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IL.XIV.H.K2f

Knowledge

System and equipment malfunctions specific to the aircraft, including:

Inoperative trim

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From the FAA library

  • Chapter 3: Identifying Hazards & Associated Risks › Aircraft Hazards › Equipage

    weight reduces climb performance. • Weight and Balance–Pilots who do not check center of gravity limits may experience difficulty trimming or controlling the aircraft, which could lead to a loss of control in-flight. Equipage The avionics and other equipment ... pilot workload. A pilot flying an aircraft in these conditions might consider aircraft without an autopilot an “A” hazard. • Inoperative Equipment–Inoperative equipment triggers an “A” hazard. For example, an inoperative landing light may make night operation more hazardous, even…

  • Chapter 6: Flight Controls › Flight Control Systems › Trim Tabs

    Common types of trim systems include trim tabs, balance tabs, antiservo tabs, ground adjustable tabs, and an adjustable stabilizer. Figure 6-19. Spoilers reduce lift and increase drag during descent and landing. Trim Tabs The most common installation on small ... aircraft is a single trim tab attached to the trailing edge of the elevator. Most trim tabs are manually operated by a small, vertically mounted control wheel. However, a trim crank may be found in some aircraft. The flight deck…

  • Chapter 9: Flight Manuals and Other Documents › Minimum Equipment Lists (MEL) and Operations With Inoperative Equipment

    flight. Using the deferral provision of 14 CFR, part 91, section 91.213(d), the pilot determines whether the inoperative equipment is required by type design, 14 CFR, or ADs. If the inoperative item is not required, and the aircraft ... safely operated without it, the deferral may be made. The inoperative item shall be deactivated or removed and an INOPERATIVE placard placed near the appropriate switch, control, or indicator. If deactivation or removal involves maintenance (removal always will), it must…

  • 14 CFR § 91.611 Authorization for ferry flight with one engine inoperative.

    takeoff path with two critical engines inoperative; and (ii) The climb speed not less than the two-engine inoperative trim speed for the actual steady gradient of the final takeoff climb prescribed by paragraph (c)(4)(i) of this section…

  • Chapter 8: Ground Procedures and Flight Preparations › Preflight › Minimum Equipment Lists (MELs) and Operations with Inoperative Equipment

    switch as INOPERATIVE. There are exceptions to the use of the MEL for deferral. For example, should a component fail that is not listed in the MEL as deferrable (the rotor tachometer, engine tachometer, or cyclic trim, for example), then ... Deferral of maintenance is not to be taken lightly, and due consideration should be given to the effect an inoperative component may have on the operation of a helicopter, particularly if other items are inoperative. Further information regarding MELs…