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Airworthiness directives › 2023-11-10

AD 2023-11-10 Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

Superseded. This directive was replaced by AD 2024-01-02. Work to the current one.
2023-07-11
2023-06-26
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Airframe
2024-01-02

Models named: 382, 382B, 382E, 382F, 382G, 382J, C-130A, C-130B, HP-C-130A, EC-130Q. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to all airplanes specified in paragraphs (c)(1) through (2) of this AD, certificated in any category. (1) Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, 382G, and 382J airplanes. (2) The airplanes specified in paragraphs (c)(2)(i) through (xi) of this AD, type certificated in the restricted category. (i) LeSEA Model C-130A airplanes (transferred from Central Air Services, Inc.), Type Certificate Data Sheet (TCDS) A34SO, Revision 1. (ii) T.B.M., Inc., Model C-130A airplanes, TCDS A39CE, Revision 3. (iii) Western International Aviation, Inc., Model C-130A airplanes, TCDS A33NM. (iv) USDA Forest Service Model C-130A airplanes, TCDS A15NM, Revision 4. (v) Snow Aviation International, Inc., Model C-130A airplanes, TCDS TQ3CH, Revision 1. (vi) International Air Response (transferred from Rogers Helicopters, Inc., and Heavylift Helicopters Inc.) Model C-130A airplanes, TCDS A31NM, Revision 3. (vii) Heavylift Helicopters, Inc., Model C-130B airplanes, TCDS A35NM, Revision 1. (viii) Hawkins & Powers Aviation, Inc., Model HP-C-130A airplanes, TCDS A30NM, Revision 1. (ix) Coulson Aviation (USA), Inc., Model EC-130Q and C-130H airplanes, TCDS T00019LA, Revision 4. (x) Lockheed-Georgia Company Model 282-44A-05 (C-130B) airplanes, TCDS A5SO. (xi) Surplus Model C-130A airplanes.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

For all airplanes except Model 382J airplanes: Within 35 days after the effective date of this AD, review the airplane maintenance records to determine if the left or right aft fuselage sloping longeron, having part number (P/N) 342986-( ), has been replaced on or after December 31, 2012.

Unsafe condition

This AD was prompted by a report indicating a quality audit found aft fuselage sloping longerons manufactured with an overaged condition ( i.e., understrength). The FAA is issuing this AD to address the possibility of both aft sloping longerons being understrength, which would reduce the structural integrity of the airplane below limit load ( i.e., maximum load to be expected in service) and could lead to failure of both longerons. The unsafe condition, if not addressed, could result in loss of the airplane.

Affected ADs

None.

Read the original on the Federal Register →

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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