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References in periodicals archive ?
Based on the observed weather at the destination, the pilot should have turned on the airplane's engine anti-ice system, an action required by the airplane flight manual when the total air temperature is below 10 C with visible moisture (including clouds).
The existing AD currently requires, for certain aircraft, a revision of the Airplane Flight Manual, and, for all aircraft, the performance of repetitive inspections to check for wear or damage of the inlet check valves and inlet adapters of the override/jettison pumps, and corrective action if necessary.
This required a novel approach, and I talked the FAA into approving a training requirement in the Limitations Section of the Eclipse 500's Airplane Flight Manual. The limitation's full quote is in the text box at right.
The current AD requires a revision of the Airplane Flight Manual (AFM) to include requirement for the activation of ice protection systems, as well as to add information regarding operation during icing conditions, the installation of an ice detector system and a revision of the AFM to include procedures for testing system integrity.
Other operating limitations which must be complied with when operating th is airplane in this category are contained in the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual.
Also applicable on this date and to the above Airbus Model aircraft is a new AD that requires revision of the Airplane Flight Manual, inspection to detect damage of the wiring and adjacent structure along the length of the fairing of the fuel boost pump, and corrective actions if necessary.
Pilots should study their Pilot's Operating Handbook or Airplane Flight Manual, as well as any autopilot-specific supplements or pilot's guides from its manufacturer, to learn the autopilot's operation and how it is integrated into the airplane's other systems.
This AD would require a revision of the Airplane Flight Manual and is necessary to provide flight crew with procedures to maintain aircraft controllability in the event of an in-flight thrust reverser deployment.
A placard was located on the cockpit pedestal immediately aft of the lift dump switch that read, "WARNING DO NOT EXTEND IN FLIGHT." The airplane flight manual states, "Do not extend lift dump in flight."
The current AD requires a revision of the Airplane Flight Manual (AFM) to include procedures that prevent dry operation of the centre wing fuel tank override/jettison pumps and, for certain aircraft, prohibit operation of the horizontal stabiliser tank transfer pumps in-flight.
According to the airplane flight manual, the starting engines checklist indicates that both fuel selectors are to be moved to on.
The AD supersedes AD 99-05-15, amendment 39-11063, to require a revision of the FAA-approved Airplane Flight Manual (AFM) procedure in the existing AD to simplify the instructions for correcting a jammed or restricted flight control condition.