AI.VII.G.R3b
Risk managementAbnormal operations, including planning for:
Potential engine failure in takeoff/climb phase of flight
From the FAA library
- Chapter 5. Air Traffic Procedures › Section 1. Preflight › 5-1-5. Flight Plan - VFR Flights
Flight Plan - VFR Flights (See Appendix 4, FAA Form 7233-4 – International Flight Plan) a. The requirements for the filing and activation of VFR flight plans can vary depending in which airspace the flight is operating. Pilots are responsible ... activating flight plans with a Flight Service Station. Control tower personnel do not automatically activate VFR flight plans. 1. Within the continental U.S., a VFR flight plan is not normally required. 2. VFR flights (except for DoD and law enforcement…
- Chapter 6: Takeoffs and Departure Climbs › Soft/Rough-Field Takeoff and Climb › Initial Climb
Initial Climb After a positive rate of climb is established, and the airplane has accelerated to VY, the pilot should retract the landing gear and flaps, if equipped. If departing from an airstrip with wet snow or slush ... takeoff surface, the gear should not be retracted immediately so that any wet snow or slush can be air-dried. In the event an obstacle needs to be cleared after a soft-field takeoff, the pilot should perform the climb…
- Chapter 3: Basic Flight Maneuvers › Climbs and Climbing Turns
Normal climb speed is generally higher than the airplane’s best rate of climb. The additional airspeed provides for better engine cooling, greater control authority, and better visibility over the nose of the airplane. Normal climb is sometimes referred ... cruise climb. ⦁ Best rate of climb (VY)—produces the most altitude gained over a given amount of time. This airspeed is typically used when initially departing a runway without obstructions until it is safe to transition to a normal…
- Chapter 13: Transition to Multiengine Airplanes › Engine Inoperative Flight Principles › OEI Climb Performance
Climb performance is reduced by the moderate sideslip. With wings level, VMC is significantly higher than published as there is no horizontal component of lift available to help the rudder combat asymmetrical thrust. Figure 13-15. Wings level engine ... flight. 2. Engine inoperative flight using ailerons alone requires an 8–10° bank angle toward the operative engine. [Figure 13-16] This assumes no rudder input, the ball is displaced well toward the operative engine, and climb performance is greatly…
- Chapter 6: Takeoffs and Departure Climbs › Short-Field Takeoff and Maximum Performance Climb
should reduce AOA to attain normal airspeed before attempting to fly out of the ground effect areas. Short-Field Takeoff and Maximum Performance Climb When performing takeoffs and climbs from fields where the takeoff area is short or the available ... takeoff area is restricted by obstructions, the pilot should operate the airplane at the maximum limit of its takeoff performance capabilities. To depart from such an area safely, the pilot needs to exercise positive and precise control of airplane attitude…
- Chapter 3: Basic Flight Maneuvers › Climbs and Climbing Turns › Establishing a Climb
Establishing a Climb A straight climb is entered by gently increasing back pressure on the elevator flight control to the pitch attitude referencing the airplane’s nose to the natural horizon while simultaneously increasing engine power to the climb power ... setting. The wingtips should be referenced in maintaining the climb attitude while cross-checking the flight instruments to verify performance. In many airplanes, as power is increased, an increase in slipstream over the horizontal stabilizer causes the airplane’s pitch…