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Airworthiness directives › 2004-11-01

AD 2004-11-01 Airworthiness Directives; Raytheon Model BAe.125 Series 800A (Including C-29A and U-125 Variant) and 800B Airplanes; and Model Hawker 800 (Including U-125A Variant), and 800XP Airplanes

2004-07-07
2004-06-02
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Airframe
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Makes named: raytheon. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model BAe.125 series 800A (including C-29A and U-125 variant) and 800B airplanes; and Model Hawker 800 (including U-125A variant) and 800XP airplanes; as listed in Raytheon Service Bulletin SB 26-3610, Revision 1, dated September 2003; certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To prevent incorrect wiring of the engine fire extinguisher bottles, which could result in one or both fire extinguisher bottles being discharged into the wrong engine nacelle, accomplish the following: Function Test, Verification, Installation, and Corrective Action (a) Within 70 flight hours or 30 days after the effective date of this AD, whichever occurs first, do the actions specified in paragraphs (a) (1) and (a) (2) of this AD per the Accomplishment Instructions of Raytheon Service Bulletin SB 26-3610, Revision 1, dated September 2003. (1) Perform a functional test of the engine fire extinguishing wiring for appropriate installation, and verify the correct wiring connector installation. If any connector is wired incorrectly, prior to further flight, correct the wiring. (2) Install the new marker bands. Exception to Service Bulletin (b) Although the service bulletin referenced in this AD specifies to submit certain information to the manufacturer, this AD does not include such a requirement. Alternative Methods of Compliance (c) In accordance with 14 CFR 39.19, the Manager, Wichita Aircraft Certification Office, FAA, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (d) The required actions shall be done in accordance with Raytheon Service Bulletin SB 26-3610, Revision 1, dated September 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 Raytheon Aircraft Company, Department 62, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. Effective Date (e) This amendment becomes effective on July 7, 2004. Issued in Renton, Washington, on May 17, 2004. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-11959 Filed 6-1-04; 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