99-10-01: Wing Attachment Bolts

99-10-01 AVIONS PIERRE ROBIN: Amendment 39-11155; Docket No. 98-CE-79-AD. Applicability: Model R2160 airplanes, serial numbers 001 through 298, 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 (d) 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 a wing from separating from the airplane caused by damaged wing attachment bolts, which could result in loss of control of the airplane, accomplish the following: (a) Within the next 100 hours time-in-service (TIS) after the effective date of this AD, replace the wing attachment bolts and associated hardware, in accordance with Avions Pierre Robin NOTE NAV 96-3, dated May 2, 1996. (b) As of the effective date of this AD, no person may install, on any affected airplane, wing attachment bolts and associated hardware that are not specified in Avions Pierre Robin NOTE NAV 96-3, dated May 2, 1996, unless the parts are an FAA-approved equivalent to that referenced in the service information. (c) 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. (d) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be used if approved by the Manager, Small Airplane Directorate, FAA, 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. (e) Questions or technical information related to the service information referenced in this AD should be directed to Avions Pierre Robin, 1, route de Troyes, 21121 Darois-France; telephone: 33-3 80 44 20 50; facsimile: 33-3 80 35 60 80. 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 64106. (f) The replacements required by this AD shall be done in accordance with Avions Pierre Robin NOTE NAV 96-3, dated May 2, 1996. 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 Avions Pierre Robin, 1, route de Troyes, 21121 Darois-France. 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. NOTE 3: The subject of this AD is addressed in French AD 96-051(A) R1, dated June 5, 1996. (g) This amendment becomes effective on June 18, 1999.