AD 2005-19-25
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-100 | Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes |
Unsafe Condition
Fatigue cracks of the countersunk rivet holes in the lower lobe, adjacent to the radio altimeter cutouts, which could result in cracks of the fuselage skin of the lower lobe and consequent rapid depressurization of the cabin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive eddy current inspections for cracks of the countersunk rivet holes in the lower lobe, adjacent to the radio altimeter cutouts. Perform additional inspections, for certain airplanes, for cracks and/or corrosion. Take further investigative and corrective action if any crack is found. Optional terminating action is provided for the repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of the AD.
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Affected Aircraft
Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes.
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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