Airworthiness Directives; Kidde Aerospace & Defense, 65193-65197 [2020-22725]
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Federal Register / Vol. 85, No. 200 / Thursday, October 15, 2020 / Rules and Regulations
revise the existing maintenance or inspection
program, as applicable, to incorporate Airbus
SAS A318/A319/A320/A321 Airworthiness
Limitations Section (ALS) Part 4, ‘‘System
Equipment Maintenance Requirements
(SEMR),’’ Revision 05, dated April 6, 2017.
The initial compliance time for doing the
revised actions is at the applicable time
specified in Airbus SAS A318/A319/A320/
A321 ALS Part 4, ‘‘System Equipment
Maintenance Requirements (SEMR),’’
Revision 05, dated April 6, 2017.
Accomplishing the maintenance or
inspection program revision required by
paragraph (i) of this AD terminates the
requirements of this paragraph.
(h) Retained No Alternative Actions or
Intervals, With a New Exception
This paragraph restates the requirements of
paragraph (h) of AD 2018–16–04, with a new
exception. Except as required by paragraph
(i) of this AD, after the maintenance or
inspection program has been revised as
required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions or
intervals are approved as an alternative
method of compliance (AMOC) in
accordance with the procedures specified in
paragraph (l)(1) of this AD.
(i) New Maintenance or Inspection Program
Revision
Except as specified in paragraph (j) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, European Union Aviation
Safety Agency (EASA) AD 2020–0034, dated
February 25, 2020 (‘‘EASA AD 2020–0034’’).
Accomplishing the maintenance or
inspection program revision required by this
paragraph terminates the requirements of
paragraph (g) of this AD.
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(j) Exceptions to EASA AD 2020–0034
(1) The requirements specified in
paragraphs (1) and (2) of EASA AD 2020–
0034 do not apply to this AD.
(2) Paragraph (3) of EASA 2020–0034
specifies revising ‘‘the AMP’’ within 12
months after its effective date, but this AD
requires revising the existing maintenance or
inspection program, as applicable, to
incorporate the ‘‘tasks and associated
thresholds and intervals’’ specified in
paragraph (3) of EASA 2020–0034 within 90
days after the effective date of this AD.
(3) The initial compliance time for doing
the tasks specified in paragraph (3) of EASA
2020–0034 is at the applicable ‘‘associated
thresholds’’ specified in paragraph (3) of
EASA AD 2020–0034, or within 90 days after
the effective date of this AD, whichever
occurs later.
(4) The provisions specified in paragraphs
(4) and (5) of EASA AD 2020–0034 do not
apply to this AD.
(5) The ‘‘Remarks’’ section of EASA AD
2020–0034 does not apply to this AD.
(k) New Provisions for Alternative Actions
and Intervals
After the maintenance or inspection
program has been revised as required by
paragraph (i) of this AD, no alternative
actions (e.g., inspections) and intervals are
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allowed unless they are approved in the
provisions of the ‘‘Ref. Publications’’ section
of EASA AD 2020–0034.
(l) 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 local Flight Standards
District 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 (m) of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov.
(i) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(ii) AMOCs approved previously for AD
2018–16–04 are approved as AMOCs for the
corresponding provisions of EASA AD 2020–
0034 that are required by paragraph (g) of this
AD.
(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 Airbus SAS’s EASA Design
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
(3) Required for Compliance (RC): For any
service information referenced in EASA AD
2020–0034 that contains RC procedures and
tests: Except as required by paragraph (l)(2)
of this AD, RC procedures and tests must be
done to comply with this AD; any procedures
or tests that are not identified as RC are
recommended. Those procedures and tests
that are not identified 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
procedures and tests identified as RC can be
done and the airplane can be put back in an
airworthy condition. Any substitutions or
changes to procedures or tests identified as
RC require approval of an AMOC.
(m) Related Information
(n) 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.
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(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(3) The following service information was
approved for IBR on November 19, 2020.
(i) European Union Aviation Safety Agency
(EASA) AD 2020–0034, dated February 25,
2020 (‘‘EASA AD 2020–0034’’).
(ii) [Reserved]
(4) The following service information was
approved for IBR on September 14, 2018 (83
FR 39581, August 10, 2018).
(i) Airbus SAS A318/A319/A320/A321
Airworthiness Limitations Section (ALS) Part
4, ‘‘System Equipment Maintenance
Requirements (SEMR),’’ Revision 05, dated
April 6, 2017.
(ii) [Reserved]
(5) For EASA AD 2019–0256, 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.
(6) For Airbus service information
identified in this AD, contact Airbus SAS,
Airworthiness Office—EIAS, Rond-Point
Emile Dewoitine No: 2, 31700 Blagnac Cedex,
France; telephone +33 5 61 93 36 96; fax +33
5 61 93 44 51; email account.airworth-eas@
airbus.com; internet https://www.airbus.com.
(7) 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–2020–0102.
(8) 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 October 2, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020–22758 Filed 10–14–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
For more information about this AD,
contact Sanjay Ralhan, Aerospace Engineer,
Large Aircraft Section, International
Validation, FAA, 2200 South 216th St., Des
Moines, WA 98198; telephone and fax 206–
231–3223; email sanjay.ralhan@faa.gov.
PO 00000
65193
[Docket No. FAA–2020–0209; Product
Identifier 2020–NM–004–AD; Amendment
39–21275; AD 2020–21–02]
RIN 2120–AA64
Airworthiness Directives; Kidde
Aerospace & Defense
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
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The FAA is adopting a new
airworthiness directive (AD) for Kidde
Aerospace & Defense cargo fire
extinguisher halon bottles installed on
various transport category airplanes.
This AD was prompted by a report
indicating that certain cargo fire
extinguisher halon bottles installed in
the cargo compartment had low charge
pressure. This AD requires 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 issuing
this AD to address the unsafe condition
on these products.
DATES: This AD is effective November
19, 2020.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of November 19, 2020.
ADDRESSES: For Boeing service
information identified in this final rule,
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 final rule
contact Kidde Aerospace & Defense,
4200 Airport Drive NW, Building B,
Wilson, NC 27896–8630; telephone
319–295–5000; https://
kiddetechnologies.com/aviation/. 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–2020–0209.
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SUMMARY:
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 final rule,
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:
Samuel Belete, Aerospace Engineer,
Systems and Equipment Section, FAA,
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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:
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to Kidde Aerospace & Defense
cargo fire extinguisher halon bottles
installed on various transport category
airplanes. The NPRM published in the
Federal Register on March 30, 2020 (85
FR 17507). The NPRM was prompted by
a report indicating that certain cargo fire
extinguisher halon bottles installed in
the cargo compartment had low charge
pressure. The NPRM proposed to
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.
Comments
The FAA gave the public the
opportunity to participate in developing
this final rule. The following presents
the comments received on the NPRM
and the FAA’s response to each
comment.
Support for the NPRM
Boeing concurred with the content of
the NPRM. United Airlines agreed with
the intent of the NPRM.
Request To Reduce the Compliance
Time
The Air Line Pilots Association,
International (ALPA) requested that the
compliance time specified in the
proposed AD be reduced from 24
months to 12 months. The commenter
stated that a compliance time of 12
months was specified in the Kidde
Aerospace service information.
The FAA disagrees with the
commenter’s request. The preamble of
the NPRM included an explanation
regarding the compliance time. As
stated in the NPRM, the Kidde
Aerospace & Defense service
information specifies a compliance time
of 12 months to do the inspection and
accomplish the replacement, and the
Boeing service information specifies a
compliance time of 24 months to
accomplish the replacement. In
developing an appropriate compliance
time for this action, the FAA considered
the urgency associated with the subject
unsafe condition, the availability of
required parts, and the practical aspects
of accomplishing the required
replacement within a period of time that
corresponds to the normal scheduled
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maintenance for most affected operators.
In light of these items, the FAA
determined that a 24-month compliance
time is appropriate and adequate to
address the unsafe condition. The FAA
has not revised this AD in regard to this
issue.
Request To Provide Detailed
Information for Bottle Test and Refill
Southwest Airlines requested that
paragraphs (g), (h), and (i) of the
proposed AD be revised to provide, or
refer to, detailed instructions on how to
test and refill cargo fire extinguisher
halon bottles prior to marking them
with a ‘‘G’’ stamp and returning them to
service. The commenter stated that it
understood the intent of the NPRM was
to have the unsafe condition removed
from operational airplanes by having
affected cargo fire extinguisher halon
bottles removed and not reinstalled
until the halon bottles had been tested,
refilled, and marked with a ‘‘G’’ stamp.
The commenter suggested that these
actions could be accomplished via
standard airplane maintenance manual
(AMM) processes instead of using the
procedures in the Boeing service
information that was specified in the
proposed AD.
The FAA does not agree with the
commenter’s request. The information
provided in paragraphs (g), (h), and (i)
of this AD is specific and complete
enough to address the unsafe condition.
The affected cargo fire extinguisher
halon bottles are installed on various
transport category airplanes, and as
such, referring to specific AMMs is not
practical. Furthermore, the FAA notes
that only halon bottles having certain
serial numbers are affected and need to
be replaced. There are a significant
number of cargo fire extinguisher halon
bottles with serial numbers that are not
affected by the requirements of this AD
and that do not need to be removed and
tested. Operators have the option of
installing a halon bottle with a serial
number that is not affected by the
requirements of this AD, or installing a
halon bottle that has been refurbished
by an authorized party. If operators
establish a different procedure to
refurbish affected cargo fire extinguisher
halon bottles, they can apply for an
alternative method of compliance by
using the procedures described in
paragraph (l) of this AD. The FAA has
not revised this AD in regard to this
issue.
Explanation of Change to
Manufacturer’s Name Specified in This
Final Rule
The FAA has revised paragraph
(c)(2)(iv) of this AD to identify the
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manufacturer name as MHI RJ Aviation
UL (instead of Bombardier, Inc.), as
published in the most recent type
certificate data sheet for the affected
models.
Conclusion
The FAA reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting this
final rule with the change described
previously and minor editorial changes.
The FAA has determined that these
minor changes:
• Are consistent with the intent that
was proposed in the NPRM for
addressing the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Related IBR Material 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 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.
Costs of Compliance
The FAA estimates that this 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. The
FAA estimates the following costs to
comply with this AD:
ESTIMATED COSTS
Action
Labor cost
Inspection ...............................
2 work-hours × $85 per hour = $170 .....................................
The FAA estimates the following
costs to do any necessary replacements
Cost per
product
Parts cost
that would be required based on the
results of the inspection. The FAA has
$0
Cost on U.S.
operators
$170
$562,360
no way of determining the number of
aircraft that might need replacements:
ON-CONDITION COSTS
Action
Labor cost
Replacement ....................................
4 work-hours × $85 per hour = $340 ........................................................
According to manufacturer for the
cargo fire extinguisher halon bottles,
some or all of the costs of this AD may
be covered under warranty, thereby
reducing the cost impact on affected
individuals. The FAA does not control
warranty coverage for affected
individuals. As a result, the FAA has
included all known costs in the cost
estimate.
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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
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Parts cost
$25,305
Cost per
product
$25,645
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.
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
Regulatory Findings
Adoption of the Amendment
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,
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List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
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2020–21–02 Transport Category Airplanes:
Amendment 39–21275; Docket No.
FAA–2020–0209; Product Identifier
2020–NM–004–AD.
(a) Effective Date
This AD is effective November 19, 2020.
(b) Affected ADs
None.
(c) Applicability
(1) This AD applies to the Kidde Aerospace
& Defense cargo fire extinguisher halon
bottles having part numbers and serial
numbers identified 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) MHI RJ Aviation ULC (type certificate
previously held by 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 Aeronautics) Model
SAAB 2000 airplanes.
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(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 already
done.
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(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 (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
identified 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 airplane 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
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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) of this
AD.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
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
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.
(n) 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) Boeing Alert Requirements Bulletin
737–26A1150 RB, dated September 27, 2019.
(ii) Boeing Alert Requirements Bulletin
737–26A1151 RB, dated September 27, 2019.
(iii) Kidde Aerospace & Defense Service
Bulletin 473919–26–521, Rev 02, dated
November 7, 2019.
(iv) Kidde Aerospace & Defense Service
Bulletin 473957–26–518, Rev 02, dated
November 4, 2019.
(3) 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
E:\FR\FM\15OCR1.SGM
15OCR1
Federal Register / Vol. 85, No. 200 / Thursday, October 15, 2020 / Rules and Regulations
Beach, CA 90740–5600; telephone 562–797–
1717; internet https://
www.myboeingfleet.com.
(4) 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; https://
kiddetechnologies.com/aviation/.
(5) 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.
(6) 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 fedreg.legal@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on October 1, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2020–22725 Filed 10–14–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–0457; Product
Identifier 2020–NM–039–AD; Amendment
39–21261; AD 2020–20–05]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is superseding
Airworthiness Directive (AD) 2018–25–
02 and AD 2019–23–01, which applied
to certain Airbus SAS Model A318
series airplanes; Model A319–111, –112,
–113, –114, –115, –131, –132, and –133
airplanes; Model A320–211, –212, –214,
–216, –231, –232, –233, –251N, –252N,
and –271N airplanes; and Model A321
series airplanes. Those ADs require
revising the existing maintenance or
inspection program, as applicable, to
incorporate new or more restrictive
maintenance requirements and/or
airworthiness limitations. This AD
requires revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations; as
specified in a European Union Aviation
Safety Agency (EASA) AD, which is
jbell on DSKJLSW7X2PROD with RULES
SUMMARY:
VerDate Sep<11>2014
15:57 Oct 14, 2020
Jkt 253001
incorporated by reference. This AD was
prompted by a determination that new
or more restrictive airworthiness
limitations are necessary and models
need to be added to the applicability.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective November
19, 2020.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of November 19, 2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain other publication listed in
this AD as of January 9, 2020 (84 FR
66579, December 5, 2019).
ADDRESSES: For the EASA material
identified in this AD that will be
incorporated by reference (IBR), 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.
For the Airbus material that is
incorporated by reference, contact
Airbus SAS, Airworthiness Office—
EIAS, Rond-Point Emile Dewoitine No:
2, 31700 Blagnac Cedex, France;
telephone +33 5 61 93 36 96; fax +33 5
61 93 44 51; email account.airwortheas@airbus.com; internet https://
www.airbus.com.
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–2020–
0457.
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–
0457; 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,
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:
Sanjay Ralhan, Aerospace Engineer,
Large Aircraft Section, International
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
65197
Validation Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
telephone and fax 206–231–3223; email
sanjay.ralhan@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The EASA, which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2020–0036R1, dated June 24, 2020
(‘‘EASA AD 2020–0036R1’’) (also
referred to as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for all Airbus SAS Model A318 series
airplanes; Model A319–111, –112, –113,
–114, –115, –131, –132, –133, –151N,
and –153N airplanes; Model A320–211,
–212, –214, –215, –216, –231, –232,
–233, –251N, –252N, –253N, –271N,
–272N, and –273N airplanes; and Model
A321 series airplanes. EASA AD 2020–
0036R1 revised EASA AD 2020–0036,
dated February 26, 2020 (‘‘EASA AD
2020–0036’’) (which the FAA referred to
as the appropriate source of service
information for accomplishing the
actions specified in the notice of
proposed rulemaking (NPRM)), and
superseded EASA AD 2018–0288
(which corresponds to FAA AD 2019–
23–01 (AD 2019–23–01, Amendment
39–19794 (84 FR 66579, December 5,
2019) (‘‘AD 2019–23–01’’)). Model
A320–215 airplanes are not certificated
by the FAA and are not included on the
U.S. type certificate data sheet; this AD
therefore does not include those
airplanes in the applicability.
The FAA issued a NPRM to amend 14
CFR part 39 to supersede AD 2019–23–
01, for certain Airbus SAS Model A318
series airplanes; A319–111, –112, –113,
–114, –115, –131, –132, and –133
airplanes; A320–211, –212, –214, –216,
–231, –232, –233, –251N, –252N, and
–271N airplanes; and A321 series
airplanes. AD 2019–23–01 required
revising the existing maintenance or
inspection program, as applicable, to
incorporate new or more restrictive
airworthiness limitations. AD 2019–23–
01 required airworthiness limitations
that are newer or more restrictive than
those specified in AD 2018–25–02,
Amendment 39–19513 (83 FR 62690,
December 6, 2018) (‘‘AD 2018–25–02’’).
AD 2019–23–01 specified that
accomplishing the revision required by
paragraph (i) of AD 2019–23–01
terminated all requirements of AD
2018–25–02. The NPRM published in
the Federal Register on June 1, 2020 (85
FR 33046). The NPRM was prompted by
a determination that new or more
restrictive airworthiness limitations are
necessary and models need to be added
E:\FR\FM\15OCR1.SGM
15OCR1
Agencies
[Federal Register Volume 85, Number 200 (Thursday, October 15, 2020)]
[Rules and Regulations]
[Pages 65193-65197]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-22725]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0209; Product Identifier 2020-NM-004-AD; Amendment
39-21275; AD 2020-21-02]
RIN 2120-AA64
Airworthiness Directives; Kidde Aerospace & Defense
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
[[Page 65194]]
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
Kidde Aerospace & Defense cargo fire extinguisher halon bottles
installed on various transport category airplanes. This AD was prompted
by a report indicating that certain cargo fire extinguisher halon
bottles installed in the cargo compartment had low charge pressure.
This AD requires 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 issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective November 19, 2020.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of November 19,
2020.
ADDRESSES: For Boeing service information identified in this final
rule, 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 final rule contact Kidde Aerospace &
Defense, 4200 Airport Drive NW, Building B, Wilson, NC 27896-8630;
telephone 319-295-5000; https://kiddetechnologies.com/aviation/. 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-2020-
0209.
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 final rule, 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: 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: [email protected].
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 Kidde Aerospace &
Defense cargo fire extinguisher halon bottles installed on various
transport category airplanes. The NPRM published in the Federal
Register on March 30, 2020 (85 FR 17507). The NPRM was prompted by a
report indicating that certain cargo fire extinguisher halon bottles
installed in the cargo compartment had low charge pressure. The NPRM
proposed to 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.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comments
received on the NPRM and the FAA's response to each comment.
Support for the NPRM
Boeing concurred with the content of the NPRM. United Airlines
agreed with the intent of the NPRM.
Request To Reduce the Compliance Time
The Air Line Pilots Association, International (ALPA) requested
that the compliance time specified in the proposed AD be reduced from
24 months to 12 months. The commenter stated that a compliance time of
12 months was specified in the Kidde Aerospace service information.
The FAA disagrees with the commenter's request. The preamble of the
NPRM included an explanation regarding the compliance time. As stated
in the NPRM, the Kidde Aerospace & Defense service information
specifies a compliance time of 12 months to do the inspection and
accomplish the replacement, and the Boeing service information
specifies a compliance time of 24 months to accomplish the replacement.
In developing an appropriate compliance time for this action, the FAA
considered the urgency associated with the subject unsafe condition,
the availability of required parts, and the practical aspects 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, the FAA determined that a 24-month
compliance time is appropriate and adequate to address the unsafe
condition. The FAA has not revised this AD in regard to this issue.
Request To Provide Detailed Information for Bottle Test and Refill
Southwest Airlines requested that paragraphs (g), (h), and (i) of
the proposed AD be revised to provide, or refer to, detailed
instructions on how to test and refill cargo fire extinguisher halon
bottles prior to marking them with a ``G'' stamp and returning them to
service. The commenter stated that it understood the intent of the NPRM
was to have the unsafe condition removed from operational airplanes by
having affected cargo fire extinguisher halon bottles removed and not
reinstalled until the halon bottles had been tested, refilled, and
marked with a ``G'' stamp. The commenter suggested that these actions
could be accomplished via standard airplane maintenance manual (AMM)
processes instead of using the procedures in the Boeing service
information that was specified in the proposed AD.
The FAA does not agree with the commenter's request. The
information provided in paragraphs (g), (h), and (i) of this AD is
specific and complete enough to address the unsafe condition. The
affected cargo fire extinguisher halon bottles are installed on various
transport category airplanes, and as such, referring to specific AMMs
is not practical. Furthermore, the FAA notes that only halon bottles
having certain serial numbers are affected and need to be replaced.
There are a significant number of cargo fire extinguisher halon bottles
with serial numbers that are not affected by the requirements of this
AD and that do not need to be removed and tested. Operators have the
option of installing a halon bottle with a serial number that is not
affected by the requirements of this AD, or installing a halon bottle
that has been refurbished by an authorized party. If operators
establish a different procedure to refurbish affected cargo fire
extinguisher halon bottles, they can apply for an alternative method of
compliance by using the procedures described in paragraph (l) of this
AD. The FAA has not revised this AD in regard to this issue.
Explanation of Change to Manufacturer's Name Specified in This Final
Rule
The FAA has revised paragraph (c)(2)(iv) of this AD to identify the
[[Page 65195]]
manufacturer name as MHI RJ Aviation UL (instead of Bombardier, Inc.),
as published in the most recent type certificate data sheet for the
affected models.
Conclusion
The FAA reviewed the relevant data, considered the comments
received, and determined that air safety and the public interest
require adopting this final rule with the change described previously
and minor editorial changes. The FAA has determined that these minor
changes:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related IBR Material 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 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.
Costs of Compliance
The FAA estimates that this 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. The FAA estimates the
following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Inspection............................ 2 work-hours x $85 per $0 $170 $562,360
hour = $170.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
inspection. The FAA has no way of determining the number of aircraft
that might need replacements:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replacement................................... 4 work-hours x $85 per hour = $25,305 $25,645
$340.
----------------------------------------------------------------------------------------------------------------
According to manufacturer for the cargo fire extinguisher halon
bottles, some or all of the costs of this AD may be covered under
warranty, thereby reducing the cost impact on affected individuals. The
FAA does not control warranty coverage for affected individuals. 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
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.
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
0
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]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
[[Page 65196]]
2020-21-02 Transport Category Airplanes: Amendment 39-21275; Docket
No. FAA-2020-0209; Product Identifier 2020-NM-004-AD.
(a) Effective Date
This AD is effective November 19, 2020.
(b) Affected ADs
None.
(c) Applicability
(1) This AD applies to the Kidde Aerospace & Defense cargo fire
extinguisher halon bottles having part numbers and serial numbers
identified 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) MHI RJ Aviation ULC (type certificate previously held by
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
Aeronautics) 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 already 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 (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 identified 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 airplane 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) of this AD.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, 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
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: [email protected].
(n) 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) Boeing Alert Requirements Bulletin 737-26A1150 RB, dated
September 27, 2019.
(ii) Boeing Alert Requirements Bulletin 737-26A1151 RB, dated
September 27, 2019.
(iii) Kidde Aerospace & Defense Service Bulletin 473919-26-521,
Rev 02, dated November 7, 2019.
(iv) Kidde Aerospace & Defense Service Bulletin 473957-26-518,
Rev 02, dated November 4, 2019.
(3) 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
[[Page 65197]]
Beach, CA 90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.com.
(4) 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;
https://kiddetechnologies.com/aviation/.
(5) 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.
(6) 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 [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on October 1, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-22725 Filed 10-14-20; 8:45 am]
BILLING CODE 4910-13-P