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2003-17-05R1: Replacement os certain life limited items

FAA order 2003-17-05R1 is an airworthiness directive in force since March 23, 2007. The FAA's subject line: Replacement os certain life limited items. It names Short Bros. & Harland SC-7: about 27 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Short Brothers PLC
Models
SC-7 Skyvan Series 2, SC-7 Skyvan Series 3
On this site
Short Bros. & Harland SC-7 27 registered

Dates and paperwork

In force since
March 23, 2007
Published
February 16, 2007 (signed February 8, 2007)
Docket
FAA-2006-25926
Replaces
2003-17-05
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) to revise AD 2003-17-05, which applies to Short Brothers & Harland (Shorts) Models SC-7 Series 2 and SC-7 Series 3 airplanes. AD 2003-17-05 currently establishes a technical service life for these airplanes and allows you to incorporate modifications, inspections, and replacements of certain life limited items to extend the life limits of these airplanes. Since we issued AD 2003-17-05, Shorts Service Bulletin SB 51-51 was revised to Revision 8, dated July 5, 2006, and the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, issued an AD for the European Community to correct an unsafe condition for the specified product. AD 2003-17-05 contains conflicting information on the repetitive visual inspection requirement. Consequently, this AD would retain the technical service life for these airplanes; would continue to allow modifications, inspections, and replacementsof certain life limited items to extend the life limits of these airplanes; and would clarify the repetitive visual inspection requirement between one of the service bulletins and the maintenance program if an operator chooses to extend the life limit. The actions specified by this AD are intended to clarify the inspection information to prevent failure of critical structure of the aircraft caused by fatigue.

The order itself the regulatory text, as published

Show the full text (7,185 characters)
2003-17-05R1 Short Brothers & Harland Ltd.: Amendment 39-14946; Docket No. FAA-2006-25926; Directorate Identifier 2000-CE-17-AD. Effective Date (a) This AD becomes effective on March 23, 2007. Affected ADs (b) This AD revises AD 2003-17-05, Amendment 39-13279. Applicability (c) This AD applies to Models SC-7 Series 2 and SC-7 Series 3 airplanes, all serial numbers, that are certificated in any category. Unsafe Condition (d) This revised AD results from conflicting information of the repetitive inspection requirement between one of the service bulletins and the maintenance program if an operator chooses to extend the life limit. We are issuing this AD to clarify the inspection information to prevent failure of critical structure of the aircraft caused by fatigue. Compliance (e) Do not operate the airplane upon accumulating the applicable life limit or within the next 90 days after September 29, 2003 (the effective date of AD 2003-17-05), whichever occurs later. For owners/operators that do not have a record of the number of flights on the aircraft, assume the number of flights on the basis of two per operating hour. The following table presents the life limits: Table 1.--Original Life Limits Serial Number Life Limit (1) SH1845 and SH1883 10,000 hours time-in-service (TIS) (2) SH1847 15,200 hours TIS (3) SH1889 13,805 flights (4) SH1943 11,306 flights (5) SH1960 4,142 flights (6) All airplanes that do not have serial number SH1845, SH1883, SH1847, SH1889, SH1943, or SH1960. 20,000 flights (f) For airplanes with serial numbers SH1845, SH1847, or SH1883: You can extend the life limits by doing the actions of Shorts Service Bulletin No. 51-52, Revision No.: 4, dated: July 16, 2002 (and all service information or modifications referenced in the Planning Information section of the service bulletin), and Shorts Skyvan Maintenance Program, Amendment List No. 22, dated May 7, 2003, or Amendment ListNo. 23, dated December 14, 2004, or Amendment List No. 24, dated November 2, 2006. You may use any future amendment to this maintenance program if it does not change the inspection intervals, requirements, or the life limits of this AD or the previous amendments. The following table presents the extended life limit: Table 2.--Extended Life Limits After Incorporation of Required Inspections and Modifications (1) SH1845: 13,456 hours TIS. (2) SH1847: 20,200 hours TIS. (3) SH1883: 15,000 hours TIS. (g) For airplanes with serial numbers SH1889, SH1943, or SH1960: You can extend the life limits by doing the actions of Shorts Service Bulletin No. 51-52, Revision No.: 4, dated: July 16, 2002 (and all service information or modifications referenced in the Planning Information section of the service bulletin including Shorts Service Bulletin No. 51-51, Revision No.: 6, dated: March 14, 1983; or Shorts Service Bulletin No. 51-51, Revision No.: 8, dated: July 5, 2006. Youcannot use Shorts Service Bulletin No. 51-51, Revision No.: 7, dated: January 2005.), and Shorts Skyvan Maintenance Program, Amendment List No. 22, dated May 7, 2003, or Amendment List No. 23, dated December 14, 2004, or Amendment List No. 24, dated November 2, 2006. You may use any future amendment to this maintenance program if it does not change the inspection intervals, requirements, or the life limits of this AD or the previous amendments. The following table presents the extended life limit: Table 3.--Extended Life Limits After Incorporation of Required Inspections and Modifications Serial Number Extended Life Limit (1) SH1889: 20,094 flights. (2) SH1943: 17,325 flights. (3) SH1960: 8,449 flights. (h) For airplanes that do not have serial numbers SH1845, SH1847, SH1883, SH1889, SH1943, or SH1960: You can extend the life limit to 27,000 flights by doing the actions of Shorts Service Bulletin No. 51-51, Revision No.: 6, dated: March 14, 1983; or Shorts Service Bulletin No. 51-51, Revision No.: 8, dated: July 5, 2006; and Shorts Skyvan Maintenance Program, Amendment List No. 22, dated May 7, 2003; or Amendment List No. 23, dated December 14, 2004 or Amendment List No. 24, dated November 2, 2006. You may use any future amendment to this maintenance program if it does not change the inspection intervals, requirements, or the life limits of this AD or the previous amendments. You cannot use Shorts Service Bulletin No. 51-51, Revision No.: 7, dated: January 2005. (i) The repetitive visual inspection requirements using Shorts Service Bulletin No. 57-59, which is referenced on page 3 of Shorts Service Bulletin No. 51-51, Revision No.: 6, dated: March 14, 1983, paragraph C (Special limitations) are every 2,400 flights; and the repetitive visual inspection program in Skyvan Maintenance Program, Maintenance Program Appendix 1, parts A and B (Section 57-00, Item 3) are every 1,100 flights or 800 hours TIS intervals, whichever occurs first. Youmust use the repetitive inspection intervals of the Skyvan Maintenance Program for the repetitive inspection of the wing structure, skin, and skin doublers to be every 1,100 flights or 800 hours TIS, whichever occurs first and not the 2,400 flights as stated in Shorts Service Bulletin No. 51-51, Revision No.: 6, dated: March 14, 1983. Alternative Methods of Compliance (AMOCs) (j) The Manager, Standards Office, Small Airplane Directorate, FAA, ATTN: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4059; facsimile: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. (k) AMOCs approved for AD 2003-17-05 are approved for this AD. Material Incorporated by Reference (l) You must use Shorts Service Bulletin Number 51-52, Revision No: 4, dated July 16, 2002; or Shorts Service Bulletin Number 51-51, Revision No: 6,dated March 14, 1983; or Shorts Service Bulletin Number 51-51, Revision No: 8, dated July 5, 2006, 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 Shorts Service Bulletin Number 51-51, Revision No: 8, dated July 5, 2006, under 5 U.S.C. 552(a) and 1 CFR part 51. (2) The Director of the Federal Register previously approved the incorporation by reference of Shorts Service Bulletin No. 51-51, Revision No.: 6, dated: March 14, 1983; and Shorts Service Bulletin No. 51-52, Revision No.: 4, dated: July 16, 2002, on September 29, 2003 (68 FR 50689, August 22, 2003). (3) For service information identified in this AD, contact Short Brothers PLC, P.O. Box 241, Airport Road, Belfast BT3 9DZ Northern Ireland; telephone: 011 44 (0) 28 9045 8444; facsimile: 011 44 (0) 28 9073 3396. (4) You may review copies at the FAA, FAA, Central Region, Office of the Regional Counsel, 901 Locust, 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/code_of_federal_regulations/ibr_locations.html .

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 26, 2026. Connections as data: /graph/directive/2003-17-05R1.json · aircraft systems.