AD 64-06-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 727-100 Series | BOEING Model 727 Series Aircraft |
| aircraft | The Boeing Company | 727-100C Series | BOEING Model 727 Series Aircraft |
| aircraft | The Boeing Company | 727-200 Series | BOEING Model 727 Series Aircraft |
| aircraft | The Boeing Company | 727-200F Series | BOEING Model 727 Series Aircraft |
| aircraft | The Boeing Company | 727 Series | BOEING Model 727 Series Aircraft |
| aircraft | The Boeing Company | 727C Series | BOEING Model 727 Series Aircraft |
Unsafe Condition
Cracks in rod end fittings P/N 907 008 001 on flight spoiler actuators due to hold down load stress.
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Required Actions
Conduct daily visual inspections of rod end fittings, turn rod end out one-half turn within 25 hours' time in service for airplanes with 350+ hours, replace cracked parts, and continue daily inspections until approved redesign is incorporated.
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Compliance Time
Within the next 25 hours' time in service unless already accomplished for airplanes with 350 or more hours' time in service.
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Affected Aircraft
Boeing Model 727 Series Aircraft listed in Boeing Alert Service Bulletin No. 27-18.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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