AD 87-22-06
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
The main landing gear door release lever may move to the door open position during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the left and right main landing gear door release levers in accordance with Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, or later FAA-approved revision. Alternate means of compliance or adjustment may be used with FAA concurrence.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 4,500 hours time-in-service or 2 years after the effective date of this AD, whichever occurs first
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Affected Aircraft
Boeing Model 727 series airplanes as listed in Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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