97-22-03: Seat Belt Safety Cover

97-22-03 EXTRA FLUGZEUGBAU GMBH: Amendment 39-10174; Docket No. 97-CE-80-AD. Applicability: Model EA-300/200 airplanes (serial numbers 01 through 15), 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 (c) 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 the next 5 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished. To prevent loss of directional control caused by seat belt interference with the rear rudder pedal controls, accomplish the following: (a) Install a seat belt safety cover (Extra part number 77205.1 and 77205.2 or FAA-approved equivalent part ) in accordance with the INSTRUCTIONS in Extra Flugzeugbau GmbH. Service Bulletin (SB) No. 300-1-97, Issue B, dated June 11, 1997. (b) 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 provided the airplane is flown single seated with the front seat belts properly stowed. (c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Small Airplane Directorate, Aircraft Certification Service, 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. (d) The installation required by this AD shall be done in accordance with Extra Flugzeugbau, GmbH. EA-300 Service Bulletin No. 300-1-97, Issue B, dated June 11, 1997. 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 Flugzeugbau, GmbH., Schwarze Heide 21, 46569 Hunxe, Germany. 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 German airworthiness directive 97-203, dated July 3, 1997. (e) This amendment becomes effective on November 24, 1997.