32.3 - Cs-23/applicable Operational Requirements Performance Class B - Use of Aeroplane Performance

OAT            ISA

Press. altitude        4000 ft

Headwind comp.    5 kt

Flaps            Zero

Runway length        2000 ft

Runway surface    Tarred

Runway radient    Zero

Runway condition    Dry

The maximum Take-off Mass (TOM) is:

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OAT                ISA +10° C

Press. Alt.            5000 ft

Mass                3400 lb

Headwind            5 kt

Flaps                Up

Runway surface        Tarred

Runway gradient        Zero

Runway condition        Dry

The [1] Rotation Speed is ___ and the [2] Take-Off Speed is ___.

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OAT            25°C

Press. Alt.        3000 ft

RWY            26L

Wind            310°/20 kt

Take-off Mass        4400 lb

Brakes             Heavy Duty

Associated Conditions: As in header of the graph.

The Accelerate-Stop Distance in ft is:

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OAT            20° C

Press. Alt.        2000 ft

RWY            24L

Wind            120°/ 8 kt

Take-Off Mass        4500 lb

Brakes            Heavy Duty

Associated conditions:    As in the header of graph.

The Accelerate-Stop Distance is:

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OAT            20° C

Press. Alt.        2000 ft

RWY            07R

Wind            120°/ 15 kt

Take-Off Mass        4500 lb

Brakes            Heavy Duty

Associated conditions:    As in header of the graph.

The Accelerate-Stop Distance is:

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With the information given below, determine the take-off distance over 50 ft:

Temperature: +9° C

Pressure altitude: 3000 ft

Headwind component: 5 kt

Take-Off Mass: 3250 lb

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With the information given below, determine the gross take-off distance over 50 ft:

Temperature: 24° C   

Pressure altitude: 5000 ft

Take-off mass: 3400 lb

Headwind component: 20 kt 

Runway surface: dry grass

Correction factor: 1.2 for runway surface/condition

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OAT            -15° C

Press. Alt.        4000 ft

RWY            12R

Wind             080°/12 kt

Take-Off Mass        4000 lb

Associated conditions     As in the header of the graph.

The Take-Off Distance is:

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OAT            24° C

Press. Alt.        3000 ft

RWY            30R

Wind            060°/4 kt

Take-Off Mass        3800 lb

Associated conditions    As in the header of the graph.

The Ground Roll Distance is:

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OAT                +18° C

Aerodrome Press. Altitude    1500 ft

Mass                1270 kg

Tailwind             4 kt

Runway surface        Hard

Runway condition        Dry

Runway slope            Zero

The Take-Off Distance to 50 ft height is:

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OAT            30°C

Press. Alt.        1000 ft

Aeroplane Mass    2950 lb

Tailwind        5 kt

Flaps            Approach setting

Runway        Short wet grass, firm subsoil

Correction Factor    1.3 (for runway conditions)

The Take-Off Distance, rounded to the nearest 50 ft, is:

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OAT                38°C

Press. Alt.            4000 ft

Aeroplane Mass        3400 lb

Tailwind            5 kt

Flaps                Approach setting

Runway surface        Grass

Runway condition        Dry

Runway slope            Zero

Correction factor        1.2 for runway condition

The Take-off Distance, rounded to the nearest 50 ft, is:

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Corrections:

+/- 20 m / 1 000 ft field elevation

- 5 m / kt headwind

+ 10 m / kt tail wind

+/- 15 m / % runway slope

 +/- 5 m / °C deviation from standard temp.

Calculate take-off distance at 1000 ft elevation, 17°C, QNH 1013.25 hPa, 1% up-slope, and 10 kt tailwind.

With the information given below, determine the engine-out Rate Of Climb (ROC):

OAT: 15° C

Pressure Altitude: 3000 ft

Mass: 4400 lb

Headwind: 35 kt

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Determine the the minimum TODA for a multi-engine piston aeroplane in commercial operation, given the information below:

Take-Off Distance Required (from AFM, defactored): 2800 ft

Runway slope: 1.5 % UP

Runway conditions: paved, wet

(no stopway / clearway available)

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Determine the the maximum take-off distance required (unfactored, from AFM) for a multi-engine piston aeroplane in commercial operation, given the information below:

Take-Off Distance Available (no stop/clearway): 3500 ft

Runway slope: 1.0 % UP

Runway conditions: Grass (firm soil 10cm long), wet

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OAT        0° C

Press. Alt.    18000 ft

Gross mass    3750 lb

Mixture    25° F rich of Peak EGT

Determine the Two-Engine Rate of Climb in ft/min:

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OAT        -20° C

Press. Alt.    14000 ft

Gross mass    4000 lb

Determine the One-Engine Inoperate Rate of Climb in ft/min:

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OAT        -20° C

Press. Alt.    18000 ft

Gross mass    4000 lb

Mixture    Leaned to 25° F rich of peak EGT

Determine the Two-Engine Rate of Climb in ft/min:

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OAT        10°C

Press. Alt,    2000 ft

Gross Mass    3750 lb

Determine the One-engine Inoperative Rate of Climb in ft/min:

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