AD 80-26-51
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-100 Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-200 Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-200C Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-300 Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-400 Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-500 Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-600 Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-700 Series | BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-800 Series | BOEING Model 737 Series Airplanes |
Unsafe Condition
Control system jamming due to improper installation of bolt assemblies at the upper and lower clevis of each elevator power control unit input rod assembly.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect bolt assemblies at the upper and lower clevis of each elevator power control unit input rod assembly for proper installation per Boeing Alert Service Bulletin 27A1109 or later FAA-approved revisions. Reinstall improperly installed bolt assemblies as required by the service bulletin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 150 hours time-in-service after the effective date
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Affected Aircraft
Boeing Model 737 series airplanes certificated in all categories, prior to line number 726.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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