AD 2006-05-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes |
Unsafe Condition
Failure of the shear pin located in the input lever of the pitch feel simulator (PFS) units due to fatigue.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive functional tests of the pilot input lever of the PFS units, including determining if the lever is disconnected. Take corrective actions if necessary, such as replacing any defective PFS unit with a serviceable one. Remove existing procedures for repetitive functional tests from the aircraft maintenance manual (AMM) once new tests are initiated.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) 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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