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Test

TD 16

Dan Hurley 7 preguntas

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Preguntas del test (7)

  1. 1SAS -Off Flight CAUTION: The 3-Axis backup SAS must not be used as [blank_start]primary[blank_end] flight aid, except after [blank_start]complete[blank_end] AP failure, in order to [blank_start]finish[blank_end] the flight.
    1. Aprimary
    2. Bcomplete
    3. Cfinish
  2. 2Constant angle or vertical takeoff can range from vertical to almost flat. It may demand that more power is available than the power required to [blank_start]hover[blank_end]. The angle is initiated from the point of hover (or ground) to a point in space clear of the [blank_start]obstacles[blank_end]. Vertical takeoffs are [blank_start]altitude[blank_end] over [blank_start]airspeed[blank_end] takeoffs and will require [blank_start]OGE[blank_end] power.
    1. Ahover
    2. Baltitude
    3. Cairspeed
    4. Dobstacles
    5. EOGE
  3. 3Level acceleration is used when the power required to hover is the [blank_start]maximum[blank_end] power available. The first objective is to achieve [blank_start]ETL[blank_end] without allowing the aircraft to settle to the surface. As the aircraft enters ETL, make a significant forward cyclic input to prevent [blank_start]blowback[blank_end]. Once through ETL, the aircraft will begin to climb at the [blank_start]current[blank_end] power setting.
    1. Amaximum
    2. BETL
    3. Cblowback
    4. Dcurrent
  4. 4Rotor RPM Limitations
    Condition Power On Power Off
    Min Transient (max 20s) [blank_start]85[blank_end]% -
    Min Continuous GM <= 2000kg [blank_start]96[blank_end]% [blank_start]80[blank_end]%
    Min Continuous GM >= 2000kg [blank_start]96[blank_end]% [blank_start]85[blank_end]%
    Max Continuous [blank_start]104[blank_end]% [blank_start]104[blank_end]%
    Partial Power (max 5 min) Torque <= 2x30% [blank_start]106[blank_end]% -
    Max Transient [blank_start]106[blank_end]% [blank_start]110[blank_end]%
    1. A85
    2. B96
    3. C80
    4. D96
    5. E85
    6. F104
    7. G104
    8. H106
    9. I106
    10. J110
  5. 5Autorotation
    Procedure
    1. Collective lever – [blank_start]Reduce to maintain NRO within limits[blank_end]
    2. Airspeed – [blank_start]75[blank_end] KIAS recommended
    NOTE Maximum range airspeed [blank_start]90[blank_end] KIAS
    Minimum rate-of-descent airspeed [blank_start]60[blank_end] KIAS
    3. Double engine emergency shutdown – [blank_start]Perform[blank_end]
    AT APPROXIMATELY [blank_start]100[blank_end] FT AGL:
    4. Flare attitude – Establish (approx. [blank_start]15[blank_end]* to [blank_start]20[blank_end]*) to reduce forward speed and rate of descent; control NRO
    AT APPROXIMATELY [blank_start]8[blank_end] – [blank_start]12[blank_end] FT AGL:
    5. Flare attitude – Reduce to approx [blank_start]7[blank_end]*
    6. Heading – Maintain
    7. Collective lever – [blank_start]Raise to stop descent[blank_end] and [blank_start]cushion landing[blank_end]
    8. BAT MSTR sw – [blank_start]OFF[blank_end]

    NOTE The appropriate values must be adjusted according to prevailing conditions of gross mass, wind and terrain.
    1. AReduce to maintain NRO within limits
    2. B75
    3. C90
    4. D60
    5. EPerform
    6. F100
    7. G15
    8. H20
    9. I8
    10. J12
    11. K7
    12. LRaise to stop descent
    13. Mcushion landing
    14. NOFF
  6. 6Prohibited flight maneuvers
    The following are prohibited:
    – [blank_start]aerobatic maneuvers[blank_end]
    – [blank_start]intentional full autorotation landings[blank_end]
    – [blank_start]flight into icing conditions[blank_end]
    1. Aaerobatic maneuvers
    2. Bintentional full autorotation landings
    3. Cflight into icing conditions
  7. 7Warning Light Indications - Rotor RPM
    Conditions/Indications
    NRO low
    – NRO [blank_start]95[blank_end]% or less - [blank_start]steady light[blank_end]
    – Audio signal - [blank_start]low-pitch beeping tone[blank_end]
    NRO high
    – NRO [blank_start]106[blank_end]% or above - [blank_start]flashing light[blank_end] and [blank_start]warning gong[blank_end]
    – Audio signal at [blank_start]110[blank_end]% or above - [blank_start]flashing light[blank_end] and [blank_start]steady high-pitch tone[blank_end]

    Procedure
    NRO low/NRO high
    1. Rotor RPM indicator – Check
    2. Collective lever – [blank_start]Adjust as necessary[blank_end] to [blank_start]maintain NRO within normal range[blank_end]
    1. A95
    2. Bsteady light
    3. Clow-pitch beeping tone
    4. D106
    5. E110
    6. Fflashing light
    7. Gsteady high-pitch tone
    8. Hflashing light
    9. Iwarning gong
    10. JAdjust as necessary
    11. Kmaintain NRO within normal range

Información

Descripción
Flight Training Daily Questions Test sobre TD 16, creado por Dan Hurley el 17/01/2021.
Idioma
English
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