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PROPOSED AD TRANSPORT CATEGORY AIRPLANES: Docket No. FAA-2020-0209; Product Identifier 2020-NM-004-AD.
(a) COMMENTS DUE DATE

    We must receive comments by May 14, 2020.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

(1) This AD  applies  to  the  Kidde Aerospace & Defense cargo fire extin-
    guisher halon bottles having part numbers  and  serial numbers identi-
    fied in Table 1 of the service information  identified  in  paragraphs
    (c)(1)(i) and (ii) of this AD.

(i) Kidde Aerospace & Defense Service Bulletin 473957-26-518 Rev 02, dated
    November 4, 2019

(ii) Kidde Aerospace & Defense  Service  Bulletin  473919-26-521,  Rev 02,
     dated November 7, 2019.

(2) These affected  cargo fire extinguisher halon bottles are installed on
    various transport category airplanes including,  but  not  limited to,
    the airplanes identified in paragraphs (c)(2)(i) through (vii) of this
    AD, certificated in any category.

(i) Airbus Canada Limited Partnership (type certificate previously held by
    C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Model
    BD-500-1A10 and BD-500-1A11 airplanes.

(ii) Airbus SAS Model A330-200 and A330-300 series airplanes.

(iii) The Boeing Company Model DC-9-81 (MD-81)  airplanes,  and  Model 737
      series airplanes.

(iv) Bombardier, Inc.,  Model CL-600-2B19  (Regional Jet Series 100 & 440)
     airplanes,  Model  CL-600-2C10  (Regional Jet Series  700, 701 & 702)
     airplanes, and Model CL-600-2C11 (Regional Jet Series 550) airplanes.

(v) De Havilland Aircraft of Canada Limited (type  certificate  previously
    held by Bombardier, Inc.) Model DHC-8-400 series airplanes.

(vi) Embraer S.A. Model ERJ 170-100 STD airplanes,  and  Model ERJ 190-100
     STD, -300, and -400 airplanes.

(vii) Saab AB, Saab Aeronautics (formerly known as Saab AB,  Saab Aeronau-
      tics) Model SAAB 2000 airplanes.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 26, Fire protection.

(e) UNSAFE CONDITION

    This AD was  prompted by a  report indicating that  certain cargo fire
    extinguisher  halon  bottles  had  low  charge  pressure.  Low  charge
    pressure of a  cargo fire extinguisher  halon bottle installed  in the
    cargo  compartment,  if  not addressed,  could result  in insufficient
    halon concentrations to extinguish a fire in the cargo compartment.

(f) COMPLIANCE

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

(g) DEFINITIONS

    For this AD,  the definitions specified  in  paragraphs (g)(1) through
    (3) of this AD apply.

(1) Group 1: Boeing Model 737-8 and 737-9 airplanes and Model 737-700, 737
    -800, and 737-900ER series airplanes.

(2) Group 2: Transport category airplanes  other than those  identified as
    group 1.

(3) Affected part: A cargo fire extinguisher halon bottle, manufactured by
    Kidde Aerospace & Defense, having a part number and serial number that
    is identified in the service information identified  in paragraphs (c)
    (1)(i) and (ii) of this AD.

Note 1 to paragraph (g)(3):  The  terms  "cargo  fire  extinguisher  halon
bottles" and "fire extinguishers" are used interchangeably  in this AD and
the service information identified  in  paragraphs (c)(1)(i)  and  (ii) of
this AD and in paragraphs (i)(1)(i) and (ii) of this AD.

(h) INSPECTION

    Within 24 months after the effective date of this AD, do an inspection
    to  determine the  part number  and serial  number of  the cargo  fire
    extinguisher  halon  bottles  installed in  the  cargo  compartment. A
    review of maintenance  records can be  done in lieu  of the inspection
    provided  the  part  number  and  serial  number  of  the  cargo  fire
    extinguisher halon  bottles can  be conclusively  determined from that
    review.

(i) REPLACEMENT

    If, during the inspection or records review required by paragraph  (h)
    of this AD, it is determined  that an affected part, as identified  in
    paragraph  (g)(3) of  this AD,  is installed,  before further  flight,
    replace  the  part with  a  serviceable part  in  accordance with  the
    applicable  service  information identified  in  paragraph (i)(1)  and
    (i)(2) of this AD.

(1) For group 1 airplanes as identified  in  paragraph (g)(1)  of this AD:
    The Accomplishment Instructions of the service information  identified
    in paragraph (c)(1)(i) of this AD,  or the service information identi-
    fied in paragraph (i)(1)(i) or (ii) of this AD, as applicable.

(i) Boeing Alert Requirements Bulletin 737-26A1150 RB, dated September 27,
    2019.

(ii) Boeing  Alert Requirements Bulletin 737-26A1151 RB,  dated  September
     27, 2019.

(2) For group 2 airplanes as identified in paragraph (g)(2)  of  this  AD:
    The Accomplishment Instructions of the service information  identified
    in paragraph (c)(1)(i) or (ii) of this AD, as applicable.

(j) PARTS INSTALLATION LIMITATION

    As of the effective date of this AD, no person may install on any air-
    plane an affected  part as identified  in paragraph (g)(3)  of this AD
    unless that part  has a circled  letter "G" stamped  at a distance  of
    approximately one inch from the  left edge of the placard,  indicating
    that the  cargo fire  extinguisher halon  bottle has  been tested  and
    refilled.

(k) SPECIAL FLIGHT PERMIT

    If low pressure is detected  or  a warning is displayed  in the flight
    deck,  special flight permits may be issued in accordance with  14 CFR
    21.197 and  21.199 to  operate the  airplane to  a location  where the
    cargo fire extinguisher halon bottles can be replaced or modified.

(l) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The  Manager,  Atlanta 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  local Flight  Standards District  Office, as
    appropriate. If  sending information  directly to  the manager  of the
    certification  office,  send  it  to  the  attention  of  the   person
    identified in paragraph (m)(1) of this AD.

(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.

(3) For  service  information  that  contains  steps  that  are labeled as
    Required for Compliance  (RC),  the provisions of paragraphs (l)(3)(i)
    and (ii) of this AD apply.

(i) The steps labeled as RC,  including substeps  under an RC step and any
    figures identified in an RC step, must be done to comply with the  AD.
    If a step or substep is  labeled "RC Exempt," then the RC  requirement
    is removed  from that  step or  substep. An  AMOC is  required for any
    deviations to RC steps, including substeps and identified figures.

(ii) Steps not labeled  as RC may be deviated  from using accepted methods
     in accordance with the  operator's maintenance or inspection  program
     without  obtaining  approval  of  an  AMOC,  provided  the  RC steps,
     including  substeps  and identified  figures,  can still  be  done as
     specified,  and  the  airplane  can  be  put  back  in  an  airworthy
     condition.

(m) RELATED INFORMATION

(1) For more information about this AD,  contact Samuel Belete,  Aerospace
    Engineer, Systems and Equipment Section, FAA, Atlanta ACO Branch, 1701
    Columbia Avenue, College Park, GA 30337; phone: 404-474-5580; fax: 404
    -474-5606; email: Samuel.Belete@faa.gov.

(2) For Boeing service information identified in this AD,  contact  Boeing
    Commercial Airplanes,  Attention:  Contractual & Data Services (C&DS),
    2600 Westminster Blvd.,  MC 110-SK57, Seal Beach, CA 90740-5600; tele-
    phone 562-797-1717; internet https://www.myboeingfleet.com.  For Kidde
    Aerospace & Defense service information identified in this AD, contact
    Kidde Aerospace & Defense,  4200 Airport Drive NW, Building B, Wilson,
    NC 27896-8630;  telephone 319-295-5000;  http://www.Kiddetechnologies.
    com/aviation.  You  may  view  this  service  information  at the FAA,
    Transport Standards Branch,  2200 South 216th St., Des Moines, WA. For
    information on the availability of this material at the FAA, call 206-
    231-3195.

Issued on March 23, 2020. Lance T. Gant, Director, Compliance & Airworthi-
ness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD by May 14, 2020.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0209; Product Identifier 2020-NM-004-AD]
RIN 2120-AA64

Airworthiness Directives; Kidde Aerospace & Defense

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for Kidde Aerospace & Defense cargo fire extinguisher halon bottles
installed on various transport category airplanes. This proposed AD was
prompted by a report indicating that certain cargo fire extinguisher
halon bottles installed in the cargo compartment had low charge
pressure. This proposed AD would require an inspection to determine the
part number and serial number of the cargo fire extinguisher halon
bottles and replacement of affected parts with serviceable parts. The
FAA is proposing this AD to address the unsafe condition on these
products.

DATES: The FAA must receive comments on this proposed AD by May 14,
2020.

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 Boeing service information identified in this NPRM, contact Boeing
Commercial Airplanes, Attention: Contractual & Data Services (C&DS),
2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone
562-797-1717; internet https://www.myboeingfleet.com. For Kidde
Aerospace & Defense service information identified in this NPRM contact
Kidde Aerospace & Defense, 4200 Airport Drive NW, Building B, Wilson, NC
27896-8630; telephone 319-295-5000; http://www.Kiddetechnologies.com/
aviation. You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For information
on the availability of this material at the FAA, call 206-231-3195.

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-2020-0209;
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 NPRM, the regulatory evaluation, any comments received, and other
information. The street address for Docket Operations is listed above.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Samuel Belete, Aerospace Engineer,
Systems and Equipment Section, FAA, Atlanta ACO Branch, 1701 Columbia
Avenue, College Park, GA 30337; phone: 404-474-5580; fax: 404-474-5606;
email: Samuel.Belete@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include "Docket No. FAA-2020-0209;
Product Identifier 2020-NM-004-AD" at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this NPRM. The FAA will
consider all comments received by the closing date and may amend this
NPRM because of those comments.

The FAA will post all comments received, without change, to https://www.
regulations.gov, including any personal information you provide.
The FAA will also post a report summarizing each substantive verbal
contact received about this NPRM.

Discussion

The FAA has received a report indicating that certain cargo fire
extinguisher halon bottles installed in the cargo compartment had low
charge pressure. An investigation revealed that a procedural change at
the manufacturer of the cargo fire extinguisher halon bottles resulted
in cargo fire extinguisher halon bottles being produced with lower than
required pressure. Indication of the low bottle pressure may not occur
until the bottles have been agitated from in-service use and a warning
is displayed in the flight deck. Low charge pressure of a cargo fire
extinguisher halon bottle installed in the cargo compartment, if not
addressed, could result in insufficient halon concentrations to
extinguish a fire in the cargo compartment.

Related Service Information Under 1 CFR Part 51

The FAA reviewed the following Boeing Alert Requirements Bulletins.
This service information describes procedures for an inspection to
determine the serial number of the cargo fire extinguisher halon bottle
having a certain part number and replacing affected parts with
serviceable parts. These documents are distinct since they apply to
different airplane models.

Alert Requirements Bulletin 737-26A1150 RB, dated
September 27, 2019.

Alert Requirements Bulletin 737-26A1151 RB, dated
September 27, 2019.

The FAA reviewed the following Kidde Aerospace & Defense service
information. This service information describes, among other actions,
procedures for replacing affected fire extinguishers (referred to as
"cargo fire extinguisher halon bottles" in this proposed AD) with
serviceable parts. These documents are distinct since they apply to
different airplane models.

Service Bulletin 473919-26-521, Rev 02, dated November 7, 2019.

Service Bulletin 473957-26-518, Rev 02, dated November 4, 2019.

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.

FAA's Determination

We are proposing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.

Proposed AD Requirements

This proposed AD would require accomplishing the actions specified
in the service information described previously, except as discussed
under "Differences Between this Proposed AD and the Service
Information." For information on the procedures, see this service
information at https://www.regulations.gov by searching for and
locating Docket No. FAA-2020-0209.

Differences Between This Proposed AD and the Service Information

The Kidde Aerospace & Defense service information specifies a
compliance time of 12 months to accomplish the replacement. The Boeing
service information specifies a compliance time of 24 months to
accomplish the replacement. In developing an appropriate compliance
time for this action, we considered the urgency associated with the
subject unsafe condition, the availability of required parts, and the
practical aspect of accomplishing the required replacement within a
period of time that corresponds to the normal scheduled maintenance for
most affected operators. In light of these items, we have determined
that a 24-month compliance time is appropriate.

Costs of Compliance

We estimate that this proposed AD affects 3,308 appliances
installed on, but not limited to, the transport category airplanes
identified in paragraphs (c)(2)(i) through (vii) of this AD. We
estimate the following costs to comply with this proposed AD:

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Inspection 2 work-hour x $85 per hour = $170
$0
$170
$562,360

We estimate the following costs to do any necessary replacements
that would be required based on the results of the proposed inspection.
We have no way of determining the number of aircraft that might need
replacements:

On-Condition Costs

Action
Labor cost
Parts cost
Cost per product
Replacement 4 work-hours x $85 per hour = $340
$25,305
$25,645

According to the cargo fire extinguisher halon bottles
manufacturer, some or all of the costs of this proposed AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all known costs in our 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.

We are 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

We determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 proposed
regulation:

(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 Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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 (AD):