[Federal Register Volume 83, Number 226 (Friday, November 23, 2018)]
[Rules and Regulations]
[Pages 59290-59295]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-25003]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-9392; Product Identifier 2016-NM-003-AD; Amendment 
39-19499; AD 2018-23-12]
RIN 2120-AA64


Airworthiness Directives; Zodiac Aero Evacuation Systems (also 
known as Air Cruisers Company)

AGENCY: Federal Aviation Administration (FAA), DOT.

[[Page 59291]]


ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for Zodiac 
Aero Evacuation Systems (also known as Air Cruisers Company) fusible 
plugs installed on emergency evacuation equipment for various transport 
category airplanes. This AD was prompted by reports indicating that 
affected fusible plugs activated (vented gas) below the rated 
temperature. This AD requires an inspection of the fusible plugs to 
determine the part number and lot number, and replacement of all 
affected fusible plugs. We are issuing this AD to address the unsafe 
condition on these products.

DATES: This AD is effective December 28, 2018.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of December 28, 
2018.

ADDRESSES: For service information identified in this final rule, 
contact Air Cruisers, 1747 State Route 34, Wall Township, NJ 07727-
3935; phone 732-681-3527; email 
[email protected]. 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. It is also available on the 
internet at http://www.regulations.gov by searching for and locating 
Docket No. FAA-2016-9392.

Examining the AD Docket

    You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9392; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, the regulatory evaluation, any comments received, and 
other information. The address for Docket Operations (phone: 800-647-
5527) 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: Darren Gassetto, Aerospace Engineer, 
Mechanical Systems and Admin Services Section, FAA, New York ACO 
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 
516-228-7323; fax 516-794-5531; email [email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 by adding an AD that would apply to Zodiac Aero Evacuation 
Systems (also known as Air Cruisers Company) fusible plugs installed on 
emergency evacuation equipment for various transport category 
airplanes. The NPRM published in the Federal Register on November 18, 
2016 (81 FR 81709). The NPRM was prompted by reports indicating that 
affected fusible plugs activated (vented gas) below the rated 
temperature. The NPRM proposed to require an inspection of the fusible 
plugs to determine the part number and lot number, and replacement of 
all affected fusible plugs.
    We subsequently issued a supplemental NPRM (SNPRM) that was 
published in the Federal Register on January 24, 2018 (83 FR 3283). The 
SNPRM proposed to extend the compliance time, clarify the 
applicability, and clarify certain requirements.
    We are issuing this AD to address fusible plugs that might activate 
below the rated temperature and render the evacuation system unusable.

Comments

    We gave the public the opportunity to participate in developing 
this final rule. The following presents the comments received on the 
SNPRM and the FAA's response to each comment.

Request to Extend Compliance Time

    Airlines for America (A4A), on behalf of its members, requested 
that we extend the compliance time specified in paragraph (h) of the 
proposed AD (in the SNPRM). A4A stated that the extended compliance 
time of 42 months after the effective date (in paragraph (g) of the 
proposed AD (in the SNPRM)) had an unintended consequence in the re-
worded compliance paragraph (h) of the proposed AD (in the SNPRM). A4A 
noted that while the allowance for maintenance records inspection was 
added, the words ``[b]efore further flight'' remained. A4A concluded 
that the current version means that either a planeside finding or a 
maintenance records discovery will each require action before further 
flight. A4A stated that while a finding by direct inspection will 
happen only in a shop and not affect operation of any aircraft, the 
accommodation for records review could immediately ground an in-service 
aircraft. A4A requested that we allow 42 months for the replacement if 
a records review was done.
    We agree to revise the compliance time in paragraph (h) of this AD 
because we have determined that a compliance time of 42 months to 
replace the affected part addresses the unsafe condition and provides 
an acceptable level of safety. We have revised paragraph (h) of the AD 
to specify a 42-month compliance time for the replacement.

Request To Specify Serial Numbers

    All Nippon Airways (ANA) requested that we revise paragraph (c) of 
the proposed AD (in the SNPRM) to refer to service information that 
specifies the serial numbers and not only the part numbers of the 
affected emergency equipment. ANA stated that identifying affected 
[parts] by only the part number means that even after expiration of the 
compliance time specified in the proposed AD, the inspection must be 
continued every time the affected emergency equipment is purchased. ANA 
stated that the serial number of the affected emergency equipment 
should be specified in the service information listed in paragraph (c) 
of the proposed AD (in the SNPRM) in order to prevent endless 
inspections.
    We do not agree because specific serial numbers for the affected 
emergency equipment have not been identified. In addition, since the 
fusible plugs are rotable we cannot limit the applicability to only the 
known emergency equipment on which the fusible plugs were initially 
installed. Therefore, in order to address the identified unsafe 
condition, all fusible plugs installed on emergency evacuation 
equipment identified in the service information specified in paragraph 
(c) of this AD must be inspected as specified in paragraph (g) of this 
AD. When installing new equipment on an airplane, operators must ensure 
the newly installed part is not one of the affected parts by complying 
with the parts installation prohibition specified in paragraph (i) of 
this AD. We have not changed this AD in this regard.

Request To Refer to Service Information

    Southwest Airlines (SWA) and A4A, on behalf of its members, 
requested that we refer to service information for accomplishing the 
actions specified in paragraph (g) of the proposed AD (in the SNPRM). 
SWA stated that the Air Cruisers service bulletins listed in paragraphs 
(c)(1) through (c)(16) of the proposed AD (in the SNPRM) have steps to 
inspect for the affected fusible plugs and to remove fusible plugs that 
are stamped with Lot PA-21 or PA-22. SWA noted that the service 
bulletins have been incorporated into the various

[[Page 59292]]

Air Cruisers component maintenance manuals (CMMs). A4A stated that the 
service bulletins and CMMs specify an inspection for the suspect 
fusible plug lot numbers and replacement if found.
    A4A and SWA also stated that maintenance records would not indicate 
the level of detail of the fusible plug part numbers and lot numbers 
installed. SWA stated that the revision of the CMM used to make the 
components serviceable is noted on FAA Form 8130-3. A4A also stated 
that access to the fusible plug part number and lot number is not 
achievable planeside, and noted that the equipment manufacturer 
recommends the system to be unpacked and inspected in the slide shop. 
SWA and A4A requested that paragraph (g) of the proposed AD (in the 
SNPRM) be revised to specify accomplishing the inspection in accordance 
with the applicable service information specified in paragraphs (c)(1) 
through (c)(16) of the proposed AD (in the SNPRM) and/or the applicable 
component maintenance manuals.
    We do not agree with revising paragraph (g) of this AD to mandate 
service information because this AD does not require operators to 
accomplish the inspection using a specific method. However, we do agree 
that operators should be aware of the service information that can be 
used to do the inspection specified in paragraph (g) of this AD. 
Therefore, we have added Note 1 to paragraph (g) of this AD to specify 
service bulletins and CMMs that provide guidance for performing the 
inspection. We have redesignated subsequent notes in this AD 
accordingly.
    We also acknowledge the commenters' statement that the records 
review might not be conclusive. As stated in paragraph (g) of this AD, 
the records review is allowed only if operators can conclusively 
determine the part number and lot number. For operators that do not 
have records that can conclusively determine the part number and lot 
number, the inspection must be done.

Request To Remove Paragraph (h) of the Proposed AD (in the SNPRM)

    SWA requested that we remove paragraph (h) of the proposed AD (in 
the SNPRM). SWA stated that paragraph (h) of the proposed AD (in the 
SNPRM) would require immediate removal of the emergency equipment if an 
inspection or a records review determines an affected part is 
installed. SWA suggested that paragraph (h) of the proposed AD (in the 
SNPRM) be deleted because it is unnecessary. SWA stated the emergency 
equipment must be removed from the aircraft in order to inspect for the 
affected fusible plug. SWA noted the component maintenance documents do 
not provide the level of detail of the fusible plug part numbers and 
lot numbers installed.
    We do not agree with removing paragraph (h) of this AD because in 
order to address the unsafe condition the affected fusible plug must 
not only be removed but must also be replaced as required by paragraph 
(h) of this AD. We have not changed this AD in this regard. However, as 
stated previously, we have revised the compliance time in paragraph (h) 
of this AD to specify replacing within 42 months instead of requiring 
immediate action.

Request for Credit for Actions Done Using Certain Service Information

    SWA requested that we give credit for inspections of the affected 
fusible plugs previously done per Air Cruisers service bulletins and/or 
CMMs incorporating the requirements of the Air Cruisers service 
bulletins.
    We agree to clarify. We have not mandated specific service 
information for accomplishing the actions specified in paragraphs (g) 
and (h) of this AD; therefore, it is not necessary to give credit for 
using specific service information. For operators that have already 
accomplished the actions required by paragraphs (g) and (h) of this AD, 
credit is given as specified in paragraph (f) of this AD, which states 
to accomplish the required actions within the compliance times 
specified, ``unless already done.'' Therefore, if operators have 
accomplished the actions required for compliance with paragraphs (g) 
and (h) of this AD before the effective date of this AD, no further 
action is necessary.

Request To Revise Parts Installation Prohibition

    A4A, on behalf of its members, requested that we revise paragraph 
(i) of the proposed AD (in the SNPRM) to specify that no person may 
install on any airplane any slide, slide/raft, or off-wing escape 
system unless the inspection of the fusible plug has been done per the 
applicable service information specified in paragraphs (c)(1) through 
(c)(16) of the proposed AD (in the SNPRM) and/or the applicable CMM 
listed in Air Cruisers Service Information Letter (SIL) 25-246, Rev. 
No. 2, dated January 24, 2017. A4A stated that paragraph (i) of the 
proposed AD (in the SNPRM) does not sufficiently close the door on 
direct inspection of the plug, which can only be accomplished by 
unpacking slides and complete disassembly. A4A stated that only the 
inspection of records (including service bulletin accomplishment 
information directly stamped on the slide) can reasonably accomplish 
the intention of the proposed AD in a practical manner.
    We do not agree because we have not mandated the service 
information specified by the commenter. In order to comply with 
paragraph (i) of this AD, operators must prevent the installation of an 
affected part on an airplane. Paragraph (i) of this AD does not mandate 
a specific method for operators to follow to ensure the affected part 
is not installed. We have not changed this AD in this regard.

Request To Revise Cost Estimate

    A4A, on behalf of its members, requested that we revise the cost 
estimate. A4A stated that the NPRM assumes one hour of labor per 
aircraft. A4A noted that because the actions need to be done at an 
appropriate facility (off wing and often not the operator's own shop), 
the cost should be per system, and include all facets from uninstalling 
through reinstallation. A4A stated the operator's actions will consume 
closer to 4 hours per slide (at $85/hour), with the addition of $500 
each way shipping, and the vendor cost (Zodiac's typical billing is 
$2,900 per slide).
    We agree with revising the cost estimate because operators that 
cannot do a records review will need to remove the affected emergency 
equipment to accomplish the inspection. We disagree with including the 
shipping and vendor costs because not all operators will need to ship 
the equipment in order to do the inspection or records review. We have 
revised the Costs of Compliance section in this final rule to specify 
up to 4 work-hours for the inspection.

Clarification of Replacement Part

    In paragraph (h) of the proposed AD (in the SNPRM), we specified to 
replace the fusible plug with a new part that does not have P/N B13984-
3, stamped with Lot PA-21 or PA-22. However, we have determined that it 
is not necessary for the replacement part to be a new part. Therefore, 
we have revised paragraph (h) of this AD to specify to replace the 
fusible plug with a serviceable fusible plug P/N B13984-3 that is not 
stamped with Lot PA-21 or PA-22.

Additional Affected Parts--Other Related Service Information

    We have reviewed Air Cruisers Service Information Letter (SIL) 25-
246, Rev. No. 2, dated January 24, 2017, which indicates additional 
fusible plugs

[[Page 59293]]

might be affected by the identified unsafe condition. We have 
determined that to delay this action in order to allow the public to 
comment on the merits of inspecting the additional fusible plugs would 
be inappropriate, since we have determined that an unsafe condition 
exists and that inspections must be conducted to ensure continued 
safety. We are considering additional rulemaking to address additional 
fusible plugs.

Clarification of Manufacturer's Name

    In the Summary of the SNPRM, we noted that Zodiac Aero Evacuation 
Systems was formerly known as Air Cruisers. However, Zodiac Aero 
Evacuation Systems is also known as Air Cruisers Company. For clarity, 
we have referred to the manufacturer as Zodiac Aero Evacuation Systems 
(also known as Air Cruisers Company) throughout this final rule.

Conclusion

    We reviewed the relevant data, considered the comments received, 
and determined that air safety and the public interest require adopting 
this final rule with the changes described previously and minor 
editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
SNPRM for addressing the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the SNPRM.
    We also determined that these changes will not increase the 
economic burden on any operator or increase the scope of this final 
rule.

Related Service Information Under 1 CFR Part 51

    We reviewed the following Air Cruisers service information. The 
service information identifies the affected fusible plugs. In addition, 
it describes procedures for inspecting and replacing affected fusible 
plugs. These documents are distinct since they apply to different 
airplane models or configurations.
     Air Cruisers Service Bulletin 737 103-25-50, dated August 
27, 2010.
     Air Cruisers Service Bulletin 757 105-25-80, dated August 
27, 2010.
     Air Cruisers Service Bulletin 757 105-25-81, dated August 
27, 2010.
     Air Cruisers Service Bulletin 767 106-25-10, Rev. No. 1, 
dated October 15, 2010.
     Air Cruisers Service Bulletin 777 107-25-29, Rev. No. 1, 
dated July 8, 2011.
     Air Cruisers Service Bulletin A300/A310 001-25-19, dated 
August 27, 2010.
     Air Cruisers Service Bulletin A300/A310 003-25-33, dated 
August 27, 2010.
     Air Cruisers Service Bulletin A310 002-25-08, dated August 
27, 2010.
     Air Cruisers Service Bulletin A320 004-25-87, Rev. No. 2, 
dated January 7, 2011.
     Air Cruisers Service Bulletin A321 005-25-21, dated August 
27, 2010.
     Air Cruisers Service Bulletin BAe 146 201-25-23, dated 
December 10, 2010.
     Air Cruisers Service Bulletin F28 352-25-02, dated 
December 10, 2010.
     Air Cruisers Service Bulletin F100 351-25-07, dated 
December 10, 2010.
     Air Cruisers Service Bulletin Liferaft 35-25-79, dated 
August 27, 2010.
     Air Cruisers Service Bulletin MD11 305-25-35, dated August 
27, 2010.
     Air Cruisers Service Bulletin MD80/90/717 304-25-45, dated 
August 27, 2010.
    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

    We estimate that this AD affects 3,384 airplanes of U.S. registry. 
We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                Cost on  U.S.
              Action                    Labor cost        Parts cost     Cost per  product        operators
----------------------------------------------------------------------------------------------------------------
Determination of part and lot      Up to 4 work-hours               $0  Up to $340.........  Up to $1,150,560.
 number.                            x $85 per hour =
                                    Up to $340.
----------------------------------------------------------------------------------------------------------------

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

                                                On-Condition Cost
----------------------------------------------------------------------------------------------------------------
                                                                                                     Cost per
                 Action                           Labor cost                  Parts cost              product
----------------------------------------------------------------------------------------------------------------
Replacement.............................  1 work-hour x $85 per hour  Not available.............             $85
                                           = $85.
----------------------------------------------------------------------------------------------------------------

    According to the manufacturer, some of the costs of this 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 available 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

[[Page 59294]]

products identified in this rulemaking action.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes and 
associated appliances to the Director of the System Oversight Division.

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) Is not a ``significant rule'' under DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) 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):

2018-23-12 Zodiac Aero Evacuation Systems (also known as Air 
Cruisers Company): Amendment 39-19499; Docket No. FAA-2016-9392; 
Product Identifier 2016-NM-003-AD.

(a) Effective Date

    This AD is effective December 28, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Zodiac Aero Evacuation Systems (also known as 
Air Cruisers Company) fusible plugs installed on emergency 
evacuation equipment identified in the service information specified 
in paragraphs (c)(1) through (c)(16) of this AD. These affected 
fusible plugs might be installed on the emergency evacuation 
equipment of the following manufacturers' airplanes: Airbus, The 
Boeing Company, BAE Systems (Operations) Limited, and Fokker 
Services B.V.
    (1) Air Cruisers Service Bulletin 737 103-25-50, dated August 
27, 2010.
    (2) Air Cruisers Service Bulletin 757 105-25-80, dated August 
27, 2010.
    (3) Air Cruisers Service Bulletin 757 105-25-81, dated August 
27, 2010.
    (4) Air Cruisers Service Bulletin 767 106-25-10, Rev. No. 1, 
dated October 15, 2010.
    (5) Air Cruisers Service Bulletin 777 107-25-29, Rev. No. 1, 
dated July 8, 2011.
    (6) Air Cruisers Service Bulletin A300/A310 001-25-19, dated 
August 27, 2010.
    (7) Air Cruisers Service Bulletin A300/A310 003-25-33, dated 
August 27, 2010.
    (8) Air Cruisers Service Bulletin A310 002-25-08, dated August 
27, 2010.
    (9) Air Cruisers Service Bulletin A320 004-25-87, Rev. No. 2, 
dated January 7, 2011.
    (10) Air Cruisers Service Bulletin A321 005-25-21, dated August 
27, 2010.
    (11) Air Cruisers Service Bulletin BAe 146 201-25-23, dated 
December 10, 2010.
    (12) Air Cruisers Service Bulletin F28 352-25-02, dated December 
10, 2010.
    (13) Air Cruisers Service Bulletin F100 351-25-07, dated 
December 10, 2010.
    (14) Air Cruisers Service Bulletin Liferaft 35-25-79, dated 
August 27, 2010.
    (15) Air Cruisers Service Bulletin MD11 305-25-35, dated August 
27, 2010.
    (16) Air Cruisers Service Bulletin MD80/90/717 304-25-45, dated 
August 27, 2010.

(d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.

(e) Unsafe Condition

    This AD was prompted by reports indicating that affected fusible 
plugs activated (vented gas) below the rated temperature. We are 
issuing this AD to address fusible plugs that might activate below 
the rated temperature and render the evacuation system unusable.

(f) Compliance

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

(g) Fusible Plug Identification

    Within 42 months after the effective date of this AD, do an 
inspection to determine if any fusible plug has part number (P/N) 
B13984-3, stamped with Lot PA-21 or PA-22. A review of the airplane 
maintenance records is acceptable to make this determination if it 
can be conclusively determined from that review that a part not 
having P/N B13984-3, stamped with Lot PA-21 or PA-22, has been 
installed.
    Note 1 to paragraph (g) of this AD: Guidance for performing the 
inspection specified in paragraph (g) of this AD can be found in 
applicable service information specified in paragraphs (c)(1) 
through (c)(16) of this AD and the applicable component maintenance 
manuals (CMMs) that have incorporated the appropriate Air Cruisers 
service information.

(h) Replacement of Affected Fusible Plug

    If, during the inspection or records review required by 
paragraph (g) of this AD, it is determined that any fusible plug has 
part number (P/N) B13984-3, stamped with Lot PA-21 or PA-22: Within 
42 months after the effective date of this AD, replace that fusible 
plug with a serviceable fusible plug P/N B13984-3 that is not 
stamped with Lot PA-21 or PA-22.
    Note 2 to paragraph (h) of this AD: Guidance can be found in the 
applicable CMM for the replacement. In addition, Air Cruisers 
Service Information Letter (SIL) 25-246, Rev. No. 1, dated February 
21, 2014, provides information regarding affected fusible plugs and 
guidance on the replacement.

(i) Parts Installation Prohibition

    As of the effective date of this AD, no person may install on 
any airplane any fusible plug having P/N B13984-3, stamped with Lot 
PA-21 or PA-22.

(j) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, New York 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 
certification office, send it to ATTN: Program Manager, Continuing 
Operational Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, 
Suite 410, Westbury, NY 11590; telephone: 516-228-7300; fax: 516-
794-5531.
    (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.

(k) Related Information

    (1) For more information about this AD, contact Darren Gassetto, 
Aerospace Engineer, Mechanical Systems and Admin Services Section, 
FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, 
NY 11590; telephone 516-228-7323; fax 516-794-5531; email [email protected].
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (l)(3) and (l)(4) of this AD.

(l) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this

[[Page 59295]]

paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to 
determine parts that are affected by this AD, unless the AD 
specifies otherwise.
    (i) Air Cruisers Service Bulletin 737 103-25-50, dated August 
27, 2010.
    (ii) Air Cruisers Service Bulletin 757 105-25-80, dated August 
27, 2010.
    (iii) Air Cruisers Service Bulletin 757 105-25-81, dated August 
27, 2010.
    (iv) Air Cruisers Service Bulletin 767 106-25-10, Rev. No. 1, 
dated October 15, 2010.
    (v) Air Cruisers Service Bulletin 777 107-25-29, Rev. No. 1, 
dated July 8, 2011.
    (vi) Air Cruisers Service Bulletin A300/A310 001-25-19, dated 
August 27, 2010.
    (vii) Air Cruisers Service Bulletin A300/A310 003-25-33, dated 
August 27, 2010.
    (viii) Air Cruisers Service Bulletin A310 002-25-08, dated 
August 27, 2010.
    (ix) Air Cruisers Service Bulletin A320 004-25-87, Rev. No. 2, 
dated January 7, 2011.
    (x) Air Cruisers Service Bulletin A321 005-25-21, dated August 
27, 2010.
    (xi) Air Cruisers Service Bulletin BAe 146 201-25-23, dated 
December 10, 2010.
    (xii) Air Cruisers Service Bulletin F28 352-25-02, dated 
December 10, 2010.
    (xiii) Air Cruisers Service Bulletin F100 351-25-07, dated 
December 10, 2010.
    (xiv) Air Cruisers Service Bulletin Liferaft 35-25-79, dated 
August 27, 2010.
    (xv) Air Cruisers Service Bulletin MD11 305-25-35, dated August 
27, 2010.
    (xvi) Air Cruisers Service Bulletin MD80/90/717 304-25-45, dated 
August 27, 2010.
    (3) For service information identified in this AD, contact Air 
Cruisers, 1747 State Route 34, Wall Township, NJ 07727-3935; phone 
732-681-3527; email [email protected].
    (4) 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.
    (5) 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, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Des Moines, Washington, on November 8, 2018.
Chris Spangenberg,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-25003 Filed 11-21-18; 8:45 am]
BILLING CODE 4910-13-P