AD Amdt-39-10487
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier Model CL-215-6B11 (CL-415 Variant) Series Airplanes |
Unsafe Condition
Temporary loss of battery bus power during engine failure and consequent erroneous indications of hydraulic system pressure, brake pressure, rudder pressure, and rudder and elevator reversion to manual mode.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the Airplane Flight Manual (AFM) to provide flightcrew procedures addressing temporary battery bus power loss during engine failure and erroneous indications.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier Model CL-215-6B11 (CL-415 Variant) series 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
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