AD Amdt-39-11838
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 727 | Airworthiness Directives; Boeing Model 727 Series Airplanes Modified in Accordance with Valsan Supplemental Type Certificate (STC) SA4363NM |
Unsafe Condition
The nut coming off the through-bolt, allowing the through-bolt to migrate out of the engine mount flange and cone bolt, and possible separation of the engine.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the through-bolt nut for proper torque and specified conditions within 48 clock hours after receiving the telegraphic AD. Repeat inspections at intervals not exceeding 35 flight hours. Install anti-rotation plates within 60 days after July 31, 1990, to terminate repetitive inspections. Submit a report of any discrepancies within 10 days after performing the initial inspection.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 48 clock hours for initial inspection, 35 flight hours for subsequent inspections, and 60 days after July 31, 1990, for anti-rotation plate installation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 727 series airplanes modified by the installation of Pratt and Whitney JT8D-217C or -219 engines in accordance with Valsan Supplemental Type Certificate (STC) SA4363NM.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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