AD 2000-20-08

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes

AD Number
2000-20-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-NM-135-AD
FR Citation
65 FR 59701

Applicability

TypeManufacturerModelDetails
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.