Airworthiness directives › 2005-11-14
AD 2005-11-14 Airworthiness Directives; Dassault Model Mystere-Falcon 50 and 900 Series Airplanes, and Model Falcon 2000 and 900EX Series Airplanes
Models named: Mystere-Falcon 50, Model Falcon 2000 series, Mystere-Falcon 900. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model Mystere-Falcon 50 and Model Falcon 2000 series airplanes equipped with Global Positioning/Inertial Reference System (GP/IRS) part number (P/N) HG2001-GC02, P/N HG2001-GC03, or P/N HG2001-GD03; Model Mystere-Falcon 900 and Model Falcon 900EX series airplanes equipped with GP/IRS P/N HG2001-GC03 or P/N HG2001-GD03; except those airplanes on which one of the following has been incorporated during production: Dassault Modification M2004, M3386, or M2873; certificated in any category.
Compliance
Required as indicated, unless accomplished previously. To prevent the erroneous cockpit display of ground speed, wind velocity and direction, flight path angle, and true track angle when using certain autopilot and/or flight management system functions; which could cause the pilot to lose situational awareness, and possibly lose control of the airplane, accomplish the following: Service Bulletin Reference (a) The term “service bulletin,” as used in this AD, means the Accomplishment Instructions of the following service bulletins, as applicable: (1) For the installation specified in paragraph (c) of this AD, the applicable service bulletin in Table 1 of this AD. Table 1.—Service Bulletins for Paragraph (c) Installation Dassault service bulletin Date Model F2000-285 October 29, 2003 Falcon 2000. F900EX-190 October 29, 2003 Falcon 900EX. F900-324 October 29, 2003 Mystere-Falcon 900. F50-424 October 29, 2003 Mystere-Falcon 50 (2) For the modification specified in paragraph (d) of this AD, the applicable service bulletin in Table 2 of this AD. Although the Accomplishment Instructions of some of these service bulletins describe procedures for submitting a reporting card to the manufacturer, this AD does not require those actions. Table 2.—Service Bulletins for Paragraph (d) Modification Dassault service bulletin Revision Date Model F2000-273 1 October 29, 2003 Falcon 2000 equipped with head-up display (HUD). F900EX-181 1 October 29, 2003 Falcon 900EX. F900-318 1 October 29, 2003 Mystere-Falcon 900. Airplane Flight Manual Revisions (b) Within 7 days after the effective date of this AD: Revise the applicable Airplane Flight Manual (AFM) by accomplishing paragraphs (b)(1), (b)(2), (b)(3) and (b)(4) of this AD, as applicable. Thereafter, operate the airplane per the limitations specified in these AFM revisions. (1) Revise the Limitations Section to include the information in Dassault Temporary Change (TC) 15, dated September 23, 2003, to the Dassault Mystere-Falcon 900 AFM, Document FM900C. (2) Revise the Limitations Section to include the information in Dassault TC 57, dated September 23, 2003, to the Dassault Falcon 900EX AFM, Document DTM561. (3) Revise the Limitations Section to include the information in Dassault TC 61, dated September 23, 2003, to the Dassault Mystere-Falcon 50 AFM, Document FM813EX. Compliance with the provisions of TC 61 constitutes terminating action for the requirements of this AD for all Mystere-Falcon 50 series airplanes. (4) Revise the Limitations Section to include the information in Dassault TC 122, dated September 23, 2003, to the Dassault Falcon 2000 AFM, Document DTM537. Compliance with the provisions of Dassault TC 122 constitutes terminating action for the requirements of this AD for all Model Falcon 2000 series airplanes not equipped with head-up display (HUD). Note 1: When the information in Dassault TCs 15, 57, 61, and 122 has been included in general revisions of the AFM, the TCs may be removed from the AFM, provided the relevant information in the general revision is identical to that in Dassault TCs 15, 57, 61, and 122. Installation of Deactivation Locking Collars (c) For airplanes on which the GPS is deactivated in accordance with the applicable TC specified in paragraph (b) of this AD: Prior to further flight after deactivating the GPS, install a deactivation locking collar on each GPS 1 and GPS 2 circuit breaker in accordance with the applicable service bulletin. This installation constitutes terminating action for the requirements of this AD for Model Falcon 2000 series airplanes that are not equipped with HUD, and for Model Mystere-Falcon 50 series airplanes. Wiring Modification (d) For Model Falcon 2000 series airplanes equipped with HUD; for Model Falcon 900EX series airplanes; and for Model Mystere-Falcon 900 series airplanes: Within 25 months after the effective date of this AD, modify the GP/IRS wiring in accordance with the applicable service bulletin. After this modification has been completed, the applicable TC required by paragraph (b) of this AD may be removed from the AFM. Alternative Methods of Compliance (e) In accordance with 14 CFR 39.19, the Manager, ANM-116, International Branch, FAA, Transport Airplane Directorate, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (f) Unless otherwise specified in this AD, the actions must be done in accordance with the applicable service bulletins listed in Table 3 of this AD, and the applicable temporary changes listed in Table 4 of this AD. Table 3.—Material Incorporated by Reference—Service Bulletins Dassault service bulletin Revision Date F2000-273 1 October 29, 2003. F2000-285 Original October 29, 2003. F50-424 Original October 29, 2003. F900-318 1 October 29, 2003. F900-324 Original October 29, 2003. F900EX-181 1 October 29, 2003. F900EX-190 Original October 29, 2003. Table 4.—Material Incorporated by Reference—Temporary Changes Dassault temporary change Date Dassault airplane flight manual Document 15 September 23, 2003 Mystere-Falcon 900 FM900C. 57 September 23, 2003 Falcon 900EX DTM561. 61 September 23, 2003 Mystere-Falcon 50 FM813EX. 122 September 23, 2003 Falcon 2000 DTM537. 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. To get copies of this service information, contact Dassault Falcon Jet, P.O. Box 2000, South Hackensack, New Jersey 07606. To inspect copies of this service information, go to the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or to the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. Note 2: The subject of this AD is addressed in French airworthiness directive 2003-409(B), dated October 29, 2003. Effective Date (g) This amendment becomes effective on July 13, 2005. Issued in Renton, Washington, on May 26, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-11052 Filed 6-7-05; 8:45 am] BILLING CODE 4910-13-P
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