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Airworthiness directives › 98-26-10

AD 98-26-10 Airworthiness Directives; Dassault Model Mystere-Falcon 20 Series Airplanes, Fan Jet Falcon Series Airplanes, and Fan Jet Falcon Series D, E, and F Series Airplanes

1999-01-22
1998-12-18
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Airframe
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Models named: Mystere-Falcon 20 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

All Model Mystere-Falcon 20 series airplanes, Fan Jet Falcon series airplanes, and Fan Jet Falcon Series D, E, and F series airplanes; certificated in any category.

Compliance

Required as indicated, unless accomplished previously. [[Page 70005]] To ensure that the flight crew is aware of the emergency procedures associated with an engine fire, or with a rear compartment fire or overheat conditions, and to prevent fire from spreading throughout the airplane, accomplish the following: (a) Within 7 days after the effective date of this AD, revise the Limitations Section and Emergency Procedures Section of the FAA- approved Airplane Flight Manual (AFM) by accomplishing the action specified in either paragraph (a)(1) or (a)(2) of this AD, as applicable. (1) For Model Mystere-Falcon 20 series airplanes: Insert a copy of Dassault 731 Falcon Retrofit 20 Airplane Flight Manual DTM30528, Revision 10, dated January 20, 1998, into the AFM. (2) For Model Fan Jet Falcon series airplanes and Model Fan Jet Falcon Series D, E, and F series airplanes: Insert a copy of the Dassault Fan Jet Falcon Airplane Flight Manual DTM589/590/591/592, Revision 49, dated January 20, 1998, into the AFM. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Operations Inspector, who may add comments and then send it to the Manager, International Branch, ANM-116. Note 1: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM-116. (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) The AFM revision shall be done in accordance with Dassault Fan Jet Falcon Airplane Flight Manual DTM589/590/591/592, Revision 49, dated January 20, 1998; or Dassault 731 Falcon Retrofit 20 Airplane Flight Manual DTM30528, Revision 10, dated January 20, 1998; as applicable, which contain the following list of effective pages: ------------------------------------------------------------------------ Revision AFM revision referenced and date Page No. level shown on page ------------------------------------------------------------------------ DTM589/590/591/592............... Falcon 20, 20D, 20E, 49 20F, Title Pages. Revision 49, January 20, 1998.... ........................ ........... Table of Contents, Pages 49 1, 2. Section 2, sub-section 49 01, Pages 1-6. DTM30528......................... List of Effective Pages. 10 Revision 10, January 20, 1998.... Pages 1-22.............. 10 ------------------------------------------------------------------------ (Note: The issue date of Revision 49 of DTM589/590/591/592, and Revision 10 of DTM30528 is indicated only on the Title Page; no other page of the document is dated.) 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 Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, New Jersey 07606. 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 2: The subject of this AD is addressed in French airworthiness directive 98-114-023(B), dated March 11, 1998. (e) This amendment becomes effective on January 22, 1998. Issued in Renton, Washington, on December 11, 1998. Darrell M. Pederson, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 98-33390 Filed 12-17-98; 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