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Airworthiness directives › 2012-21-07

AD 2012-21-07 Airworthiness Directives; Agusta S.p.A. Helicopters

2012-11-27
2012-10-23
39-17223
FAA-2012-0448
Airframe
—

Applicability*9

This AD becomes effective November 27, 2012.

Compliance

Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199 to operate the helicopter to a location where the requirements of this AD can be accomplished provided that you do not simultaneously operate the landing light and the search light.

Required actions

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

Within 50 hours time-in-service, modify the electrical power distribution system by installing the “BATT BUS” Circuit Breaker Modification Kit, part number 109-0824-73-107, as depicted in Figures 1 through 3 and by following the Compliance Instructions, paragraphs 4. through 7., of Agusta Bollettino Tecnico No. 109S-35, dated December 11, 2009 (ASB). Thereafter, operationally test the electrical system by following paragraphs 19.1 through 19.7 of the ASB.

Affected ADs

This AD defines the unsafe condition as failure of the 35 ampere (amp) “BATT BUS,” which could result in an electrical failure and fire, loss of electrical power to instruments powered by the “BATT BUS” system, and subsequent loss of control of the helicopter.

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