Airworthiness directives › 2004-06-14
AD 2004-06-14 Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes
Models named: SAAB 2000 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model SAAB 2000 series airplanes, serial numbers -004 through -063 inclusive; certificated in any category.
Compliance
Required as indicated, unless accomplished previously. To prevent long-term damage to the engine mounting structure (EMS), and loss of redundancy on the EMS, which could result in possible separation of an engine from the airplane, reduced controllability of the airplane, and injury to persons or property on the ground, accomplish the following: Service Bulletin References (a) The following information pertains to the service bulletin referenced in this AD: (1) The term “service bulletin,” as used in this AD, means the Accomplishment Instructions of Saab Service Bulletin 2000-71-014, dated January 23, 2003. (2) Although the service bulletin specifies to submit certain information to the manufacturer, this AD does not include such a requirement. Torque Check (b) Within 3 months after the effective date of this AD: Measure the torque of the adjustable pin in the rear attachment of the intermediate strut for both engines, in accordance with the inspection requirements and torque values in the service bulletin. Retorque (c) Retorque the adjustable pin in the intermediate strut rear attachment of the EMS to the correct torque value, in accordance with the service bulletin. Alternative Methods of Compliance (d) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (e) The actions shall be done in accordance with Saab Service Bulletin 2000-71-014, dated January 23, 2003. 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 Saab Aircraft AB, SAAB Aircraft Product Support, S-581.88, Linköping, Sweden. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Note 1: The subject of this AD is addressed in Swedish airworthiness directive 1-183, dated January 23, 2003. Effective Date (f) This amendment becomes effective on April 30, 2004. Issued in Renton, Washington, on March 16, 2004. Kevin M. Mullin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-6581 Filed 3-25-04; 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