AA.VII.E.K1
KnowledgeFlight characteristics and controllability associated with maneuvering to a landing with inoperative powerplant(s).
From the FAA library
- Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Landing Performance
item that alters the landing speed or deceleration rate during the landing roll affects the landing distance. The effect of gross weight on landing distance is one of the principal items determining the landing distance. One effect of an increased ... gross weight is that a greater speed is required to support the aircraft at the landing AOA and lift coefficient. For an example of the effect of a change in gross weight, a 21 percent increase in landing weight requires…
- Chapter 18: Emergency Procedures › Flight Control Malfunction/Failure › Landing Gear Malfunction
pilot can request that the runway surface be foamed. The pilot should consider burning off excess fuel. This reduces landing speed and fire potential. If the landing gear malfunction is limited to one main landing gear leg, the pilot should ... that side. The reduced weight makes it possible to delay the unsupported wing from contacting the surface during the landing roll until the last possible moment. Reduced impact speeds result in less damage. If only one landing gear leg fails…
- Chapter 9: Approaches and Landings › Crosswind Approach and Landing
Common Errors Common errors with forward slips to a landing: 1. Incorrect pitch adjustments that result in poor airspeed control. 2. Reacting to erroneous airspeed indications. 3. Using excess power while trying to lose altitude. 4. A slip ... same direction as any crosswind. 5. Poor glidepath control. 6. Late transition to a sideslip during landing with crosswinds. 7. Landing without the longitudinal axis parallel to runway. 8. Landing off the centerline. Crosswind Approach and Landing Most runways…
- Chapter 9: Approaches and Landings › Emergency Approaches and Landings (Simulated)
Emergency Approaches and Landings (Simulated) During dual training flights, the instructor should give simulated emergency landings by retarding the throttle and calling “simulated emergency landing.” The objective of these simulated emergency landings is to develop a pilot’s accuracy, judgment ... planning, procedures, and confidence when little or no power is available. A simulated emergency landing may be given with the airplane in any configuration. If the simulated power failure occurs while above best glide speed, the pilot allows the airplane…
- Chapter 9: Approaches and Landings › Go-Arounds (Rejected Landings)
Arounds (Rejected Landings) A go-around is a normal maneuver that is used when approach and landing parameters deviate from expectations or when it is hazardous to continue. Situations such as air traffic control (ATC) requirements, unexpected appearance of hazards ... overtaking another airplane, wind shear, wake turbulence, mechanical failure, or an unstable approach are all reasons to discontinue a landing approach. Like any other normal maneuver, the go-around should be practiced and perfected. The flight instructor should emphasize early…
- Chapter 16: Transition to Jet-Powered Airplanes › Jet Engine Landing › Landing Speeds
Landing Speeds As in the takeoff planning, there are certain speeds that should be taken into consideration when landing a jet airplane. The speeds are as follows: ⦁ VSO —stall speed in the landing configuration. ⦁ VREF —1.3 times the stall speed ... landing configuration. ⦁ Approach climb—the speed that guarantees adequate performance in a go-around situation with an inoperative engine. ⦁ Landing climb—the speed that guarantees adequate performance in arresting the descent and making a go-around from the final stages…