Airworthiness directives › 2018-18-11
AD 2018-18-11 Airworthiness Directives; Airbus Helicopters
Applicability*9
This AD becomes effective October 18, 2018.
Compliance
(1) The Manager, Safety Management Section, Rotorcraft Standards Branch, FAA, may approve AMOCs for this AD. Send your proposal to: George Schwab, Aviation Safety Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email 9-ASW-FTW-AMOC-Requests@faa.gov. (2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, we suggest that you 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.
Required actions
The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2016-0258, dated December 30, 2016. You may view the EASA AD on the internet at http://www.regulations.gov in Docket No. FAA-2018-0418.
Unsafe condition
Within 50 hours time-in-service: (1) Install cable mount part number (P/N) ASMS-A to the helicopter structure as depicted in Figure 1, Detail A and Detail C, of Airbus Helicopters Alert Service Bulletin No. AS365-05.00.73, Revision 1, dated December 12, 2016 (ASB AS365-05.00.73). (2) Inspect the lower strobe light harness and the harness between the cut-off connector and Frame 2000 for tears in the spiral tape and for chafing of the harness wires. If there is a tear in the spiral tape, before further flight, replace the spiral tape. If there is any chafing, before further flight, replace the chafed harness. (3) Route the lower strobe light harness and the harness between the cut-off connector and Frame 2000 and secure as depicted in Figure 1, Detail A and Section B-B, of ASB AS365-05.00.73. Note 1 to paragraph (e) of this AD: Airbus Helicopters identifies the actions in ASB AS365-05.00.73 as Modification 365P084778.00.
Affected ADs
This AD defines the unsafe condition as interference between the lower strobe light electrical harness wiring and the helicopter structure. This condition could result in chafing of an electrical harness adjacent to the inboard fuel tank vapor space, a fuel tank fire, and subsequent loss of control of the helicopter.
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