Performance 1

Refer to CAP698 Section 2 - SEP1 Page 10 Figure 2.4 Landing.

With regard to the graph for landing performance, what is the minimum headwind component required in order to land at Helgoland airport?

Given:

Runway length: 1300'

Runway elevation: MSL

Weather: assume ISA conditions

Mass: 3200 lbs

Obstacle height: 50'

• 5 KT

• No wind

• 15 KT

• 10 KT

Refer to CAP698 Section 2 - SEP1 Page 10 Figure 2.4

With regard to the landing chart for the single engine aeroplane determine the landing distance from a height of 50'

OAT: ISA +15°C

Pressure Altitude: 0'

Aeroplane Mass: 2940 lbs

Headwind component: 10 KT

Flaps: Landing position (down)

Runway: short and wet grass - firm soil

Correction factor (wet grass): 1.38

• A) approximately: 2000'

• B) approximately: 1300'

• C) approximately: 1450'

• D) approximately: 1794'

Use Performance Manual MEP1 Figure 3.2; With regard to the graph for the light twin aeroplane, if the brakes are released before take-off power is achieved, the accelerate/stop distance will be:

• shorter than the graphical distance.

• the same as the graphical distance because both techniques are accounted.

• longer than the graphical distance.

• unaffected because all take-off techniques are accounted.

At reference or use or Performance Manual MEP 1 Figure 3.2 PAGE 5

Given:

OAT: 25°C

Pressure Altitude: 3000 ft

RWY: 24L

Wind: 310°/20kts

Take off Mass: 4400 lbs

Heavy Duty Brakes installed.

Other conditions as associated in the header of the graph.

What is the Accelerate and Stop Distance under the conditions given?

• 3350 ft

• 3750 ft

• 4000 ft

• 4300 ft

Refer to CAP698 Section 3 - MEP1 Figure 3.1 Take-off Normal Procedure

Given:

OAT +24°C

Pressure Altitude: 3000'

RWY 30R

Wind·060°/4 KT

Take-off Mass: 3800 lbs

Other conditions as associated in the header of the graph. What is the Take-off Distance under the conditions given?

• 2000'

• 1670'

• 1550'

• 2150

Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure

Given:

OAT 24 °C

Pressure Altitude 3000'

RWY, 12L

Wind· 080/12 KT

Take-off Mass: 3800 lbs

Runway Surface· Wet Grass - firm soil

Runway Slope: 2% downslope

What is the minimum runway length?

No stopway or clearway are available.

• 1400 ft

• 2850 ft

• 1750 ft

• 2550 ft

Refer to CAP698 Section 3 - MEP1 Figure 3.7 Climb Performance - Gear Retracted Maximum Continuous Power

Given:

OAT, - 20 °C

Pressure Altitude: 14 000 ft

Gross Mass 4.000 lbs Other conditions as associated in the header of the graph. What is the one engine inoperative rate of climb?

• 1250 ft/min

• 625 ft/min

• 175 ft/min

• 375 ft/min

OAT, 10 °C

Pressure Altitude: 2000 ft

Gross Mass 3750 lbs

Mixture: full rich

Other conditions as associated in the header of the graph. What is the two engine rate of climb for the conditions given?

• 430 ft/min

• 1770 ft/min

• 1570 ft/min

• 1970 ft/min

Refer to CAP698 Section 3 - MEP1 Figure 3.9 Landing Distance Normal Procedure

Given:

Flaps 40

Aerodrome pressure altitude: Sea level

Ambient temperature +15 °C

Landing weight 4000 lbs

Wind· calm

Runway paved and dry

What is the Landing Distance?

• 2040'

• 1240'

• 1400'

• 2400

The speed VSR is defined as:

• safe rotation speed for take-off

• design stress speed

• as reference stall speed and may not be less than 1-g stall speed

• speed for best specific range