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Where are the procedures associated with take-off and landing on contaminated runways found?
Refer to figure.NOTE: For this question do NOT interpolate, Choose the most conservative figures at ALL times.The annex shows a regulated take-off mass (RTOM) table for runway 23L from take-off position VB. In each RTOM chartbox, the following information is provided for a given wind component / outside air temperature combination: MTOM /limitation code / V,/VR/V2 (+100 kt). Given the following information, determine the RTOM for departure.W/V: 140°/14 ktOAT: +10°CQNH: 1008 hPaRunway: WETEngine anti-ice: ONPacks: OFFQuick line-up
What is the result of an increase in air density?
The crew of a Medium-Range Jet Transport aeroplane are planning for a Commercial Air Transport flight departing from Mykonos (LGMK) Runway 16, which is 1902 m long with a take-off path over the sea. The aeroplane has three take-off flap settings, which give the following maximum take-off masses:
T/0 1: 1 stage of slats and 1 stage of flaps - 78.1 tonnes.
T/0 2: 2 stages of slats and 2 stages of flaps - 81.1 tonnes.
T/0 3: 2 stages of slats and 3 stages of flaps - 82.9 tonnes.
These maximum take-off masses are limited by the...
Refer to figure.You are taking-off with a single-engined aeroplane, and a field-lenght-limited take-off mass, fromrunway 18, in Vmc, for a straight-out departure. Given the following information, what will be theexpected obstacle clearance over the trees on the extended centre line?Climb gradient: 9%TAS: 124 ktWind component: 10 kt headwind1 NM = 6080 ftHeight Difference = ((GD × TAS)/GS) × Gradient/100
Refer to figure or CAP 698 file 4.20.Given the following information for a medium range jet transport aeroplane, determine the regulated take-off mass forthe new runway:OAT: +15°CAirfield pressure altitude: 0 ftNil WindFlap setting: 5°TORA: 7000 ftThe normal Take-off mass limits relevant for this flight are:Maximum Structural Limit: 62 800 kgField Length Limit: 60 500 kgClimb Limit: 64 000 kgTyre Speed Limit: greater than 84 000 kgDue to wind direction change, ATC changes the runway in use, which will have the same conditions described previously,except for the following:Wind: 10 kt headwindObstacle height: 360 ftObstacle distance from the break release point: 21 000 ft
Refer to figure or CAP698 file 3.1.TORA: 2250 ftRunway surface: grassRunway condition: dryNo clearway and no stopway availableAirfield pressure altitude: 2000 ftAirfield temperature: +11°CHeadwind component: 5 ktGiven the following information, what is the Field Length Limited Take-Off Mass?
Which of the following options correctly describes the effects on aircraft performance of landing on wet or contaminated runways?
The following runways are available: 07/25 and 01/19. The wind is coming from 350°25 degrees. Which runway should the pilot choose?
Refer to figure. (For this question use CAP 698 Figure 4.7).Planned take-off mass is 64000 kg, pressure altitude 4000 ft, OAT +10°C, V, 151, 155, 161. Runway slope is -1% andtailwind 5 kt. What is the maximum permitted take-off mass?