Mdl Question Attempts

Mdl Question Attempts :: List

Mdl Question Attempts

Found 186 records
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		Id	Questionusageid	Slot	Behaviour	Questionid	Variant	Maxmark	Minfraction	Maxfraction	Flagged	Questionsummary	Rightanswer	Responsesummary	Timemodified
		74	4	1	immediatefeedback	52	1	1.0000000	0.0000000	1.0000000	0	When the pilot defects the elevators in flight the...	pitching about its lateral axis		1693281937

		75	4	2	immediatefeedback	293	1	2.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE...	1090kg		1693281937

		76	4	3	immediatefeedback	297	1	2.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE...	690m		1693281937

		77	4	4	immediatefeedback	301	1	2.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE...	790m		1693281937

		78	4	5	immediatefeedback	305	1	2.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE...	No		1693281937

		79	4	6	immediatefeedback	819	1	2.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE...	109		1693281937

		80	4	7	immediatefeedback	823	1	2.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE...	690		1693281937

		81	4	8	immediatefeedback	827	1	2.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE...	790		1693281937

		82	4	9	immediatefeedback	307	1	3.0000000	0.0000000	1.0000000	0		190 lbs		1693281937

		83	4	10	immediatefeedback	311	1	3.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK (Page 1 to 12) ...	30lbs		1693281937

		84	4	11	immediatefeedback	834	1	3.0000000	0.0000000	1.0000000	0		190		1693281937

		85	4	12	immediatefeedback	838	1	3.0000000	0.0000000	1.0000000	0	Refer to RPL-PPL-CPL WORKBOOK (Page 1 to 12) ...	30		1693281937

		86	4	13	immediatefeedback	56	1	1.0000000	0.0000000	1.0000000	0	When a left twisting movement is applied to the co...	the left aileron rises and the aircraft rolls to t...		1693281937

		87	4	14	immediatefeedback	60	1	1.0000000	0.0000000	1.0000000	0	Which is the most appropriate recovery action if a...	apply opposite aileron to level the wings		1693281937

		88	4	15	immediatefeedback	64	1	1.0000000	0.0000000	1.0000000	0	The form of drag that predominates at low airspeed...	induced drag		1693281937

		89	4	16	immediatefeedback	68	1	1.0000000	0.0000000	1.0000000	0	Total drag is the combined effect of parasite drag...	near the middle of the speed range, when both indu...		1693281937

		90	4	17	immediatefeedback	72	1	1.0000000	0.0000000	1.0000000	0	The direction of the relative airfow is always: op...	opposite to the direction of the aircraft’s moti...		1693281937

		91	4	18	immediatefeedback	76	1	1.0000000	0.0000000	1.0000000	0	The magnitude of the total aerodynamic reaction on...	both the angle of attack of the aerofoil and the s...		1693281937

		92	4	19	immediatefeedback	80	1	1.0000000	0.0000000	1.0000000	0	For any given airspeed, the stalling angle of atta...	lift reaches its maximum value		1693281937

		93	4	20	immediatefeedback	84	1	1.0000000	0.0000000	1.0000000	0	If an aircraft is taxiing on level ground with a s...	yaw to the left		1693281937

		94	4	21	immediatefeedback	88	1	1.0000000	0.0000000	1.0000000	0	The application of full flap during a power-off gl...	the approach path to be steeper with no increase i...		1693281937

		95	4	22	immediatefeedback	92	1	1.0000000	0.0000000	1.0000000	0	Which of these figures correctly shows the relatio...	[a]		1693281937

		96	4	23	immediatefeedback	96	1	1.0000000	0.0000000	1.0000000	0	The purpose of aerodynamic balancing of rudders or...	lighten the control force required to operate the ...		1693281937

		97	4	24	immediatefeedback	100	1	1.0000000	0.0000000	1.0000000	0	If a pilot applies flap during a power-off glide, ...	more drag and a decrease in gliding distance		1693281937

		98	4	25	immediatefeedback	104	1	1.0000000	0.0000000	1.0000000	0	Given that the recommended indicated air speed for...	climbing at a reduced indicated air speed		1693281937

		99	4	26	immediatefeedback	108	1	1.0000000	0.0000000	1.0000000	0	The best angle of climb speed is called Vx and the...	a lower nose attitude and a higher indicated air s...		1693281937

		100	4	27	immediatefeedback	112	1	1.0000000	0.0000000	1.0000000	0	Which of the following most fully describes the be...	any increase or decrease in angle of attack result...		1693281937

		101	4	28	immediatefeedback	116	1	1.0000000	0.0000000	1.0000000	0	If the pilot observes that the aircraft is slippin...	apply more rudder in the direction of the turn		1693281937

		102	4	29	immediatefeedback	120	1	1.0000000	0.0000000	1.0000000	0	A heavy jet aircraft has just departed from a runw...	aim to lift off before the jet’s lift off point,...		1693281937

		103	4	30	immediatefeedback	124	1	1.0000000	0.0000000	1.0000000	0	What effect will an increase in bank angle during ...	load factor will increase and stalling speed will ...		1693281937

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immediatefeedback

When the pilot defects the elevators in flight the aeroplane responds by -: pitching about its longitudinal axis; pitching about its lateral axis; pitching about its normal axis; yawing about its normal axis

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE 5<br /> <br /> Consider the following conditions:<br /> <br /> > Pressure Altitude: 1000 ft<br /> > Shade Temp: 10oC<br /> > TODA: 750m<br /> > Surface: Short dry grass<br /> > Slope: Level<br /> > Wind: 5kt headwind<br /> Using the Type 1 take-off charts, the grea

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE 5<br /> <br /> Consider the following conditions:<br /> <br /> > Pressure Alt: Sea Level<br /> > Shade Temp: 30oC<br /> > Take-off Weight: MTOW<br /> > Surface: Asphalt<br /> > Slope: Level<br /> > Wind: 5kt headwind<br /> <br /> : 750m; 600m; 790m; 690m

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE 5<br /> <br /> Consider the following conditions:<br /> <br /> > Pressure Alt: 3000ft<br /> > Shade Temp: 9oC<br /> > Take-off weight: 950kg<br /> > Runway: 14<br /> > Surface: Long, dry grass<br /> > Slope: 1% down to the NW<br /> > Wind: 140oM at 5kt<br /> <br /> : 900m; 720

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE 5<br /> <br /> Consider the following conditions:<br /> <br /> > Pressure Alt: 5500 ft<br /> > Shade Temp: 0oC<br /> > Weight: 1060 kg<br /> > Runway: 680m short dry grass<br /> > Slope: 1% down<br /> > Wind: Light and variable<br /> <br /> : Yes, but not if the runway h

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE 5<br /> <br /> Consider the following conditions:<br /> <br /> > Pressure Altitude: 1000 ft<br /> > Shade Temp: 10oC<br /> > TODA: 750m<br /> > Surface: Short dry grass<br /> > Slope: Level<br /> > Wind: 5kt headwind<br /> Using the Type 1 take-off charts, the grea

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE 5<br /> <br /> Consider the following conditions:<br /> <br /> > Pressure Alt: Sea Level<br /> > Shade Temp: 30oC<br /> > Take-off Weight: MTOW<br /> > Surface: Asphalt<br /> > Slope: Level<br /> > Wind: 5kt headwind<br /> What is the required takeoff distance: ___

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK TAKE-OFF CHART PAGE 5<br /> <br /> Consider the following conditions:<br /> <br /> > Pressure Alt: 3000ft<br /> > Shade Temp: 9oC<br /> > Take-off weight: 950kg<br /> > Runway: 14<br /> > Surface: Long, dry grass<br /> > Slope: 1% down to the NW<br /> > Wind: 140oM at 5kt<br /> What is the

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK (Page 11 to 12) <br /> <br /> A Bravo type aircraft has a BEW of 1320lbs and a moment index of 110 index units. If the pilot and co-pilot have a combined weight 425lbs, a passenger in row 2 weighs 225lbs and they wish to carry 25lbs of

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK (Page 1 to 12) A Bravo type aircraft has an all up weight of 2100lbs and a Moment Index of 196. There is 100lbs of baggage in the<br /> <br /> baggage compartment. The minimum amount of baggage that must be removed from the baggage

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK (Page 11 to 12) <br /> <br /> A Bravo type aircraft has a BEW of 1320lbs and a moment index of 110 index units. If the pilot and co-pilot have a combined weight 425lbs, a passenger in row 2 weighs 225lbs and they wish to carry 25lbs of

immediatefeedback

Refer to RPL-PPL-CPL WORKBOOK (Page 1 to 12) A Bravo type aircraft has an all up weight of 2100lbs and a Moment Index of 196. There is 100lbs of baggage in the<br /> <br /> baggage compartment. <br /> <br /> The minimum amount of baggage that must be removed from the baggag

immediatefeedback

When a left twisting movement is applied to the control column, during flight: the right aileron rises and the aircraft rolls to the right; the left aileron rises and the aircraft rolls to the left; the right aileron rises and the aircraft rolls to the le

immediatefeedback

Which is the most appropriate recovery action if an aircraft is allowed to enter a spiral dive?: apply opposite aileron to level the wings; pull back firmly on the control column; apply full rudder against the direction of turn; apply aileron in the direc

immediatefeedback

The form of drag that predominates at low airspeed is known as: induced drag; pressure drag; parasite drag; total drag

immediatefeedback

Total drag is the combined effect of parasite drag and induced drag is known as total drag. The least total drag occurs: near the middle of the speed range, when both induced drag and parasite drag are fairly low; near the middle of the speed range, when

immediatefeedback

The direction of the relative airfow is always: opposite to the direction of the aircraft’s motion and equal to the true air speed; opposite to the direction of the aircraft’s motion and faster than the true air speed; in the same direction of the aircraf

immediatefeedback

The magnitude of the total aerodynamic reaction on an aerofoil depends upon: the camber of the aerofoil only; both the angle of attack of the aerofoil and the speed of the relative airflow; the speed of the relative airflow only; the angle of attack of th

immediatefeedback

For any given airspeed, the stalling angle of attack is the angle of attack at which: lift reaches its minimum value; drag reaches its maximum value; drag reaches its minimum value; lift reaches its maximum value

immediatefeedback

If an aircraft is taxiing on level ground with a strong cross-wind from the left, the pilot would notice a tendency to: roll to the left; roll to the right; yaw to the left; yaw to the right

immediatefeedback

The application of full flap during a power-off glide would permit: the aircraft to glide at a higher nose attitude; the current flight path to be maintained at a lower speed; the extra lift to produce a flatter approach path; the approach path to be stee

immediatefeedback

Which of these figures correctly shows the relationship between the tailplane, elevator and trim tab for an aircraft that has been trimmed to fly level at a low speed?: [a]; [c]; [b]; [d]

immediatefeedback

The purpose of aerodynamic balancing of rudders or elevators is to: prevent the rudder or elevator from fluttering; improver controllability at low speeds; lighten the control force required to operate the control surface; to increase the rate at which th

immediatefeedback

If a pilot applies flap during a power-off glide, the effect on glide performance will be: less drag an an increase in gliding distance; more drag and a decrease in gliding distance; less drag and a decrease in gliding distance; more drag and an increase

immediatefeedback

Given that the recommended indicated air speed for best angle of climb in a particular aircraft is published as 60 knots. Which of the following would reduce the angle of climb?: climbing at a reduced indicated air speed; a reduction in take-off weight; a

immediatefeedback

The best angle of climb speed is called Vx and the best rate of climb speed is called Vy. Assuming power is kept constant, compared with climbing at Vx, climbing at Vy would result in: a lower nose attitude and a lower indicated airspeed; a higher nose at

immediatefeedback

Which of the following most fully describes the behaviour of an aerofoil that is operating at its stalling angle: any increase or decrease in angle of attack results in more drag; a decrease in angle of attack results in more lift; any increase or decreas

immediatefeedback

If the pilot observes that the aircraft is slipping during a turn, an appropriate remedy would be: apply more bank in the direction of the turn; apply more rudder in the direction of the turn; apply a greater back pressure on the control column; apply les

immediatefeedback

A heavy jet aircraft has just departed from a runway you are about to use. Select the actions that would give the best chance of avoiding an encounter with the jet’s wake turbulence: aim to lift off after the jet's lift off point, maintain the best angle

immediatefeedback

What effect will an increase in bank angle during a level turn have on load factor and stalling speed?: load factor will increase and stalling speed will increase; load factor will decrease and stalling speed will increase; load factor will decrease and s

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