AD 2003-14-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed | 382G | Airworthiness Directives; Lockheed Model 382G Series Airplanes |
Unsafe Condition
Failure of the latch mechanism located inside the emergency exit door, which could result in the inability to open the door in an emergency.
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Required Actions
Within 30 days after the effective date, perform a general visual inspection of bearings with part numbers 3326653-1 and 3326653-2 for evidence of a groove greater than 0.060 inch deep. If a groove is found, repair the bearings before further flight. If no groove is found, repeat the inspection at 30-day intervals until the repair is completed. Repair the bearings within 90 days after the effective date to terminate further inspections.
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Compliance Time
Within 30 days for initial inspection, 90 days for repair, and 30-day intervals for subsequent inspections until repair is completed.
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Affected Aircraft
Lockheed Model 382G series airplanes, as listed in Hercules Service Bulletin 382-52-9, dated July 5, 2000, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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