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Airworthiness directives › 2014-21-03

AD 2014-21-03 Airworthiness Directives; Airbus Helicopters (Previously Eurocopter France) Helicopters

Superseded. This directive was replaced by AD 2022-03-13. Work to the current one.
2014-11-12
2014-10-27
39-17995
FAA-2014-0832
Airframe
2022-03-13

Applicability*9

This AD becomes effective November 12, 2014.

Compliance

Special flight permits are prohibited.

Required actions

(1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Rao Edupuganti, Aviation Safety Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email rao.edupuganti@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.

Unsafe condition

For helicopters with 3,900 hours time-in-service (TIS) or more, within 100 hours TIS and thereafter at intervals not exceeding 825 hours TIS, using a light source and a mirror, inspect each support at the four attachment points for a crack. If there is a crack, before further flight, replace the support.

Affected ADs

This AD defines the unsafe condition as a crack on a support at an attachment point, which could result in failure of the support, separation of the yaw damper unit, blocking of the yaw flight control channel, and reduced control of the helicopter.

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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