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Airworthiness directives › 2020-11-05

AD 2020-11-05 Airworthiness Directives; Airbus Helicopters

Superseded. This directive was replaced by AD 2021-26-07. Work to the current one.
2020-06-08
2020-05-22
39-21130
FAA-2020-0455
Airframe
2021-26-07

Models named: EC120B. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus Helicopters Model EC120B helicopters, certificated in any category, all serial numbers.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

(1) For the purposes of this AD, an affected part is any tail rotor hub body part number C642A0100103. (2) For the purposes of this AD, a serviceable part is any affected part that is new (not previously installed on any helicopter); or any affected part on which an inspection has been done as specified in the instructions of Airbus Helicopters Emergency Alert Service Bulletin 05A020, Revision 0, dated October 29, 2019, or Airbus Helicopters Emergency Alert Service Bulletin 05A020, Revision 1, dated November 8, 2019, and there were no cracks.

Unsafe condition

This AD was prompted by a report of recurrent loss of tightening torque on several attachment bolts on the tail rotor hub body. The FAA is issuing this AD to address this condition, which could lead to cracking and potential loss of the tail rotor drive and consequent loss of yaw control of the helicopter.

Affected ADs

None.

Read the original on the Federal Register →

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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