Airworthiness directives › 2005-13-03
AD 2005-13-03 Airworthiness Directives; AvCraft Dornier Model 328-100 and -300 Airplanes
Models named: 328-100, -300 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to AvCraft Dornier Model 328-100 and -300 series airplanes, certificated in any category; as identified in Dornier Service Bulletin SB-328J-27-176, Revision 1, dated April 15, 2003; and Dornier Service Bulletin SB-328-27-436, Revision 1, dated April 15, 2003; as applicable.
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. Installation (f) Within 24 months after the effective date of this AD, install colored identification strips on the pulley brackets, fairlead bracket assemblies, operational assemblies, and flight control cables, in accordance with the Accomplishment Instructions of Dornier Service Bulletin SB-328J-27-176, Revision 1, dated April 15, 2003; or Dornier Service Bulletin SB-328-27-436, Revision 1, dated April 15, 2003; as applicable. Prior or Concurrent Requirements (g) Prior to or concurrently with the accomplishment of the actions in paragraph (f) of this AD, accomplish the actions in the applicable service bulletins listed in Table 1 of this AD. Table 1.—Prior or Concurrent Requirements Model Dornier Service Bulletin Revision Date Action 328-100 airplanes SB-328-27-290 1 December 8, 2000 Relocate the auto-pilot rudder servo. SB-328-27-291 1 December 8, 2000 Relocate the auto-pilot aileron servo. SB-328-27-292 1 December 8, 2000 Relocate the auto pilot elevator servo. 328-300 airplanes SB-328J-27-035 Original April 25, 2000 Relocate the auto-pilot rudder servo. SB-328J-27-036 Original April 25, 2000 Relocate the auto-pilot elevator servo. SB-328J-27-037 Original April 25, 2000 Relocate the auto-2000 pilot aileron servo. Alternative Methods of Compliance (AMOCs) (h) 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 (i) German airworthiness directive 2003-376, effective November 11, 2003; and German airworthiness directive 2003-377, effective November 11, 2003; also address the subject of this AD. Material Incorporated by Reference (j) You must use the applicable service bulletins in Table 2 of this AD to perform the actions that are required by this AD, unless the AD specifies otherwise. 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/code_of_federal_regulations/ibr_locations.html . Table 2.—Material Incorporated by Reference Dornier service bulletin Revision level Date SB-328-27-290 1 December 8, 2000. SB-328-27-291 1 December 8, 2000. SB-328-27-292 1 December 8, 2000. SB-328-27-436 1 April 15, 2003. SB-328J-27-035 Original April 25, 2000. SB-328J-27-036 Original April 25, 2000. SB-328J-27-037 Original April 25, 2000. SB-328J-27-176 1 April 15, 2003. Issued in Renton, Washington, on June 10, 2005. Michael J. Kaszycki, Acting Manager, Transport Airplane Directorate,Aircraft Certification Service. [FR Doc. 05-12001 Filed 6-20-05; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD was prompted by a report that the flight control systems do not have elements that are distinctively identified. We are issuing this AD to prevent the incorrect re-assembly of the flight control system during maintenance, which could result in reduced controllability of the airplane.
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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