Airworthiness directives › 2000-26-11
AD 2000-26-11 Airworthiness Directives; Agusta S.p.A. Model A109E Helicopters
Models named: A109E. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model A109E helicopters with tail rotor blade (blade), part number (P/N) 109-8132-01-109, serial number (S/N) A5-0130, A5-0131, A5-0224 through A5-0246, or A5-0249 through A5-0253, installed, certificated in any category. Note 1: This AD applies to each helicopter identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For helicopters that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.
Compliance
Required within 10 hours time-in-service, unless accomplished previously. To prevent a blade failure and subsequent loss of control of the helicopter, accomplish the following: (a) Replace each affected blade with an airworthy blade, P/N 109-8132-01-109 or P/N 109-8132-01-107, with an S/N other than those listed in the applicability section of this AD. Note 2: Agusta Bollettino Tecnico No. 109EP-13, dated August 3, 2000, pertains to the subject of this AD. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Regulations Group, Rotorcraft Directorate, FAA. Operators shall submit their requests through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Regulations Group. Note 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Regulations Group. (c) 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. (d) This amendment becomes effective on January 16, 2001. Note 4: The subject of this AD is addressed in Ente Nazionale per l'Aviazione Civile (Italy) AD 2000-393, dated August 8, 2000. Issued in Fort Worth, Texas, on December 21, 2000. Henry A. Armstrong, Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 00-33335 Filed 12-28-00; 8:45 am] BILLING CODE 4910-13-P
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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