IL.XIV.B.R3
Risk managementDeceleration in a space-limited environment.
From the FAA library
- Chapter 10: Weight and Balance › Balance, Stability, and Center of Gravity › Stability
same manner as those mentioned for an excess weight condition. It is vital to comply with weight and balance limits established for all aircraft. Operating above the maximum weight limitation compromises the structural integrity of the aircraft and can adversely ... undesirable characteristic. This makes it easy for the pilot to inadvertently overstress an aircraft. Stability and Center of Gravity Limits for the location of the CG are established by the manufacturer. These are the fore and aft limits beyond which…
- Chapter 9: Flight Manuals and Other Documents › Weight and Loading Distribution
weight and balance section of the AFM/POH. Figure 9-4. Manifold pressure gauge (top) and tachometer (bottom). Flight Limits Flight Limits list authorized maneuvers with appropriate entry speeds, flight load factor limits, and types of operation limits. It also indicates ... those maneuvers that are prohibited, such as spins or acrobatic flight, as well as operational limitations such as flight into known icing conditions. Placards Most aircraft display one or more placards that contain information having a direct bearing…
- Chapter 5: Aerodynamics of Flight › High Speed Flight › Speed Ranges
VMO/MMO is defined as the maximum operating limit speed. VMO is expressed in knots calibrated airspeed (KCAS), while MMO is expressed in Mach number. The VMO limit is usually associated with operations at lower altitudes and deals with structural loads ... flutter. The MMO limit is associated with operations at higher altitudes and is usually more concerned with compressibility effects and flutter. At lower altitudes, structural loads and flutter are of concern; at higher altitudes, compressibility effects and flutter…
- Chapter 5: Aerodynamics of Flight › Load Factors › Vg Diagram
less than this does not provide negative lift capability sufficient to damage the aircraft from excessive flight loads. The limit airspeed (or redline speed) is a design reference point for the aircraft—this aircraft is limited ... flight is attempted beyond the limit airspeed, structural damage or structural failure may result from a variety of phenomena. The aircraft in flight is limited to a regime of airspeeds and Gs that do not exceed the limit (or redline…
- Chapter 10: Teaching Practical Risk Management during Flight Instruction › Notes on Instructional Risk Management in the Flight Deck › Managing Risk while Teaching Takeoffs
beyond the learner’s control and should pay close attention to pitch attitude and airspeed throughout the maneuver. Insufficient spacing from preceding aircraft during takeoffs also creates various hazards. Some hazards include wake turbulence, insufficient in-trail spacing, and insufficient ... separation from an aircraft approaching to land. The instructor ensures that there is sufficient spacing from landing and departing aircraft prior to entering any space being used for departures and arrivals. This will also help teach the learner sound decision…
- Chapter 3: Identifying Hazards & Associated Risks › Hazard Identification and Risk Analysis › Environment
overrun or stall after takeoff. Her personal minimums include a 20 percent additional margin over calculated runway takeoff distance. Environment • The weather system moving in from northwest Colorado is the main environmental hazard affecting the flight to Santa Rosa ... hazard on the route to Santa Rosa. This requires relatively high cruising altitudes which may approach the performance limits of her airplane. • The departure airport has no ATC services, although fuel is available. ATC may limit the altitude selection…