AD 2001-26-03

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes

AD Number
2001-26-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-282-AD
FR Citation
66 FR 66299

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-8 Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes

Unsafe Condition

Opening of the cargo door while the airplane is in flight or collapse of the main deck cargo floor, and consequent rapid decompression of the airplane including possible loss of flight control or severe structural damage.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Modify the main deck cargo door structure and fuselage structure; modify a main deck cargo door hinge; modify the main deck cargo floor; install a main deck cargo 9g crash barrier.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 3 years or 4,000 flight hours after the effective date of this AD, whichever occurs first.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

McDonnell Douglas Model DC-8 series airplanes that have been converted from a passenger- to a cargo-carrying (``freighter'') configuration in accordance with Supplemental Type Certificate (STC) SA1832SO.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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