Airworthiness directives › 2018-05-02
AD 2018-05-02 Airworthiness Directives; AgustaWestland S.p.A. Helicopters
Applicability*9
This AD becomes effective April 4, 2018.
Compliance
(1) The Manager, Safety Management Section, Rotorcraft Standards Branch, FAA, may approve AMOCs for this AD. Send your proposal to: Martin R. Crane, Aviation Safety Engineer, Regulations & Policy 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
(1) Leonardo Helicopters Bollettino Tecnico No. 189-118, dated October 20, 2016, which is not incorporated by reference, contains additional information about the subject of this AD. For service information identified in this AD, contact Leonardo S.p.A. Helicopters, Matteo Ragazzi, Head of Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-711756; fax +39-0331-229046; or at http://www.leonardocompany.com/-/bulletins. You may review a copy of the service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy, Room 6N-321, Fort Worth, TX 76177. (2) The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2016-0216, dated October 28, 2016. You may view the EASA AD on the internet at http://www.regulations.gov in AD Docket No. FAA-2017-0111.
Unsafe condition
Within 75 hours time-in-service, replace the seal and filler wedges of each cabin and cockpit door emergency exit window, except bubble windows installed in accordance with bubble window kit part number 8G5620F00111.
Affected ADs
This AD defines the unsafe condition as improperly glued emergency exit windows. This condition could result in the window failing to jettison, preventing the occupants from exiting the helicopter during an emergency.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1