NEW
Font size
WorksheetsCONTACT (FINAL) FOR CT-4E ชุดที่ 2
Total questions: 40
Worksheet time: 40mins
คลื่นวิทยุความถี่ฉุกเฉิน
VHF 127.5 MHz, UHF 251.0 MHz
VHF 125.1 MHz, UHF 234.0 MHz
VHF 126.2 MHz, UHF 328.0 MHz
VHF 121.5 MHz, UHF 243.0 MHz
อากาศยาน 2 เครื่องกำลังบินเข้าหากัน ในระยะสูงเดียวกัน อากาศยานทั้งสองต้องปฏิบัติอย่างไร
เลี้ยวขวาออกจากกัน
เลี้ยวซ้ายออกจากกัน
เลี้ยวข้างไหนก็ได้
เครื่องที่เห็นก่อนลดระยะสูง
Basic empty weight (approximate) และ A.U.W. ของ บ.ฝ.16 ก คือเท่าใด
1600 lbs., 2600 lbs.
1700 lbs., 2600 lbs.
1600 lbs., 2700 lbs.
1700 lbs., 2700 lbs.
For all emergencies the glide speed will be in the range ….. to ….. KIAS. Dependent on flaps setting.
68 – 80 KIAS.
70 – 80 KIAS.
72 – 85 KIAS.
80 – 85 KIAS.
The minimum height from which a bale-out should be attempted is ….. ft.AGL. and canopy jettison procedures should be completed above ….. ft.AGL. if bale-uot is intened.
1000, 1000
1000, 1500
1500, 1000
1500, 1500
An air load start may be achieved by attaining a minimum of ……... KIAS. A minimum height loss of ……... ft. can be expected.
120 KIAS., 1500 ft.
140 KIAS., 1500 ft.
120 KIAS., 1000 ft.
140 KIAS., 1000 ft.
The rate of descent, engine off, propeller ‘windmilling’. Flaps up and ..... KIAS. Is ….. nautical miles per ………. ft. at zero wind velocity.
85 KIAS., 1.0 nm., 1,000 ft.
70 KIAS., 1.0 nm., 1,000 ft.
85 KIAS., 1.1 nm., 1,000 ft.
70 KIAS., 1.1 nm., 1,000 ft.
Which is true regarding the use of flaps during level turn?
The raising of flaps decreases the stall speed.
The lowering of flaps decreases the stall speed.
Lowering flaps will requires added rearward pressure on the yoke or stick.
Raising flaps will require added rearward pressure on the yoke or stick.
Principle purpose of flaps is to
Increase drag and decrease lift.
Increase climbing speed.
Decrease the gliding angle.
Increase drag and increase lift.
The stalling of and aero plane flying upwind as compared with flying downwind.
is the same.
is less when flying upwind.
is less when flying downwind.
Differs by an amount equal to twice the wind velocity.
Induced drag increases in level flight as:
Speed and angle of attack increase
Speed and angle of attack decrease
Speed decreases and angle of attack increases
Speed decreases and angle of attack decreases
An airplane entering ground effect will: not leaving
Higher air pressure below the wing’s surface and lower air pressure above the wing’s surface.
Require a higher angle of attack to maintain the same lift coefficient.
Experience an increase in induced drag and require more thrust.
Experience a decrease in induced drag and require more thrust.
The takeoff run an A/C in summer as compared with the takeoff run in winter will be:
Independent of the weather conditions.
Shorter.
Approximately 10% shorter due to the heavier air.
Longer because of less density air.
The angle of attack of an aerofoil is defined as the angle between.
The chord line and the longitudinal axis.
The aircraft’s nose and the natural horizon.
The chord line and the relative airflow.
The aircraft indicator and the horizontal bar on the artificial is increased.
The angle of attack at wing stall remain constant regardless of:
Dynamic pressure, but varies with weight, bank angle and pitch attitude.
Weight, dynamic pressure, bank angle, or pitch attitude.
Weight and pitch attitude, but varies with dynamic pressure and bank angle.
Bank angle and weight, but varies with dynamic pressure and pitch attitude.
How will the magnitude of the lift force vary if the angle of attack of an aerofoil is increased forwards the stalling angle?
Lift will increase.
Lift will decrease.
Lift will decrease then increase.
Lift will increase then decrease.
Propeller is sometimes called airscrew. The object of the airscrew is to:
Produce torque
Produce turning effect
Convert the thrust to be a torque
Convert the torque to be a thrust
By changing the angle of attack of a wing, the pilot can control the airplane’s:
Lift, airspeed and CG
Lift, airspeed and drag
Lift, airspeed but not drag
Lift, drag but not airspeed.
The rules of the air shall apply to:
Aircraft of all states wherever they may be.
Aircraft of all states while operating in controlled airspaces.
Aircraft of all ICAO contracting states wherever they may be.
Aircraft of all ICAO contracting states while operating in controlled airspaces.
Aircraft ‘A’ is overtaking aircraft ‘B’. Both are on the same course and cruising level.
‘A’ must alter its heading to the right and ‘B’ to the left until entirely past and clear.
‘B’ must give way to the right until traffic has past and clear.
‘B’ must alter its heading to the right and ‘A’ to the left until entirely past and clear.
‘A’ must alter its heading to the right until entirely past and clear.
The term “Flight Visibility” indicates.
The visibility at an aerodrome as reported a meteorological observer.
The visibility that a tower controller can see the aircraft in flight approaching to land.
The visibility forward from the cockpit of an aircraft in flight.
The visibility as observed on a particular runway threshold.
If an air traffic control clearance is not satisfactory to a pilot of an aircraft.
He may disregard and proceed at his own responsibility.
He may disregard and cancel his flight plan.
He may request and an amended flight plan will be issued by air traffic control unit.
He may request and an amended clearance will be issues by air traffic control unit.
The term ‘Air Traffic’ means?
All aircraft in flight.
All aircraft in flight or operating on the manoeuvring area of an aerodrome.
All aircraft flying in the vicinity of an aerodrome.
All aircraft flying in the vicinity of an aerodrome and all traffic on the manoeuvring area of an aerodrome.
The aeronautical radio of Thailand and limited provides operates and maintains the equipment for provision of
Approach control service.
Radar approach control service.
Alerting service.
Area control service.
A flight plan should be submitted prior to operating.
For and flight to be provided with air traffic control service.
All flight.
Every cross-country flight.
For international flight only.
Using of a fuel of too low an octane rating will result in
Detonation
A lean mixture
Too rich a mixture
A loss of engine power from too lean a mixture
An abnormally high engine oil temperature indication may be caused by
The oil level being too low
A defective bearing
Operating with an excessively rich mixture
The oil level being too high
What is the result of permitting an aircraft engine to idle for a long period of time while on the ground?
A hydraulic lock may develop in one or more cylinders
It may cause excessive high oil pressure
The lean mixture may cause the engine to miss or quit.
The spark plug may become fouled.
What conditions would you likely observe if you descend from a high altitude without readjusting the mixture?
The engine will immediately run rough.
Carburetor icing will cause a decrease in r.p.m.
The fuel/air mixture may become excessively lean.
The fuel/air mixture will become excessively rich.
The main advantage of a constant-speed propeller is that it
Provides more power because of higher r.p.m.
Allows you to select and maintain a desired airspeed.
Allows a much lower cruising speed than a fixed-pitch propeller.
Allows selection of the blade angle that will provide the most efficient performance.
Deviation means:
The angle between true north and magnetic north use true north as reference line.
The angle between magnetic north and compass north use magnetic north as reference line.
The angle between true north and compass north.
The angle between magnetic north and true north.
When you recover from unusual attitude without the aid of an attitude indicator, you know you have reached a level pitch attitude when the
Heading indicator stops moving.
Vertical speed indicator shows a zero rate of climb.
Turn coordinator indicator straight and level flight.
Altimeter and airspeed needles stop and reverse direction.
As you commence a descent you become aware that the pitot tube has become blocked by ice. During the descent the altimeter will
Over read
Under read
Read correct
Vary between over and under reading
You are entering Phisanulok control area for landing but unable to contact Phisanulok approach. What should you try to do first?
Continue to aerodrome and do communications failure procedures.
Divert to alternate aerodrome which has radar control.
Try to communicate by using Phisanulok tower frequency.
Stay on previous frequency and inform the provious ATC.
Fulfillment of speech transmitting that the highest possible intelligibility is incorporated in each transmission, air crew and ground personnel should maintain even rate of speech not exceeding…………….
100 words per minute.
100 words per second
1,000 words per minute.
1,000 words per second.
CRM is to improve the ….. of the pilot so as to bring about better decision making
personality traits
Attitudes
life style
family life
“Basic-T Pattern” layout of the flight instruments in the old days are consisting of;
The Attitude Indicator (AI),the airspeed indicator (ASI),the altimeter and heading indicator.
The Attitude Indicator (AI),the airspeed indicator (ASI),the altimeter and standby attitude indicator.
The Attitude Indicator (AI),the airspeed indicator (ASI),the heading and standby attitude indicator.
The Attitude Indicator (AI),the altimeter and standby attitude indicator.
Differential control is related to which system?
Rudder system.
Aileron system.
Elevator system.
Trim system.
The internal resistance of a fluid which tends to prevent it from flowing is called:
Volatility.
Flashpoint.
Acidity.
Viscosity.
The principal load bearing member in a wing is the:
Struts.
Ribs.
Spars.
Fabric
