AD 2005-07-18
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-9-15F | Airworthiness Directives; McDonnell Douglas Model DC-9-15F Airplanes Modified In Accordance With Supplemental Type Certificate (STC) SA1993SO; and Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes in All-Cargo Configuration, Equipped With a Main-Deck Cargo Door |
Unsafe Condition
Deficiencies related to the cargo loading system may exist, potentially leading to failure of components of the cargo loading system, failure of the floor structure, or shifting of cargo. These conditions could cause cargo to exceed load distribution limits or cause damage to the fuselage or control cables, which could result in reduced controllability of the airplane.
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Required Actions
Inspect to determine the airplane's cargo configuration and report findings to the FAA. Revise certain manuals and manual supplements to specify cargo limitations for airplanes modified in accordance with STC SA1993SO or with a cargo configuration that deviates from the as-delivered configuration. Relocate all cargo restraints on the main cargo deck.
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Compliance Time
Within 60 days after the effective date of May 11, 2005.
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Affected Aircraft
McDonnell Douglas Model DC-9-15F airplanes modified in accordance with Supplemental Type Certificate (STC) SA1993SO; and Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes in all-cargo configuration, equipped with a main-deck cargo door.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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