IH.VII.B.R1
Risk managementPotential engine failure during approach and landing.
From the FAA library
- Chapter 2: Aeronautical Decision-Making › TEAM Checklist: Choose and Implement Risk Controls › The DECIDE Model
First, adjust the power to the maximum controllable level on both engines. Because the left engine is the only engine delivering thrust, the yaw increases to the right, which necessitates application of additional left rudder application. Figure ... worldwide. Its application is illustrated in column A while automatic/naturalistic decision-making is shown in column B. The failed engine is the side that requires no rudder pressure, in this case the right engine. Second, having identified the failed right…
- Chapter 10: IFR Flight › Approach to an Airport With an Operating Tower, With an Approach Control › Approaches to Parallel Runways
Approaches to Parallel Runways Procedures permit ILS instrument approach operations to dual or triple parallel runway configurations. A parallel approach is an ATC procedure that permits parallel ILS approach to airports with parallel runways separated by at least ... feet between centerlines. Wherever parallel approaches are in progress, pilots are informed that approaches to both runways are in use. Simultaneous approaches are permitted to runways: 1. With centerlines separated by 4,300 to 9,000 feet; 2. Equipped with…
- Chapter 10: IFR Flight › Approaches › Approach to Airport With an Operating Tower, With No Approach Control
instrument approach and advises “change to advisory frequency approved.” When the aircraft arrives on a “cruise” clearance, ATC does not issue further clearance for approach and landing. If an approach clearance is required, ATC authorizes the pilots to execute ... choice of standard instrument approach (if more than one is published for the airport) with the phrase “Cleared for the approach” and the communications frequency change required, if any. From this point on, there is no contact with…
- 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…
- 14 CFR § 91.1705 Required pilot training.
Required pilot training. (xviii) No flap or 5- degrees flaps landing; (xix) One engine inoperative landing with 5- and 20- degrees flaps; (xx) Crosswind landing; (xxi) Instrument landing system (ILS) and missed approach ; (xxii) Two engine missed approach; (xxiii ... engine inoperative ILS and missed approach; (xxiv) One engine inoperative missed approach; (xxv) Non-precision and missed approach; (xxvi) Non-precision continuous descent final approach and missed approach; (xxvii) One engine inoperative non-precision and missed approach; (xxviii) One engine…
- Chapter 10: IFR Flight › Approaches › Instrument Approaches to Civil Airports
Instrument Approaches to Civil Airports Unless otherwise authorized, when an instrument letdown to an airport is necessary, the pilot should use a standard IAP prescribed for that airport. IAPs are depicted on IAP charts and are found ... approach procedures depend upon the facilities available at the terminal area, the type of instrument approach executed, and the existing weather conditions. The ATC facilities, NAVAIDs, and associated frequencies appropriate to each standard instrument approach are given on the approach…