Airworthiness directives › 2012-06-09
AD 2012-06-09 Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes
Models named: 382, 382B, 382E, 382F, 382G. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G airplanes, certificated in any category.
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.
Required actions
Within 12 months after the effective date of this AD, incorporate a revision into the maintenance inspection program that provides no less than the required damage tolerance assessment/analysis (DTA) for each structural significant item (SSI) listed in Lockheed Martin Model 382, 382B, 382E, 382F, and 382G Series Aircraft Service Manual Publication (SMP), Supplemental Structural Inspection Document (SSID), SMP 515-C-SSID, Change 1, dated September 10, 2007. (The required inspection interval for each principal structural element (PSE) is listed in Lockheed Martin Model 382, 382B, 382E, 382F, and 382G Series Aircraft Service Manual Publication (SMP), Supplemental Structural Inspection Document (SSID), SMP 515-C-SSID, Change 1, dated September 10, 2007.) The revision to the maintenance inspection program must include and must be implemented in accordance with the procedures in Section 5.0 (Damage Tolerance Analysis Methodology), Section 6.0 (Structural Inspection Requirements), and Section 7.0 (Discrepancy Reporting) of Lockheed Martin Model 382, 382B, 382E, 382F, and 382G Series Aircraft Service Manual Publication (SMP), Supplemental Structural Inspection Document (SSID), SMP 515-C-SSID, Change 1, dated September 10, 2007. One report may be used to report findings for both the service difficulty report and this AD, provided the report refers to this AD and the PSE number for the inspection being accomplished when the discrepancy was found. Note 1 to paragraphs (g) through (p) of this AD: Compliance with the requirements of this AD establishes compliance with section 121.1109(c)(1) of the Federal Aviation Regulations (14 CFR 121.1109(c)(1)).
Unsafe condition
Air Transport Association (ATA) of America Code 51: Standard Practices/Structures.
Affected ADs
None.
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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