021-0882.

(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 the AD specifies otherwise.

(i) Umlaut Vendor Service Bulletin  Doc. No. P3VSB000003,  Issue C,  dated
    August 3, 2021.

(ii) [Reserved]

(3) For Umlaut service information  identified in this AD,  contact Umlaut
    Engineering GmbH, Blohmstrasse 12, 21079 Hamburg, Germany;  telephone:
    +49 (0) 551-19240; email: hafex@umlaut.com; or web: https://www.umlaut
    .com/hafex.

(4) You may view  this  service  information  at  the  FAA,  Office of the
    Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
    Fort Worth, TX 76177.  For information  on  the  availability  of this
    material at the FAA, call (817) 222-5110.

(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 October 15, 2021. Lance T Gant, Director, Compliance & Airworth-
iness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:  Hal Jensen,  Aerospace Engineer,  Opera-
tional Safety  Branch,  Compliance  &  Airworthiness  Division,  FAA,  950
L'Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267-9167; email
hal.jensen@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0882; Project Identifier MCAI-2021-00929-Q;
Amendment 39-21780; AD 2021-22-07]
RIN 2120-AA64

Airworthiness Directives; Umlaut Engineering GmbH (Previously P3
Engineering GmbH) HAFEX (Halon-Free) Hand-Held Fire Extinguishers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Umlaut Engineering GmbH (previously P3 Engineering GmbH) HAFEX
(Halon-free) hand-held fire extinguishers (fire extinguishers).This AD
was prompted by a report of a safety issue on certain fire
extinguishers, where certain environmental factors may prohibit the
discharge of the fire extinguisher. This AD requires repetitively
inspecting the fire extinguisher, and depending on the results,
removing the fire extinguisher from service. This AD also prohibits
installing an affected fire extinguisher unless it passes the required
inspections. The FAA is issuing this AD to address the unsafe condition
on these products.

DATES: This AD becomes effective November 18, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of November 18,
2021.
The FAA must receive comments on this AD by December 20, 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 service information identified in this final rule, contact
Umlaut Engineering GmbH, Blohmstrasse 12, 21079 Hamburg, Germany;
telephone: +49 (0) 551-19240; email: hafex@umlaut.com; or web: https://www.umlaut.com/hafex. You may view this service information at the FAA,
Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy.,
Room 6N-321, Fort Worth, TX 76177. For information on the availability
of this material at the FAA, call (817) 222-5110. Service information
that is incorporated by reference is also available at https://www.regulations.gov
by searching for and locating Docket No. FAA-2021-0882.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0882; 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,
European Union Aviation Safety Agency (EASA) AD, any comments received,
and other information. The street address for Docket Operations is
listed above.

FOR FURTHER INFORMATION CONTACT: Hal Jensen, Aerospace Engineer,
Operational Safety Branch, Compliance & Airworthiness Division, FAA,
950 L'Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267-
9167; email hal.jensen@faa.gov.

SUPPLEMENTARY INFORMATION:

Background

EASA, which is the Technical Agent for the Member States of the
European Union, has issued a series of ADs, the most recent being EASA
AD 2021-0185R1, dated August 11, 2021 (EASA AD 2021-0185R1), to correct
an unsafe condition for Umlaut Engineering GmbH, formerly P3
Engineering GmbH, fire extinguishers, having part number (P/N)
P3APP003010A, P/N P3APP003010B, or P/N P3APP003010C. EASA advises of a
safety issue that has been reported on the affected fire extinguishers
where certain environmental conditions may prohibit discharge of the
fire extinguisher. An investigation has determined that prolonged
exposure to high temperature conditions can dislodge the spindle in the
fire extinguisher head, subsequently making the fire extinguisher
inoperative. This condition, if not addressed, could prevent proper
extinguishing of a fire in the cabin or cockpit, possibly resulting in
damage to the aircraft and injury to the occupants.
Initially, EASA issued EASA AD 2021-0185, dated August 5, 2021
(EASA AD 2021-0185), which required repetitive inspections of each
affected fire extinguisher, and, depending on findings, replacement with a
serviceable part, as identified in EASA AD 2021-0185. EASA AD 2021-0185
also required inspection of an affected fire extinguisher prior to the
return to service of an aircraft with an affected part installed if the
aircraft had been parked or stored for a period of 30 days or more.
EASA AD 2021-0185 also required inspection of an affected fire
extinguisher prior to installation on any aircraft.
EASA later issued EASA AD 2021-0185R1 to revise EASA AD 2021-0185.
EASA AD 2021-0185R1 contains the same requirements, clarifies some
nomenclature, removes the Group definitions and references, and adds
Note 3 to clarify the parts prohibition.

FAA's Determination

These products have been approved by EASA and are approved for
operation in the United States. Pursuant to the FAA's bilateral
agreement with the European Union, EASA has notified the FAA about the
unsafe condition described in its AD. The FAA is proposing this AD
after evaluating all known relevant information and determining that
the unsafe condition described previously is likely to exist or develop
on other products.

Related Service Information Under 1 CFR Part 51


The FAA reviewed Umlaut Vendor Service Bulletin (VSB) Doc. No.
P3VSB000003, Issue C, dated August 3, 2021 (VSB P3VSB000003, Issue C).
This service information specifies procedures for identifying affected
fire extinguishers with P/N P3APP003010A, P3APP003010B, or
P3APP003010C. VSB P3VSB000003, Issue C, also specifies procedures for
inspecting and depending on the results, replacing affected fire
extinguishers.
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.

Other Related Service Information

The FAA also reviewed Umlaut VSB Doc. No. P3VSB000003, Issue A,
dated May 10, 2021 (VSB P3VSB000003, Issue A), and Issue B, dated July
14, 2021 (VSB P3VSB000003, Issue B). VSB P3VSB000003, Issue A, and VSB
P3VSB000003, Issue B, specify the same procedures as VSB P3VSB000003,
Issue C, except VSB P3VSB000003, Issue B updated the introductory
information of the Accomplishment Instructions, revised the
determination/evaluation of the aircraft/equipment history procedures,
and clarified reporting procedures; and VSB P3VSB000003, Issue C, adds
more in-depth inspection procedures.

AD Requirements

This AD requires within 30 days after the effective date of this
AD, and thereafter at intervals not to exceed 6 months, repetitively
inspecting an affected fire extinguisher and depending on the results,
removing the fire extinguisher from service. For an affected fire
extinguisher that is installed on any aircraft that has not been in
operation for 30 or more consecutive days, or if it cannot be
determined how long an aircraft has not been in operation, this AD
requires those actions before further flight and thereafter at
intervals not to exceed 6 months. This AD also prohibits installing, as
a replacement part or as an original installation, an affected fire
extinguisher on any aircraft unless it passes the required inspections.

Differences Between This AD and the EASA AD

If it cannot be determined how long an aircraft (with an affected
fire extinguisher installed) has not been in operation, this AD
requires inspecting each affected fire extinguisher before further
flight, whereas EASA AD 2021-0185R1 does not.

Justification for Immediate Adoption and Determination of the Effective
Date


Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
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 foregoing notice and comment prior to adoption of this rule
because the initial inspection of the fire extinguisher must be
accomplished within 30 days after the effective date of this AD.
Accordingly, notice and opportunity for prior public comment are
impracticable and contrary to the public interest pursuant to 5 U.S.C.
553(b)(3)(B).
In addition, the FAA finds that good cause exists pursuant to 5
U.S.C. 553(d) for making this amendment effective in less than 30 days,
for the same reasons the FAA found good cause to forego notice and
comment.

Comments Invited


The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
ADDRESSES. Include ``Docket No. FAA-2021-0882; Project Identifier MCAI-
2021-00929-Q'' 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 Hal
Jensen, Aerospace Engineer, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 950 L'Enfant Plaza N SW, Washington, DC
20024; telephone (202) 267-9167; email hal.jensen@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

The requirements of the Regulatory Flexibility Act (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 prior notice and
comment, RFA analysis is not required.

Costs of Compliance

The FAA estimates that this AD affects up to 2,850 fire
extinguishers installed on aircraft of U.S. registry. Labor rates are
estimated at $85 per work-hour. Based on these numbers, the FAA
estimates the following costs to comply with this AD.
Inspecting an affected fire extinguisher would take about 0.25
work-hour for an estimated cost of $21 per fire extinguisher, and up to
$59,850 for the U.S. fleet, per inspection cycle. Replacing an affected
fire extinguisher would take about 0.25 work-hour and parts would cost
about $1,200 for an estimated cost of $1,221 per fire extinguisher.

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, 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.

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: