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The selection of data by the handbook producer, to be included in this Section shall be governed by the concepts contained in the preface of this Specification.
Remove the test cap on the control pressure sense line from the Precooler Control Valve to the 3908 sensor and make sure air flows out of the test port.
The airworthiness concern requires prompt action, based on the potential for having similar or more severe corrosion on any other airplane in the operator＇s fleet, prior to the next scheduled inspection of that area.
This data sheet prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements.
This is the minimum concentration of flammable vapors in air below which propagation of flame does not occur on contact with a source of ignition.
The purpose of the autopilot actuator is to change electrical commands from the FCC into a hydraulically controlled mechanical output.The outputs of the actuators become inputs to the aileron and the elevator power control units(PCU).
The mach trim actuator also causes the elevator to be in a more nose down position during takeoff which allows the pilots to move the stabilizer to a more nose up position.
The trailing edge flaps up limit switch sends flap position data to SMYD1.The SMYD1 uses this during yaw damping to limit rudder movement when flaps are up.
Where possible, examples, associated conditions and technique should be presented on the same page as the chart. If space is not sufficient to include the necessary information, then the page facing the chart should be used.
An “emergency” however, almost always involves a failure that requires immediate and rapid response, such as a total powerplant failure, fire or smoke, or rapid cabin decompression.
