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Airworthiness directives › 2013-06-51

AD 2013-06-51 Airworthiness Directives; Various Helicopter Models

2013-07-15
2013-06-28
39-17486
FAA-2013-0521
Airframe
—

Applicability*9

This AD publishes EAD No. 2013-06-51, issued March 25, 2013.

Compliance

Before next flight involving a hoist operation, perform the following one-time actions: (1) Perform a cable conditioning lift by following the Accomplishment Instructions, paragraphs 2.A. through 2.A.(2), of the ASB. (2) Perform a load inspection test by following the Accomplishment Instructions, paragraphs 2.B. through 2.I., of the ASB. Refer to the aircraft weight and balance limitations prior to performing this test and use a balancing load if necessary to prevent helicopter rollover. Any alternate method of complying with the load inspection test must first be approved in accordance with paragraph (g) of this AD. (3) If the hoist fails the load inspection test, deactivate or replace the hoist with an airworthy hoist. (4) Record the result of the load inspection test on the hoist component history card or equivalent record.

Required actions

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

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.

Affected ADs

This AD defines the unsafe condition as failure of the overload clutch resulting in in-flight failure of the hoist, which could result in injury to persons being lifted.

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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