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2018-26-02 |
AIRBUS HELICOPTERS (PREVIOUSLY EUROCOPTER FRANCE):
Amendment 39-19532; Docket No. FAA-2018-0669; Product Identifier 2017-SW-041-AD. |
(a) APPLICABILITY This AD applies to the following helicopters, certificated in any cat- egory: (1) Model AS350B3 helicopters with an ARRIEL 2B1 engine with the two- channel Full Authority Digital Engine Control (FADEC) and with new twist grip modification (MOD) 073254 or with an ARRIEL 2D engine installed; (2) Model EC130B4 helicopters with an ARRIEL 2B1 engine with the two- channel FADEC and with new twist grip MOD 073773 installed; and (3) Model EC130T2 helicopters with an ARRIEL 2D engine installed. (b) UNSAFE CONDITION This AD defines the unsafe condition as failure of one of the two contactors, 53Ka or 53Kb, which can prevent switching from "IDLE" mode to "FLIGHT" mode during autorotation training making it impossible to recover from a practice autorotation and compelling the pilot to continue the autorotation to the ground. This condition could result in unintended touchdown to the ground at a flight-idle power setting during a practice autorotation, damage to the helicopter, and injury to occupants. (c) AFFECTED ADS This AD replaces AD 2016-25-19, Amendment 39-18745 (81 FR 95854, December 29, 2016). (d) EFFECTIVE DATE This AD becomes effective January 30, 2019. (e) COMPLIANCE You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time. (f) REQUIRED ACTIONS (1) Before the next practice autorotation or within 100 hours time-in-ser- vice (TIS), whichever occurs first, inspect the wiring, perform an insulation test, inspect the pilot and copilot throttle twist grip controls, and test the pilot and copilot throttle twist grip controls for proper functioning by following the Accomplishment Instructions, paragraph 3.B.1 through 3.B.6, of Airbus Helicopters Emergency Alert Service Bulletin (EASB) No. 05.00.61, Revision 3, dated June 15, 2015, for Model AS350B3 helicopters with an ARRIEL 2B1 engine; EASB No. 05.00.77, Revision 1, dated June 15, 2015, for Model AS350B3 helicopters with an ARRIEL 2D engine; EASB No. 05A009, Revision 3, dated June 15, 2015, for Model EC130B4 helicopters; or EASB No. 05A014, Revision 1, dated June 15, 2015, for Model EC130T2 helicopters, as appropriate for your model helicopter. (2) Repeat the inspections in paragraph (f)(1) of this AD at intervals not to exceed the following compliance times. For purposes of this AD, salt laden conditions exist when a helicopter performs a flight from a takeoff and landing area, heliport, or airport less than 0.5 statute mile from salt water or performs a flight within 0.5 statute mile from salt water below an altitude of 1,000 ft. above ground or sea level. (i) For helicopters that have operated in salt laden conditions since the previous inspection required by this AD, at intervals not to exceed 330 hours TIS. (ii) For helicopters that have not operated in salt laden conditions since the previous inspection required by this AD, at intervals not to ex- ceed 660 hours TIS. (g) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS) (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, Rotor- craft Standards Branch, FAA, 10101 Hillwood Parkway, Fort Worth, Texas 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. (h) ADDITIONAL INFORMATION The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2017-0059, dated April 6, 2017. You may view the EASA AD on the internet at http://www.regulations.gov in Docket No. FAA-2018- 0669. (i) SUBJECT Joint Aircraft Service Component (JASC) Code: 7697, Engine Control System Wiring. (j) MATERIAL INCORPORATED BY REFERENCE (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (3) The following service information was approved for IBR on January 30, 2019. (i) Airbus Helicopters Emergency Alert Service Bulletin (EASB) No. 05.00.77, Revision 1, dated June 15, 2015. (ii) Airbus Helicopters EASB No. 05A014, Revision 1, dated June 15, 2015. Note 1 to paragraph (j)(3): Airbus Helicopters EASB Nos. 05.00.77 and 05A014, both Revision 1 and dated June 15, 2015, are co-published as one document along with Airbus Helicopters EASB No. 05.00.52 Revision 1, dated June 15, 2015, which is not incorporated by reference in this AD. (4) The following service information was approved for IBR on February 2, 2017 (81 FR 95854, December 29, 2016). (i) Airbus Helicopters EASB No. 05.00.61, Revision 3, dated June 15, 2015. (ii) Airbus Helicopters EASB No. 05A009, Revision 3, dated June 15, 2015. Note 2 to paragraph (j)(4): Airbus Helicopters EASB Nos. 05.00.61 and 05A009, both Revision 3 and dated June 15, 2015, are co-published as one document along with Airbus Helicopters EASB No. 05.00.41 Revision 2, dated June 15, 2015, which is not incorporated by reference in this AD. (5) For Airbus Helicopters service information identified in this AD, con- tact Airbus Helicopters, 2701 N. Forum Drive, Grand Prairie, TX 75052; telephone (972) 641-0000 or (800) 232-0323; fax (972) 641-3775; or at http://www.helicopters.airbus.com/website/en/ref/Technical-Support_73. html. (6) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy, Room 6N-321, Ft Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110. (7) 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 Fort Worth, Texas, on December 13, 2018. Scott A. Horn, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT: George Schwab, Aviation Safety Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 10101 Hill- wood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email george. schwab@faa.gov.
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