AD 2015-19-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | M7 | Aerospace LLC | Airworthiness Directives; M7 Aerospace LLC Airplanes |
Unsafe Condition
Loss of elevator control due to failure of the bolt attaching the elevator control rod to the elevator walking beam under the cockpit floor.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for movement and correct torque of the elevator control pivot bearing. Inspect the elevator control rod for damage and correct configuration. Replace parts as necessary. Require a 10,000-hour time-in-service (TIS) repetitive replacement of the control column pivot bearing and elevator control rod bolt. Replace the control column pivot bearing with the improved design by 35,000 hours TIS.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of effective date (November 3, 2015).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
M7 Aerospace LLC Models SA26-AT, SA26-T, SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.