\n ","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"Head wind 10 crosswind 12 kt","comment":{"@type":"Comment","text":"Head wind 10 crosswind 12 kt"}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"Head wind 15 kt crosswind 15 kt","comment":{"@type":"Comment","text":"Head wind 15 kt crosswind 15 kt"}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"Head wind 20 kt crosswind 20 kt","comment":{"@type":"Comment","text":"Head wind 20 kt crosswind 20 kt"}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"Head wind 19 kt crosswind 23 kt","comment":{"@type":"Comment","text":"Head wind 19 kt crosswind 23 kt"}}],"acceptedAnswer":[{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"Head wind 19 kt crosswind 23 kt","comment":{"@type":"Comment","text":"."},"answerExplanation":{"@type":"Comment","text":"."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class B - Use Of Data","text":"Departing SID requires 6.1% gradient with T/O flaps, speed 130 kts to 1800ft and thereafter a 5% gradient to FL80 clean at 230 kts. What is the ROC required to 1800ft?","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"600 fpm to 1800 ft with non-standard speed change altitude.","comment":{"@type":"Comment","text":"600 fpm to 1800 ft with non-standard speed change altitude."}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"1150 fpm with standard speed change altitude","comment":{"@type":"Comment","text":"1150 fpm with standard speed change altitude"}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"800 fpm to 1800 ft with non-standard speed change altitude.","comment":{"@type":"Comment","text":"800 fpm to 1800 ft with non-standard speed change altitude."}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"1250 fpm with standard speed change altitude.","comment":{"@type":"Comment","text":"1250 fpm with standard speed change altitude."}}],"acceptedAnswer":[{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"800 fpm to 1800 ft with non-standard speed change altitude.","comment":{"@type":"Comment","text":"The Rate of Climb (ROC) required to climb to 1800ft is 800 fpm with a non-standard speed change altitude when departing on the Standard Instrument Departure (SID) that requires a 6.1% gradient with takeoff flaps and a speed of 130 kts."},"answerExplanation":{"@type":"Comment","text":"The Rate of Climb (ROC) required to climb to 1800ft is 800 fpm with a non-standard speed change altitude when departing on the Standard Instrument Departure (SID) that requires a 6.1% gradient with takeoff flaps and a speed of 130 kts."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class A - Use Of Data","text":"Refer to the annex or CAP 698 Figure 4.5. Given the following information what is the Climb Limited Take-Off Mass?OAT + 35°CPressure altitude 2000 ftFlaps 5°A/C packs OFFAnti-icing OFFPMC OFF \n ","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"52800 kg","comment":{"@type":"Comment","text":"52800 kg"}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"53700 kg","comment":{"@type":"Comment","text":"53700 kg"}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"57900 kg","comment":{"@type":"Comment","text":"57900 kg"}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"57000 kg","comment":{"@type":"Comment","text":"57000 kg"}}],"acceptedAnswer":[{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"57900 kg","comment":{"@type":"Comment","text":"."},"answerExplanation":{"@type":"Comment","text":"."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class A - Theory","text":"With regard to the FMC and reduced thrust take-off’s which of the following statements is correct.","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"Reduced thrust cannot be used on a contaminated runway.","comment":{"@type":"Comment","text":"Reduced thrust cannot be used on a contaminated runway."}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"Reduced thrust is not recommended at very low temperatures (OAT).","comment":{"@type":"Comment","text":"Reduced thrust is not recommended at very low temperatures (OAT)."}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"Reduced thrust can lower VMCG and VMCA","comment":{"@type":"Comment","text":"Reduced thrust can lower VMCG and VMCA"}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"Reduced thrust cannot be used on a wet runway","comment":{"@type":"Comment","text":"Reduced thrust cannot be used on a wet runway"}}],"acceptedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"Reduced thrust cannot be used on a contaminated runway.","comment":{"@type":"Comment","text":"Reduced thrust take-off cannot be used on a contaminated runway."},"answerExplanation":{"@type":"Comment","text":"Reduced thrust take-off cannot be used on a contaminated runway."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class B - Theory","text":"A single engine aircraft has a gross glide gradient of 8%. Determine the net glide distance from 10 000 ft to 2 000 ft:","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"15.5 NM","comment":{"@type":"Comment","text":"15.5 NM"}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"16.5 NM","comment":{"@type":"Comment","text":"16.5 NM"}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"17 NM","comment":{"@type":"Comment","text":"17 NM"}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"94 120 NM","comment":{"@type":"Comment","text":"94 120 NM"}}],"acceptedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"15.5 NM","comment":{"@type":"Comment","text":"The net glide distance can be calculated by multiplying the gross glide gradient (8%) by the difference in altitude (8000 ft), and then dividing by 100 to convert it to nautical miles. Therefore, the net glide distance from 10 000 ft to 2 000 ft is 15.5 NM."},"answerExplanation":{"@type":"Comment","text":"The net glide distance can be calculated by multiplying the gross glide gradient (8%) by the difference in altitude (8000 ft), and then dividing by 100 to convert it to nautical miles. Therefore, the net glide distance from 10 000 ft to 2 000 ft is 15.5 NM."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class B - Use Of Data","text":"Please refer to the annex or to CAP 698, Figure 3.7. What is the time required by a multi-engined piston aeroplane to climb 2400 ft? Assume that the rate of climb is constant throughout the climb and equals the rate of climb at 6000 ft pressure altitude. Use the following data:2 engines operating at maximum continuous power,Gear retracted,Pressure altitude: 6000 ft,OAT: +17° C,Mass: 4000 lb. \n ","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"8 minutes 0 seconds","comment":{"@type":"Comment","text":"8 minutes 0 seconds"}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"3 minutes 55 seconds","comment":{"@type":"Comment","text":"3 minutes 55 seconds"}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"1 minute 33 seconds","comment":{"@type":"Comment","text":"1 minute 33 seconds"}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"1 minute 55 seconds","comment":{"@type":"Comment","text":"1 minute 55 seconds"}}],"acceptedAnswer":[{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"1 minute 33 seconds","comment":{"@type":"Comment","text":"."},"answerExplanation":{"@type":"Comment","text":"."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class A - Use Of Data","text":"Refer to figure 032-62.Given: Airport elevation:\n \n1 998 ft\nTemperature (OAT):\n+38 ⁰C\nTailwind:\n8 kt\nTyres:\n \n225 mph\nFlaps:\n5⁰\nAircraft:\nmedium range jet\nPower management computer (PMC):\nON\nDetermine the tyre speed limited take-off mass for a departure from Madrid, Spain:\n\n ","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"79 100 kg","comment":{"@type":"Comment","text":"79 100 kg"}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"78 850 kg","comment":{"@type":"Comment","text":"78 850 kg"}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"84 300 kg","comment":{"@type":"Comment","text":"84 300 kg"}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"73 900 kg","comment":{"@type":"Comment","text":"73 900 kg"}}],"acceptedAnswer":[{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"73 900 kg","comment":{"@type":"Comment","text":"."},"answerExplanation":{"@type":"Comment","text":"."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class A - Theory","text":"Under which conditions would VMC be lowest?","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"Low temperatures, low pressure altitudes, low humidity.","comment":{"@type":"Comment","text":"Low temperatures, low pressure altitudes, low humidity."}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"Low temperatures, high pressure altitudes, low humidity.","comment":{"@type":"Comment","text":"Low temperatures, high pressure altitudes, low humidity."}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"High temperatures, high pressure altitudes, high humidity.","comment":{"@type":"Comment","text":"High temperatures, high pressure altitudes, high humidity."}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"High temperatures, low pressure altitudes, high humidity.","comment":{"@type":"Comment","text":"High temperatures, low pressure altitudes, high humidity."}}],"acceptedAnswer":[{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"High temperatures, high pressure altitudes, high humidity.","comment":{"@type":"Comment","text":"VMC (Minimum Control Speed) would be lowest under conditions of high temperatures, high pressure altitudes, and high humidity."},"answerExplanation":{"@type":"Comment","text":"VMC (Minimum Control Speed) would be lowest under conditions of high temperatures, high pressure altitudes, and high humidity."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class B - Theory","text":"Which option describes, for a Class B performance category single engine piston aeroplane, a restriction on determining the take-off speed VR?","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"VR must be equal to or greater than VS and V2 must be equal to or greater than 1.3 x VSO.","comment":{"@type":"Comment","text":"VR must be equal to or greater than VS and V2 must be equal to or greater than 1.3 x VSO."}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"VR and V2 both must be equal to or greater than VS.","comment":{"@type":"Comment","text":"VR and V2 both must be equal to or greater than VS."}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"VR must be equal to or greater than VS1.","comment":{"@type":"Comment","text":"VR must be equal to or greater than VS1."}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"VR must be equal to or greater than VSO.","comment":{"@type":"Comment","text":"VR must be equal to or greater than VSO."}}],"acceptedAnswer":[{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"VR must be equal to or greater than VS1.","comment":{"@type":"Comment","text":"VR must be equal to or greater than VS1."},"answerExplanation":{"@type":"Comment","text":"VR must be equal to or greater than VS1."}}]},{"@type":"Question","eduQuestionType":"Multiple choice","learningResourceType":"Practice problem","name":"Performance Class B - Use Of Data","text":"Refer to figure or CAP697 file 2.1. Given the following information, what is the required fuel to climb?\nAirport Pressure Altitude: 4000 ft\nAirport OAT: +10°C\nClimb to: FL100\nOAT at FL100: -5°C T\nTake-Off Mass: 3400 lb\nGear: up\n\n ","comment":{"@type":"Comment","text":""},"encodingFormat":"text/html","suggestedAnswer":[{"@type":"Answer","position":0,"encodingFormat":"text/html","text":"4.2 gal","comment":{"@type":"Comment","text":"4.2 gal"}},{"@type":"Answer","position":1,"encodingFormat":"text/html","text":"16 gal","comment":{"@type":"Comment","text":"16 gal"}},{"@type":"Answer","position":2,"encodingFormat":"text/html","text":"8.0 gal","comment":{"@type":"Comment","text":"8.0 gal"}},{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"2.8 gal","comment":{"@type":"Comment","text":"2.8 gal"}}],"acceptedAnswer":[{"@type":"Answer","position":3,"encodingFormat":"text/html","text":"2.8 gal","comment":{"@type":"Comment","text":"."},"answerExplanation":{"@type":"Comment","text":"."}}]}]},{"@context":"https://schema.org/","@type":"AggregateRating","itemReviewed":{"@type":"Course","name":"IN CPL (H) Technical Specific Practice Exam","description":"CPL (H) Technical Specific Practice Exam - Quiz: 422 questions with explanations and solutions, also available in PDF","provider":{"@type":"Organization","name":"Easy Quizzz","sameAs":"https://www.easy-quizzz.com"},"offers":[{"@type":"Offer","category":"CPL - Commercial Pilot License Test for Helicopters","priceCurrency":"INR","price":0}],"about":["Performance Class A - Use Of Data","Performance Class A - Theory","Performance Class B - Theory","Performance Class B - Use Of Data"],"hasCourseInstance":[{"@type":"CourseInstance","courseMode":"Online","courseWorkload":"PT20M"}]},"ratingCount":209,"ratingValue":4.6,"bestRating":5,"worstRating":0}]}
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Question 1/101/10
Performance Class B - Theory
Performance Class B - Theory
Performance Class B - Theory
Refer to figure or CAP698 file 4.1.
Calculate the relative direction of the wind to the runway. i.e. (wind direction - runway direction) or (runway direction - wind direction).
Example: W/V 330/30
Runway 0
Wind angle = 50°
Select the answer:Select the answer
1 correct answer
A.
Head wind 10 crosswind 12 kt
B.
Head wind 15 kt crosswind 15 kt
C.
Head wind 20 kt crosswind 20 kt
D.
Head wind 19 kt crosswind 23 kt
.
Right Answer: D
Quiz
Question 2/102/10
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Departing SID requires 6.1% gradient with T/O flaps, speed 130 kts to 1800ft and thereafter a 5% gradient to FL80 clean at 230 kts. What is the ROC required to 1800ft?
Select the answer:Select the answer
1 correct answer
A.
600 fpm to 1800 ft with non-standard speed change altitude.
B.
1150 fpm with standard speed change altitude
C.
800 fpm to 1800 ft with non-standard speed change altitude.
D.
1250 fpm with standard speed change altitude.
The Rate of Climb (ROC) required to climb to 1800ft is 800 fpm with a non-standard speed change altitude when departing on the Standard Instrument Departure (SID) that requires a 6.1% gradient with takeoff flaps and a speed of 130 kts.
Right Answer: C
Quiz
Question 3/103/10
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Refer to the annex or CAP 698 Figure 4.5. Given the following information what is the Climb Limited Take-Off Mass?OAT + 35°CPressure altitude 2000 ftFlaps 5°A/C packs OFFAnti-icing OFFPMC OFF
Select the answer:Select the answer
1 correct answer
A.
52800 kg
B.
53700 kg
C.
57900 kg
D.
57000 kg
.
Right Answer: C
Quiz
Question 4/104/10
Performance Class A - Theory
Performance Class A - Theory
Performance Class A - Theory
With regard to the FMC and reduced thrust take-off’s which of the following statements is correct.
Select the answer:Select the answer
1 correct answer
A.
Reduced thrust cannot be used on a contaminated
runway.
B.
Reduced thrust is not recommended at very low
temperatures (OAT).
C.
Reduced thrust can lower VMCG and VMCA
D.
Reduced thrust cannot be used on a wet runway
Reduced thrust take-off cannot be used on a contaminated runway.
Right Answer: A
Quiz
Question 5/105/10
Performance Class B - Theory
Performance Class B - Theory
Performance Class B - Theory
A single engine aircraft has a gross glide gradient of 8%. Determine the net glide distance from 10 000 ft to 2 000 ft:
Select the answer:Select the answer
1 correct answer
A.
15.5 NM
B.
16.5 NM
C.
17 NM
D.
94 120 NM
The net glide distance can be calculated by multiplying the gross glide gradient (8%) by the difference in altitude (8000 ft), and then dividing by 100 to convert it to nautical miles. Therefore, the net glide distance from 10 000 ft to 2 000 ft is 15.5 NM.
Right Answer: A
Quiz
Question 6/106/10
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Please refer to the annex or to CAP 698, Figure 3.7. What is the time required by a multi-engined piston aeroplane to climb 2400 ft? Assume that the rate of climb is constant throughout the climb and equals the rate of climb at 6000 ft pressure altitude. Use the following data:2 engines operating at maximum continuous power,Gear retracted,Pressure altitude: 6000 ft,OAT: +17° C,Mass: 4000 lb.
Select the answer:Select the answer
1 correct answer
A.
8 minutes 0 seconds
B.
3 minutes 55 seconds
C.
1 minute 33 seconds
D.
1 minute 55 seconds
.
Right Answer: C
Quiz
Question 7/107/10
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Refer to figure 032-62.Given:
Airport elevation:
1 998 ft
Temperature (OAT):
+38 ⁰C
Tailwind:
8 kt
Tyres:
225 mph
Flaps:
5⁰
Aircraft:
medium range jet
Power management computer (PMC):
ON
Determine the tyre speed limited take-off mass for a departure from Madrid, Spain:
Low temperatures, high pressure altitudes, low humidity.
C.
High temperatures, high pressure altitudes, high humidity.
D.
High temperatures, low pressure altitudes, high humidity.
VMC (Minimum Control Speed) would be lowest under conditions of high temperatures, high pressure altitudes, and high humidity.
Right Answer: C
Quiz
Question 9/109/10
Performance Class B - Theory
Performance Class B - Theory
Performance Class B - Theory
Which option describes, for a Class B performance category single engine piston aeroplane, a restriction on determining the take-off speed VR?
Select the answer:Select the answer
1 correct answer
A.
VR must be equal to or greater than VS and V2 must be equal to or greater than 1.3 x VSO.
B.
VR and V2 both must be equal to or greater than VS.
C.
VR must be equal to or greater than VS1.
D.
VR must be equal to or greater than VSO.
Right Answer: C
Quiz
Question 10/1010/10
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Refer to figure or CAP697 file 2.1.
Given the following information, what is the required fuel to climb?
Airport Pressure Altitude: 4000 ft
Airport OAT: +10°C
Climb to: FL100
OAT at FL100: -5°C T
Take-Off Mass: 3400 lb
Gear: up
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The CPL (H) Technical Specific Practice Exam Simulator Practice Tests are part of the CPL - Commercial Pilot License Test for Helicopters Database and are the best way to prepare for any CPL (H) Technical Specific Practice Exam exam. The CPL (H) Technical Specific Practice Exam practice tests consist of 422 questions divided by 4 topics and are written by experts to help you and prepare you to pass the exam on the first attempt. The CPL (H) Technical Specific Practice Exam database includes questions from previous and other exams, which means you will be able to practice simulating past and future questions. Preparation with CPL (H) Technical Specific Practice Exam Simulator will also give you an idea of the time it will take to complete each section of the CPL (H) Technical Specific Practice Exam practice test . It is important to note that the CPL (H) Technical Specific Practice Exam Simulator does not replace the classic CPL (H) Technical Specific Practice Exam study guides; however, the Simulator provides valuable insights into what to expect and how much work needs to be done to prepare for the CPL (H) Technical Specific Practice Exam exam.
CPL (H) Technical Specific Practice Exam Practice test therefore represents an excellent tool to prepare for the actual exam together with our CPL - Commercial Pilot License Test for Helicopters practice test . Our CPL (H) Technical Specific Practice Exam Simulator will help you assess your level of preparation and understand your strengths and weaknesses. Below you can read all the quizzes you will find in our CPL (H) Technical Specific Practice Exam Simulator and how our unique CPL (H) Technical Specific Practice Exam Database made up of real questions:
Info quiz:
Quiz name:CPL (H) Technical Specific Practice Exam
Total number of questions:422
Number of questions for the test:100
Pass score:90%
Number of topics:4 Topics
Study topics:Number of questions:
Performance Class A - Theory:222 Questions
Performance Class A - Use Of Data:55 Questions
Performance Class B - Theory:102 Questions
Performance Class B - Use Of Data:43 Questions
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