Airworthiness directives › 2014-12-12
AD 2014-12-12 Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France) Helicopters
Applicability*9
This AD becomes effective August 4, 2014.
Compliance
(1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Gary Roach, Aviation Safety Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email gary.b.roach@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. 2013-0093, dated April 15, 2013, and corrected on April 17, 2013. You may view the EASA AD on the Internet at http://www.regulations.gov in Docket No. FAA-2013-1090.
Unsafe condition
Within 165 hours time-in-service: (1) Visually inspect each upper and lower locking pin control rod end fitting (control end fitting) for a bend, twist, or breakage. If a control end fitting is bent, twisted, or broken, before further flight, replace the control end fitting with an airworthy control end fitting. (2) Clean and dye penetrant inspect the star support pin for a crack in the areas identified as Zone X and Zone Y in Figure 3 of Eurocopter Alert Service Bulletin No. EC120-52A014, Revision 1, dated January 25, 2013 (ASB No. EC120-52A014) or Eurocopter Alert Service Bulletin No. EC130-52A009, Revision 1, dated January 25, 2013 (ASB No. EC130-52A009), as applicable to your model helicopter. If there is a crack in the star support pin, before further flight, replace the star support pin with an airworthy star support pin. (3) Reinforce the sliding door star support stringer by installing three carbon fabric plies by following the Accomplishment Instructions, paragraph 3.B.2.d. of ASB No. EC120-52A014 or ASB No. EC130-52A009, as applicable to your model helicopter, except this AD does not require you to comply with paragraph 3.C.
Affected ADs
This AD defines the unsafe condition as a failure of the sliding door star axle support. This condition could prevent operation of a sliding door from inside, which could delay evacuation of passengers during an emergency.
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