AD 2007-16-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | M7 | Aerospace LP SA226 and SA227 Series | Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes |
Unsafe Condition
Excessive freeplay or rod slippage in the pitch trim actuator could result in pitch trim actuator failure, which could lead to possible loss of control.
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Required Actions
Inspect, overhaul, or replace pitch trim actuators as required. Replace certain part number (P/N) pitch trim actuators with an improved design. Revise the FAA-approved airplane flight manual (AFM) to remove limitations once the improved design is installed.
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Compliance Time
Within 12 months of the effective date (September 7, 2007)
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Affected Aircraft
M7 Aerospace LP SA226 and SA227 series airplanes equipped with certain pitch trim actuators, including models SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, and others as specified.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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