AD 95-02-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 757-200 Series | Airworthiness Directives; Boeing Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-200CB Series | Airworthiness Directives; Boeing Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-200PF Series | Airworthiness Directives; Boeing Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-300 Series | Airworthiness Directives; Boeing Model 757 Series Airplanes |
Unsafe Condition
Damage to the left inboard trailing edge flap during flap retraction after landing, caused by sheared titanium bolts attaching the Number 4 transmission bracket to the flap track structure, which do not meet the designed limit load.
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Required Actions
Replace the bolts, nuts, and washers (kit number 012N8037) attaching the support bracket at the Number 4 and Number 5 transmissions to the inboard trailing edge flap system with Inconel 718 material, following Boeing Alert Service Bulletin 757-27A0118. Compliance must be within 60 days after the effective date of this AD.
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Compliance Time
Within 60 days after the effective date of this AD
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Affected Aircraft
Boeing Model 757 series airplanes having line numbers 181 through 647 inclusive, 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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