Turbulent Air Penetration Speed: A. Allows the other outflow valve to take full control of cabin pressure. The autopilot will normally be used for the descent. Calling the checklist complete is a last safeguard that everything is in order. Be aware of possible asymmetrical thrust condition depending upon individual engine start and acceleration times. The Captain will be prepared to perform the rejected takeoff maneuver, if required.
Initiates maximum reverse thrust consistent with runway and aircraft conditions. If directional control becomes marginal during deceleration return the reverse lever to the idle detent. Each checklist item will be treated separately, read in a command tone, and answered only when the challenged action has been completed and is in agreement with the appropriate response. Notify of abnormal aircraft conditions and the decision to evacuate or not. Checklists must be continued until the flight crew reaches an end-of-procedure symbol four centered asterisks. Maximum Operating Pressure Altitude: 43,100 feet 2.
C1 And C2 Demand Pump Selectors. Each kit is divided into two separate compartments. The procedure can be used at any speed or altitude in the aircraft's operating envelope. For the safety of the personnel evacuating, ensure positive shutdown of both engines when the decision is made to evacuate the aircraft. This certain point or time is a bottom line for prompting a checklist.
The crew does not accomplish these checklists. Seat passengers with life vests on and seat belts fastened. Loss of R or c hydraulic systems results in loss of only one hydraulic actuator. Smoothly apply rudder proportionate to thrust decay. Restores flight control normal mode following reversion to secondary mode caused by loss of pitot heat. Use flch for level off in these circumstances.
If magnetic compass information is unreliable or unavailable, track information may be used. If a battery start is required battery powers left start valve only or left engine must be started first for operational reasons, the pneumatic air cart s may be positioned on the right side of the aircraft and the left engine started first. E crew in evacuating aircraft. Provides air ventilation to cabin. Tire and brake replacement may be required.
Repeat procedure to start remaining engine. Flight Controls: Takeoff is permitted only in the normal flight control mode. The aircraft may remain afloat indefinitely if fuel load is minimal and no serious damage was sustained during landing. All are obligated to seek and give information. The autoland system is not certified for overweight landings.
Put on life vest, shoulder harness, and seat belts. Notes, information items, and condition statements are read aloud. Place Fuel Control Switch to run when engine reaches max motoring, minimum N2 22%. This will indicate to the pilot that only one of the connected procedures should be performed and all others ignored. If the autopilots are disconnected, be prepared to maintain required rudder pedal pressure. Aircraft response is changed by simplified elevator feel and rudder ratio systems. With incorrect settings the normal amber colored font reminder will be incorrect.
The Crew Effectiveness Markers can also serve as a debriefing tool after a line flight or training event. Single engine taxi to the gate is permissible at Captain's discretion. At high altitude thrust deterioration or engine flameout may occur. Adjust pitch attitude, as required, to maintain desired airspeed of V 2 to V 2 + 15. Engines may accelerate to idle slowly.
Continental Flight Manual The maximum operating limit speed shall not be deliberately exceeded in any regime of flight. If a fire exists, the Flight Attendant will attempt to extinguish it. If the decision is to continue to another airport, flaps should be retracted on schedule. Valve may take up to 6 seconds to begin moving. Additional procedures and information are presented as necessary. Non-normal procedures are presented in expanded format grouped by aircraft system. If the autothrottle is engaged, do not increase command speed until target speed is reached.