AD 94-07-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 727-100 Series | Airworthiness Directives; Boeing Model 727 Series Airplanes |
| aircraft | The Boeing Company | 727-100C Series | Airworthiness Directives; Boeing Model 727 Series Airplanes |
| aircraft | The Boeing Company | 727-200 Series | Airworthiness Directives; Boeing Model 727 Series Airplanes |
| aircraft | The Boeing Company | 727-200F Series | Airworthiness Directives; Boeing Model 727 Series Airplanes |
| aircraft | The Boeing Company | 727 Series | Airworthiness Directives; Boeing Model 727 Series Airplanes |
| aircraft | The Boeing Company | 727C Series | Airworthiness Directives; Boeing Model 727 Series Airplanes |
Unsafe Condition
Fatigue cracking and corrosion in transport category airplanes that are approaching or have exceeded their economic design service goal.
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Required Actions
Accomplish inspections specified in Section 4 and Appendices A.4 and B.4 of Boeing Document D6-54860, Revision G, within the times specified in paragraph (b) of this AD, and thereafter at intervals not to exceed those specified in the Boeing Document. If any discrepant condition is found, accomplish the corresponding corrective action prior to further flight.
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Compliance Time
Prior to the later of the times specified in either paragraph (b)(1) or (b)(2) of this AD, which calculates based on threshold inspection times in the Boeing Document or 15 months after the effective date of this AD (April 28, 1994).
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Affected Aircraft
Boeing Model 727 series airplanes as listed in Boeing Document D6-54860, Revision G, including 727-100, 727-100C, 727-200, 727-200F, 727 Series, and 727C Series models.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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