AD 88-24-01
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
Failure of the main landing gear support link shaft could result in damage to the wing and/or hydraulic system.
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Required Actions
Perform ultrasonic inspections for cracks of the main landing gear support link at intervals not to exceed 1,000 hours time-in-service. Conduct visual and magnetic particle inspections for corrosion and cracks, repair or replace components as needed, and replace or modify the support link and bushing according to specified service bulletins.
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Compliance Time
Within the next 1,000 hours time-in-service since the last inspection or within the next 6,000 hours time-in-service or 2 years after the effective date of this AD, whichever occurs sooner.
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Affected Aircraft
Boeing Model 727 series airplanes listed in Boeing Service Bulletin 727-32-306, Revision 1, dated February 25, 1988, 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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