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Airworthiness directives › 2005-15-16

AD 2005-15-16 Airworthiness Directives; AvCraft Dornier Model 328-300 Airplanes

2005-09-06
2005-08-01
39-14205
FAA-2005-21054
Airframe
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Models named: 328-300. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to AvCraft Dornier Model 328-300 airplanes, certificated in any category, serial numbers 3105 through 3223 inclusive.

Compliance

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Without Option 033F003 Installed: Modification and Installations (f) For airplanes without option 033F003 installed: Within 12 months after the effective date of this AD, do the actions in Table 1 of this AD in accordance with the Accomplishment Instructions of AvCraft Service Bulletin SB-328J-00-197, dated August 23, 2004. Table 1.—Requirements for Airplanes Without Option 033F003 Installed Do the following actions— By accomplishing all the actions specified in— (1) Modify the electrical wiring of the left-hand and right-hand fuel pumps Paragraph 1.B(1) of the service bulletin. (2) Install insulation at the left-hand and right-hand flow control and shut-off valves and other components of the environmental control system Paragraph 1.B(2) of the service bulletin. (3) Install markings at fuel wiring harnesses Paragraph 1.B(3) of the service bulletin. With Option 033F003 Installed: Modification, Replacement, and Installation (g) For airplanes with option 033F003 installed: Within 12 months after the effective date of this AD, do the actions in Table 2 of this AD in accordance with the Accomplishment Instructions of AvCraft Service Bulletin SB-328J-00-198, dated August 23, 2004. Table 2.—Requirements for Airplanes With Option 033F003 Installed Do the following actions— By accomplishing all the actions specified in— (1) Modify the electrical wiring of the left-hand and right-hand fuel pumps Paragraph 2.B(1) of the service bulletin. (2) Replace the wiring harness of the auxiliary fuel system with a new wiring harness Paragraph 2.B(2) of the service bulletin. (3) Install markings at fuel wiring harnesses Paragraph 2.B(3) of the service bulletin. (4) Install insulated couplings in the fuel system Paragraph 2.B(5) of the service bulletin. Revision to Airworthiness Limitations (h) Within 12 months after the effective date of this AD, revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness to incorporate the information in AvCraft Temporary Revision (TR) ALD-028, dated October 15, 2003, into the AvCraft 328JET Airworthiness Limitations Document. Thereafter, except as provided in paragraph (i) of this AD, no alternative inspection intervals may be approved for this fuel tank system. Note 1: This may be done by inserting a copy of AvCraft TR ALD-028, dated October 15, 2003, in the AvCraft 328JET Airworthiness Limitations Document. When this TR has been included in general revisions of the AvCraft 328JET Airworthiness Limitations Document, the temporary revision no longer needs to be inserted into the revised Airworthiness Limitations document. Alternative Methods of Compliance (AMOCs) (i) The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. Related Information (j) German airworthiness directives D-2005-002 (for airplanes with option 033F003 installed) and D-2005-063 (for airplanes without option 033F003 installed), both dated January 26, 2005, also address the subject of this AD. Material Incorporated by Reference (k) You must use the applicable documents in Table 3 of this AD to perform the actions that are required by this AD, unless the AD specifies otherwise. (Only the odd-numbered pages of AvCraft Service Bulletins SB-328J-00-197 and SB-328J-00-198 contain the issue date of the documents.) The Director of the Federal Register approves the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get copies of the service information, contact AvCraft Aerospace GmbH, P.O. Box 1103, D-82230 Wessling, Germany. To view the AD docket, go to the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC. To review copies of the service information, go 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/cfr/ibr-locations.html . Table 3.—Material Incorporated by Reference Service information Date AvCraft Service Bulletin SB-328J-00-197, including Price Information Sheet August 23, 2004. AvCraft Service Bulletin SB-328J-00-198, including Price Information Sheet August 23, 2004. AvCraft Temporary Revision ALD-028 to the AvCraft 328JET Airworthiness Limitations Document October 15, 2003. Issued in Renton, Washington, on July 20, 2005. Kevin M. Mullin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-14789 Filed 7-29-05; 8:45 am] BILLING CODE 4910-13-P

Unsafe condition

This AD was prompted by the results of fuel system reviews conducted by the airplane manufacturer. We are issuing this AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.

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