AD 93-08-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-100 Series | Airworthiness Directives; BOEING Model 737-100, -200, and -200C Series Airplanes |
| aircraft | The Boeing Company | 737-200 Series | Airworthiness Directives; BOEING Model 737-100, -200, and -200C Series Airplanes |
| aircraft | The Boeing Company | 737-200C Series | Airworthiness Directives; BOEING Model 737-100, -200, and -200C Series Airplanes |
Unsafe Condition
Degradation of the structural capability of the airplane due to aging-related structural issues requiring inspections and modifications as specified in Boeing Document D6-38505.
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Required Actions
Accomplish inspections specified in Boeing Document D6-38505 within the times specified in paragraph (b) of the AD, and thereafter at intervals not exceeding those in the document. If discrepant conditions are found, perform corrective actions prior to further flight. Modifications specified in corresponding service bulletins must be accomplished as terminating actions.
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Compliance Time
Within the later of the threshold inspection time specified in the Boeing Document (measured as flight cycles or time-in-service) or the phase-in period starting 15 months after the AD's effective date (May 27, 1993).
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Affected Aircraft
BOEING Model 737-100, -200, and -200C Series airplanes listed in Section 4 and Appendices A.4 and B.4 of Boeing Document D6-38505, Revision F.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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