AD 2000-20-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-8 | Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes |
Unsafe Condition
Fatigue cracks in the fuselage skin and doublers at the corners of the doorjambs of the passenger and service doors, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracks at the corners of the doorjambs of the passenger and service doors. For Group 1 airplanes, perform an initial inspection. For other airplanes, install a preventative modification and then inspect for cracks at the corners of the doorjambs. Take follow-on or corrective actions as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 17,000 landings following accomplishment of the modification specified in the service bulletin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model DC-8 series airplanes, as listed in McDonnell Douglas Service Bulletin DC8-53-075, dated August 17, 1995; certificated in any category.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.