Airworthiness directives › 98-08-06
AD 98-08-06 Airworthiness Directives; AERMACCI S.p.A. S.205 Series and Models S.208 and S.208A Airplanes
Models named: S.205-18/F, S.205-18/R, S.205-20/F, S.205- 20/R, S.205-22/R, S.208, S.208A. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Models S.205-18/F, S.205-18/R, S.205-20/F, S.205- 20/R, S.205-22/R, S.208, and S.208A airplanes, all serial numbers, certificated in any category. Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes 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 (e) 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 as indicated in the body of this AD, unless already accomplished. To prevent loss of critical airplane functions because of cracked flight control cables, which could result in loss of control of the airplane if occurring during flight, accomplish the following: (a) Within the next 100 hours time-in-service (TIS) after the effective date of this AD, inspect all flight control cables (elevator control, aileron control, rudder, flaps, nose gear steering, parking brake, safety belts, and autopilot systems) for cracks in the eye end. Accomplish this inspection in accordance with SIAI Marchetti, S.p.A. Mandatory Service Bulletin No. 205B58. (b) If any cracked flight control cable is found, prior to further flight after the inspection required by paragraph (a) of this AD, replace the cracked cable with a new cable of the same design that is found to be free of cracks in the eye end. The replacement(s) shall be accomplished in accordance with the applicable maintenance manual. (c) As of the effective date of this AD, no person may install a flight control cable on an affected airplane, unless the cable has been found to be free of cracks in the eye end. (d) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (e) An alternative method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City, Missouri 64106. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Small Airplane Directorate. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Small Airplane Directorate. (f) Questions or technical information related to SIAI Marchetti, S.p.A. Mandatory Service Bulletin No. 205B58, should be directed to SIAI Marchetti S.p.A., Product Support Department, Via Indipendenza 2, 21018 Sesto Calende (VA), Italy; telephone: +39-331- 929117; facsimile: +39-331-922525. This service information may be examined at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri. (g) The inspection required by this AD shall be done in accordance with SIAI Marchetti, S.p.A. Mandatory Service Bulletin No. 205B58, dated December 31, 1995. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from SIAI Marchetti S.p.A., Product Support Department, Via Indipendenza 2, 21018 Sesto Calende (VA), Italy. Copies may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC. (h) This amendment becomes effective on May 26, 1998. Issued in Kansas City, Missouri, on March 31, 1998. Michael Gallagher, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 98-9139 Filed 4-9-98; 8:45 am] BILLING CODE 4910-13-U
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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