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Federal Register / Vol. 86, No. 39 / Tuesday, March 2, 2021 / Rules and Regulations
the seat, resulting in injury to the seat occupants during an accident.
f Compliance Comply with this AD within the compliance times specified, unless already done.

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g Retained Inspection and Corrective Actions With Revised Service Information This paragraph restates the requirements of paragraph e of AD 20152601, with revised service information. Within 110
hours time in service after January 26, 2016
the effective date of AD 20152601, do the actions specified in paragraph g1 or 2 of this AD, as applicable for your model helicopter.
1 For Model AS332C1, AS332L1, AS332L2, and EC225LP helicopters:
i Inspect the cabin and cockpit for labels, placards, or markings that prohibit stowing anything under the seats in the locations shown in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No.
AS33201.00.85 or No. EC22504A012, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No.
AS33201.00.85, Revision 1, dated September 7, 2017, or Airbus Helicopters Alert Service Bulletin No. EC22504A012, Revision 2, dated November 6, 2019; as applicable for your model helicopter.
ii If a label, placard, or marking is not located in every location depicted in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No. AS33201.00.85 or No. EC22504A012, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No. AS33201.00.85, Revision 1, dated September 7, 2017, or Airbus Helicopters Alert Service Bulletin No.
EC22504A012, Revision 2, dated November 6, 2019 or is not visible and legible to every occupant, before further flight, install a placard in accordance with the Accomplishment Instructions, paragraph 3.B., of Airbus Helicopters Alert Service Bulletin No. AS33201.00.85 or No. EC225
04A012, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No. AS33201.00.85, Revision 1, dated September 7, 2017, or Airbus Helicopters Alert Service Bulletin No.
EC22504A012, Revision 2, dated November 6, 2019; as applicable for your model helicopter.
2 For Model AS365N2, AS 365 N3, EC
155B, and EC155B1 helicopters:
i Inspect each seat leg in the cabin and cockpit for labels, placards, or markings that prohibit stowing anything under the seats.
ii If a label, placard, or marking does not exist on one leg of each seat or is not visible and legible, before further flight, install a placard in accordance with the Accomplishment Instructions, paragraph 3.B., and the Appendix of Airbus Helicopters Alert Service Bulletin No. AS36501.00.66 or No. EC15504A013, both Revision 0, dated August 26, 2014; or Airbus Helicopters Alert Service Bulletin No. AS36501.00.66 or No.
EC15504A013, both Revision 1, dated February 12, 2019; as applicable for your model helicopter.

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h New Inspection and Corrective Actions for Certain Helicopters 1 For Model AS332C and AS332L
helicopters: Within 110 hours time in service or 30 days, whichever occurs first, after the effective date of this AD, inspect the cabin and cockpit for labels, placards, or markings that prohibit stowing anything under the seats in the locations shown in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No. AS33201.00.85, Revision 1, dated September 7, 2017.
2 If a label, placard, or marking is not located in every location depicted in the figure in the Appendix of Airbus Helicopters Alert Service Bulletin No. AS33201.00.85, Revision 1, dated September 7, 2017 or is not visible and legible to every occupant, before further flight, install a placard in accordance with the Accomplishment Instructions, paragraph 3.B., of Airbus Helicopters Alert Service Bulletin No. AS33201.00.85, Revision 1, dated September 7, 2017.
i New Requirements of This AD:
Modification Install New Placards 1 At the applicable times specified in paragraph i2 of this AD, install new placards prohibiting stowage of any object under an energy-absorbing seat in accordance with the Accomplishment Instructions, paragraph 3.B., of the applicable service information specified in paragraphs i1i through vii of this AD, except you are not required to discard the old labels placards.
Doing the installation required by this paragraph terminates the requirements of paragraphs g and h of this AD.
i Airbus Helicopters Alert Service Bulletin No. AS33225.03.16, Revision 0, dated September 7, 2017.
ii Airbus Helicopters Alert Service Bulletin No. AS33225.03.41, Revision 0, dated September 7, 2017.
iii Airbus Helicopters Alert Service Bulletin No. AS33225.03.42, Revision 0, dated September 7, 2017.
iv Airbus Helicopters Alert Service Bulletin No. AS36525.01.67, Revision 0, dated February 12, 2019.
v Airbus Helicopters Alert Service Bulletin No. EC15525A144, Revision 0, dated February 12, 2019.
vi Airbus Helicopters Alert Service Bulletin No. EC22525A179, Revision 1, dated November 6, 2019.
vii Airbus Helicopters Alert Service Bulletin No. EC22525A203, Revision 0, dated September 7, 2017; as applicable for your model helicopter.
2 At the applicable times specified in paragraph i2i or ii of this AD, do the installation required by paragraph i1 of this AD.
i For Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, AS365N2, AS 365 N3, EC 155B, EC155B1, and EC225LP helicopters, all manufacturer serial numbers, except Model EC225LP helicopters, manufacturer serial numbers 2663, 2670, 2854, 2883, 2885, 2901 and 2921: Within 110 hours time in service or 6 months, whichever occurs first after the effective date of this AD.
ii For Model EC225LP helicopters, manufacturer serial numbers 2663, 2670, 2854, 2883, 2885, 2901 and 2921: Within 50

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hours time in service or 2 months, whichever occurs first after the effective date of this AD.
j No Actions Required for Certain Helicopters For Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and EC225LP
helicopters delivered after September 7, 2017: No actions are required, provided that no energy-absorbing seat, as identified in figure 1 to paragraph c of this AD, has been installed on that helicopter since delivery.
k Credit for Previous Actions 1 This paragraph provides credit for the actions specified in paragraph g of this AD, if those actions were performed before the effective date of this AD using Airbus Helicopters Alert Service Bulletin No.
EC22504A012, Revision 1, dated September 7, 2017.
2 This paragraph provides credit for the actions specified in paragraphs i1 and 2
of this AD, if those actions were performed before the effective date of this AD using Airbus Helicopters Alert Service Bulletin No.
EC22525A179, Revision 0, dated September 7, 2017.
l Alternative Methods of Compliance AMOCs 1 The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Validation Branch, send it to the attention of the person identified in paragraph m2 of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@
faa.gov. 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.
2 For operations conducted under a 14
CFR part 119 operating certificate or under 14 CFR part 91, subpart K, notify your principal inspector or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC.
m Related Information 1 The subject of this AD is addressed in European Union Aviation Safety Agency EASA AD 20190088R1, dated November 8, 2019. This EASA AD may be found in the AD
docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA20200905.
2 For more information about this AD, contact Kathleen Arrigotti, Aviation Safety Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198;
phone and fax: 2062313218; email:
kathleen.arrigotti@faa.gov.
3 Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs n5 and 6 of this AD.

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