32.2 - Cs-23/applicable Operational Requirements Performance Class B - Theory_在线真题试卷与模拟练习_32.2 - Cs-23/applicable Operational Requirements Performance Class B

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The abbreviation for the Stalling Speed or the minimum steady flight speed at which the aeroplane is controllable in landing configuration is...

(See attachment IC-032-016 or CAP 698 Figure 2.1)

Using the attached graph for single-engine class B aeroplane, estimate the maximum value for the stall speed at a mass of 3200 lbs:

（含图）

In case of an engine failure during straight and level flight with a twin-engine class B aeroplane, which of the following statements is correct?

1. Thrust required decreases.

2. Excess thrust reduces by more than 50%.

The maximum obstacle clearance in a climb is achieved at...

With the critical engine inoperative...

With regard to Regulation (EU) No 965/2012 Part CAT (performance class B aeroplanes), the unfactored take-off distance, specified in the AFM, shall not exceed:

- when multiplied by a factor of (1) ___ the take-off run available (TORA)

- or, when stop way and/or clearway is available, when multiplied by a factor of (2) ___, the take-off distance available (TODA).

With flaps at 35° instead of 25°, the aircraft will have a/an [1] ___ landing distance and a/an [2] ___ go-around performance.

Approved take-off flap settings: UP 5° / 10° / 15°.

When performing a take-off with flaps UP instead of 10°, the...

When choosing a higher flap setting for landing, the effect will be a(n) (1) ___ in approach speed and a (2) ___ in ground roll distance.

Taking off and landing a short dry grass instead of a paved runway, the take-off distance [1] ___ and the landing distance [2] ___.

According AMC1 CAT.POL.A.330, unless otherwise specified in the AFM, or other performance or operating manuals from the manufacturers, the variable affecting the landing performance and the associated factor that should be applied to the AFM data on a dry short-grass runway is:

According AMC1 CAT.POL.A.330, unless otherwise specified in the AFM, or other performance or operating manuals from the manufacturer, the landing distances required should be increased by (1) ___ for each (2) ___ of downslope.

According AMC1 CAT.POL.A.330, unless otherwise specified in the AFM, or other performance or operating manuals from the manufacturer, the landing distance required for a 1.5% downslope should be increased by:

(See attachment IC-032-018 or CAP 698 Figure 4.1)

Given the maximum allowed wind components below for an aeroplane, already accounting for all wind safety factors, available runways 04 and 22 and wind from 090, what is the maximum allowed wind speed and preferred runway?

Crosswind: 20 kt

Headwind: 30 kt

Tailwind: 10 kt

（含图）

(For this question, use attachment IC-032-018 or a suitable calculation method)

Given the maximum allowed crosswind component of 25 kt for take-off on runway direction 220(M) and wind from 270(M), what is the maximum allowed reported wind speed to NOT exceed maximum crosswind component?

（含图）

When calculating the take-off field length required, not more than [1] ___ head wind are taken into account and not less than [2] ___ tailwind.

If a graph is used to show compliance with the obstacle clearance requirement, the gradient from 50 ft to the assumed engine failure height is to be the average all-engine gradient multiplied by a factor of:

With regard to Class A Medium Range Jet Transport aircraft, any part of the net take-off flight path in which the aeroplane is banked by more than 15° shall clear all obstacles within the horizontal distances specified by a vertical distance of at least:

With regard to obstacle accountability area of performance class B multi-engine piston aeroplanes, the dimensions of the obstacle accountability area start with a semi-width at the end of TODA of 90 m. If the wing span is less than 60 m, then at least (1) ___ is the semi-width to be used. The area expands at a rate of (2) ___ x horizontal distance D travelled from the end of TODA.

The take-off distance will increase with (1) ___ pressure altitude and with (2) ___ temperature.

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