IL.X.B.R2
Risk managementPowerplant failure during conversion.
From the FAA library
- Chapter 11: Aircraft Performance › Performance › Straight-and-Level Flight
remain in steady, level flight, equilibrium must be obtained by a lift equal to the aircraft weight and a powerplant thrust equal to the aircraft drag. Thus, the aircraft drag defines the thrust required to maintain steady, level flight ... becomes four times as great, but the power required to overcome that drag is eight times the original value. Conversely, when the aircraft is operated in steady, level flight at twice as great a speed, the induced drag…
- Chapter 3: Identifying Hazards & Associated Risks › Leading Accident Causes
general aviation fatal accidents include loss of control in-flight (LOC-I), controlled flight into terrain (CFIT), system component failure of the powerplant (SCF-PP), and fuel-related issues. These causes often signify the final result of a chain ... Examples of loss of control scenarios include continued VFR into IMC, wake turbulence upsets, thunderstorm encounters, instrument failure, improper aircraft loading, loss of outside references during flight at night or over water, and conditions that exceed the pilot’s capability…
- Chapter 16: Navigation › Distance D = GS X T › Converting Knots to Miles Per Hour
Converting Knots to Miles Per Hour Another conversion is that of changing knots to miles per hour (mph). The aviation industry is using knots more frequently than mph, but is important to understand the conversion for those that ... hour (NMPH). Because there are 6,076.1 feet in 1 NM and 5,280 feet in 1 SM, the conversion factor is 1.15. To convert knots to mph, multiply speed in knots by 1.15. For example: a wind speed…
- Chapter 7: Automation & Flight Path Management › Failure to Anticipate, Act, & Verify
Failure to Anticipate, Act, & Verify Automation offers increased safety with enhanced situational awareness. However, these systems make it possible for a pilot to become complacent, unprepared, or lose situational awareness. If this occurs and an unexpected change in flight plan ... crew was unexpectedly cleared for an approach, lost situational awareness, and crashed into mountainous terrain. The accident summary cites failure of the flight crew to revert to basic radio navigation at the time when the FMS-assisted navigation became confusing…
- Chapter 9: Flight Manuals and Other Documents › General (Section 1)
General (Section 1) The General section provides the basic descriptive information on the airframe and powerplant(s). Some manuals include a three-dimensional drawing of the aircraft that provides dimensions of various components. Included are such items as wingspan, maximum ... symbology, and some of the terminology used in the POH. At the discretion of the manufacturer, metric and other conversion tables may also be included. Limitations (Section 2) The Limitations section contains only those limitations required by regulation or that…
- 14 CFR § 91.185 IFR operations: Two-way radio communications failure.
operations: Two-way radio communications failure. (a) General. Unless otherwise authorized by ATC, each pilot who has two-way radio communications failure when operating under IFR shall comply with the rules of this section. (b) VFR conditions. If the failure ... occurs in VFR conditions, or if VFR conditions are encountered after the failure, each pilot shall continue the flight under VFR and land as soon as practicable. (c) IFR conditions. If the failure occurs in IFR conditions, or if paragraph…