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Airworthiness directives › 2007-14-04

AD 2007-14-04 Airworthiness Directives; Pacific Aerospace Corporation, Ltd Model 750XL Airplanes

2007-08-16
2007-07-12
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Airframe
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Makes named: pacific aerospace. Models named: 750XL. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Model 750XL airplanes, all serial numbers, that are: (1) Not fitted with modification PAC/XL/0267 (upper bearing part number (P/N) 11-33121-1); and (2) certificated in any category.

Compliance

Unless already done, do the following actions: (1) Within the next 150 hours time-in-service (TIS) after August 16, 2007 (the effective date of this AD) and thereafter at intervals not to exceed 150 hours TIS, inspect the rudder trim tab upper pivot following the instructions in Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007. (i) If there is any lateral movement of the bush found in any inspection required in paragraph (f)(1) of this AD, before further flight, install modification PAC/XL/0267 following Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007. (ii) Modification PAC/XL/0267 comprises removing the upper bush P/N 11-33119-1 and installing upper bearing P/N 11-33121-1 following Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007. Modification PAC/XL/0267 is a terminating action to the requirements of this AD. (2) Within the next 450 hours TIS after August 16, 2007 (the effective date of this AD) or within the next 24 months after August 16, 2007 (the effective date of this AD), whichever occurs first, modify the rudder trim tab upper pivot with modification PAC/XL/0267 following Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq. ), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI Civil Aviation Authority of New Zealand AD DCA/750XL/11, dated March 29, 2007; Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007, for related information. Material Incorporated by Reference (i) You must use Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Pacific Aerospace Corporation Ltd., Hamilton Airport, Private Bag HN 3027, Hamilton, New Zealand; telephone: 011 (64) 7-843-6144; fax: 011 (64) 7-843-6134. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; 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/cfr/ibr-locations.html. Issued in Kansas City, Missouri, on June 29, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-13242 Filed 7-11-07; 8:45 am] BILLING CODE 4910-13-P

Required actions

Unless already done, do the following actions: (1) Within the next 150 hours time-in-service (TIS) after August 16, 2007 (the effective date of this AD) and thereafter at intervals not to exceed 150 hours TIS, inspect the rudder trim tab upper pivot following the instructions in Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007. (i) If there is any lateral movement of the bush found in any inspection required in paragraph (f)(1) of this AD, before further flight, install modification PAC/XL/0267 following Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007. (ii) Modification PAC/XL/0267 comprises removing the upper bush P/N 11-33119-1 and installing upper bearing P/N 11-33121-1 following Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007. Modification PAC/XL/0267 is a terminating action to the requirements of this AD. (2) Within the next 450 hours TIS after August 16, 2007 (the effective date of this AD) or within the next 24 months after August 16, 2007 (the effective date of this AD), whichever occurs first, modify the rudder trim tab upper pivot with modification PAC/XL/0267 following Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Staff, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq. ), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI Civil Aviation Authority of New Zealand AD DCA/750XL/11, dated March 29, 2007; Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007, for related information. Material Incorporated by Reference (i) You must use Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/023, dated February 15, 2007; and Pacific Aerospace Ltd Drawing No. 11-03131, Drawing Approved Date: February 17, 2007, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Pacific Aerospace Corporation Ltd., Hamilton Airport, Private Bag HN 3027, Hamilton, New Zealand; telephone: 011 (64) 7-843-6144; fax: 011 (64) 7-843-6134. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; 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/cfr/ibr-locations.html. Issued in Kansas City, Missouri, on June 29, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-13242 Filed 7-11-07; 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