AD 2008-05-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-100 | Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes |
Unsafe Condition
Fatigue cracking in the longitudinal floor beam web, upper chord, and lower chord at certain body stations could result in rapid loss of cabin pressure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the longitudinal floor beam web, upper chord, and lower chord for fatigue cracking at specified body stations. Repair any detected cracks as necessary.
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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 737-100, -200, -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 4, 2026
Rights: U.S. Government Public Domain
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