Airworthiness directives › 2003-22-10
AD 2003-22-10 Airworthiness Directives; Eurocopter France Model EC120B Helicopters
Models named: EC120B. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model EC120B helicopters, certificated in any category.
Compliance
Required as indicated, unless accomplished previously. To prevent an unsecured bonding braid from restricting travel of the cyclic pitch control stick, and subsequent loss of control of the helicopter, accomplish the following: (a) Within 10 hours time-in-service (TIS), temporarily secure the electrical bonding braid or in stall the permanent attachment system for the bonding braid in accordance with the Accomplishment Instructions, paragraph 2.B., of Eurocopter France Alert Telex No. 67A008, dated July 8, 2002 (Alert Telex). (b) Within 500 hours TIS or 12 months, whichever occurs first, install the permanent attachment system for the bonding braid in accordance with the Accomplishment Instructions, paragraph 2.B.2. and 2.B.3., of the Alert Telex. (c) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Send the proposal to the Manager, Safety Management Group, FAA. Contact the Safety Management Group for information about previously approved alternative methods of compliance. (d) The required actions shall be done in accordance with the Eurocopter France Alert Telex No. 67A008, dated July 8, 2002. The Director of the Federal Register approved this incorporation by reference in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from American Eurocopter Corporation, 2701 Forum Drive, Grand Prairie, Texas 75053-4005, telephone (972) 641-3460, fax, (972) 641-3527. Copies may be inspected at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on December 10, 2003. Note: The subject of this AD is addressed in Direction Generale De L'Aviation (France) AD 2003-371-010(A), dated July 24, 2002. Issued in Fort Worth, Texas, on October 24, 2003. David A. Downey, Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 03-27542 Filed 11-4-03; 8:45 am] BILLING CODE 4910-13-M
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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