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5. Performance
  • Eduard Velichkov

  • 問題数 23 • 9/18/2024

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    問題一覧

  • 1

    At ISA +15 maximum continuous engine power is ____ and fuel consumption is ____ .

    5% lower and 3% lower respectively

  • 2

    At ISA-15°, maximum continuous engine power is _____ and fuel consumption is _____

    5% higher and 3% higher respectively.

  • 3

    To keep engine wear to minimum, engine operating below ______ is not recommended

    1700 RPM

  • 4

    Vs at most FWD C.G, max mass

    43kt 0° bank; 46kt 30° bank; 51kt 45° bank; 60kt 60° bank

  • 5

    VS1 at most FWD C.G, max mass

    39kt 0° bank; 42kt 30° bank; 46kt 45° bank; 55kt 60° bank

  • 6

    VS0 at most FWD C.G, max mass

    38kt 0° bank; 41kt 30° bank; 45kt 45° bank; 54kt 60° bank

  • 7

    Fast cruise setting. (AFM recommended)

    2200 RPM; 0.7 inHg below maximum MP

  • 8

    Economical cruise. (AFM recommended)

    2100-1900 RPM; 1-2 inHg below max MP

  • 9

    TORR 0ft _______ and at 6000ft _______. Conditions 730kg (1609lb), ISA, Flaps in T/O, VLOF 57kts, Calm

    180m (600ft); 300m (1000ft)

  • 10

    TODR over 15m (50ft) obstacle at 0ft _______ and at 6000ft _______. Conditions 730kg (1609lb), ISA, Flaps in T/O, VLOF 57kts, Calm

    320m (1050ft); 500m (1650ft)

  • 11

    Maximum endurance at 6000ft, 55%, 75l, 58kg MOGAS

    4 h 30 min with FRF

  • 12

    Maximum endurance at 6000ft, 75%, 78l, 58kg MOGAS

    3 h 15 min with FRF

  • 13

    Maximum endurance at 2000ft, 95%, 75l, 58kg MOGAS

    2 h 45 min with FRF

  • 14

    ROC during balked landing at 0ft _______ and at 6000ft _______. Conditions: 58kt, Flaps LDG, 730kg (1609lb), ISA T, most FWD C.G, Max T/O power.

    440ft/min; 170ft/min

  • 15

    ROC with best rate of climb speed (Vy) at 0ft _______ and at 6000ft _______. Conditions: 65kt, Flaps T/O 730kg (1609lb), ISA T, most FWD C.G., Max T/O power. 650kg (BEM: 520 + PIC: 100 + Fuel 30) at 0ft _______ and at 6000ft _______.

    730kg - 810ft/min; 550ft/min; 650kg - 900ft/min; 630ft/min

  • 16

    LRR at 59kt, Flaps in LDG, 730kg (1609lb), Idle, max RPM, ISA.

    228m (748ft).

  • 17

    LDR over 15m (50ft) obstacle at 59kt, Flaps in LDG, 730kg (1609lb), Idle, max RPM, ISA.

    454m (1490ft).

  • 18

    In case of operation without wheel fairings the maximum cruise speed at specific altitude and power setting is reduced by approximately

    5%

  • 19

    TODR for different than paved RWY should:

    For take-off from dry, short-cut grass covered runways compared to paved runways, a 25% increase in take-off roll distance must be taken into account. On soft grass covered runways with grass deeper than 10 cm (4 in.), the take-off roll distance might be increased by as much as 40%.

  • 20

    In case of operation without wheel fairings the climb performance is reduced by approximately

    3%

  • 21

    For each 750m (2500ft) additional height above MSL add ______ to the LDR

    10%

  • 22

    Fuel consumption at: RPM, MP, Fuel flow at 55% power, ISA at 0ft _______ and 6000ft ______ is

    1900 RPM, 24.7 inHg, 13.6l/h (3.6gal/h); 2000 RPM, 22.0 inHg, 16.8l/h (4.4gal/h)

  • 23

    Fuel consumption at: RPM, MP, Fuel flow at 75% power, ISA at 0ft _______ and 6000ft ______ is

    2100 RPM, 27.0 inHg, 18l/h (4.8gal/h); 2260 RPM, 23.3 inHg, 23.2l/h (6.1 gal/h)