AD Amdt-39-11192
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-200C | Airworthiness Directives; Boeing Model 737-200C Series Airplanes |
Unsafe Condition
Cracking of the fuselage skin in the lower lobe cargo compartment and frames between stringers 19 left and 25 left at body stations 360 to 500B, which could lead to opening or loss of the cargo door during flight and consequent rapid decompression.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Accomplish the previously optional terminating modification to prevent cracking in the fuselage skin and frames. This modification constitutes terminating action for repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Boeing Model 737-200C 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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