AD 2013-13-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Pilatus | Aircraft Ltd | Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes |
Unsafe Condition
Need to incorporate new revisions into the Limitations section of the FAA-approved maintenance program, including an emergency fuel control system adjustment test.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 90 days after August 14, 2013, and repetitively thereafter at intervals not exceeding 300 hours time-in-service, perform the Emergency Fuel Control System-Adjustment/Test following specified procedures. If a discrepancy is found that is not identified in the referenced document, contact Pilatus Aircraft Ltd. for an FAA-approved repair scheme and incorporate the repair before further flight.
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Compliance Time
Within 90 days after August 14, 2013, and repetitively thereafter at intervals not exceeding 300 hours time-in-service.
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Affected Aircraft
PILATUS Aircraft Ltd. Model PC-7 airplanes, all serial numbers, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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