M-11 Aeroplane Aerodynamics, Structures and Systems
Exam no 1
1. A lead-acid battery is considered to be fully charged when the
a) SG reaches 1.180
* b) cells begin to gas freely
c) SG and voltage remain constant for specified period
2. The preferred method of battery charging a Ni-Cad battery is constant
a) voltage
* b) current
c) power
3. Wing spoilers, when used asymmetrically, are associated with
a) elevators
b) rudder
* c) ailerons
4. In an aircraft flying control system employing servo-tabs, the installation of external ground locks to the main control surface
a) is unnecessary since the system is irreversible and therefore the control surface cannot be displaced by the wind
* b) would not prevent movement of the control column
c) would also prevent movement of the control column
5. Air above Mach 0.7 is
* a) Compressible
b) incompressible
c) compressible only when above the speed of sound
6. Supersonic air passing through a divergent duct causes the
a) pressure to increase, velocity to increase
* b) pressure to decrease, velocity to increase
c) pressure to increase, velocity to decrease
7. An aircraft flying below the tropo-pause descends at a constant True Airspeed, its Mach. No. will
a) increase
* b) decrease
c) not change
8. Spongy brakes are usually a result of
* a) air in the system
b) internal leakage
c) external leakage
9. Over inflated tyres may cause damage to the
a) wheel hub
* b) wheel flange
c) brake drum
10. Blow-out panels are fitted to floors of pressurised aircraft to
a) provide access for pressurising the aircraft
b) relieve pressure if the maximum differential is exceeded
* c) provide venting should a differential pressure build up across the floor
,now did you do'
Question : I The correct answer Is b Pallett Aircraft Electrical Systems 3rd Edition Page 23.
Question :2 The correct answer Is b CAIPs EEL/I - 5 Para 4.1
Question :3 The correct answer is c Pallett Automatic Flight Control 4th Edition Page 51. Jeppesen A&P Technician Airframe
Textbook Page 1-1.2
Question :4 The correct answer Is a Aircraft Flight Barnard and Philpot, Second Edition Page 253 (first line)
Question :5 The correct answer Is b Aircraft Flight Barnard and Philpot, Second Edition Pagel23. Mechanics of Flight AC Kermode
10th Edition Page 355
Question :6 The correct answer Is b Speed of sound INCREASES with DECREASING altitude, so mach number will decrease.
Mechanics of Flight AC Kermode 10th Edition Page 340
Question ;7 The correct answer Is b Pallett Aircraft Instruments and Integrated Systems 2nd Edition Page 111
Question :8 The correct answer Is a CAAIPs 5-8 Jeppesen A&P Technician Airframe Textbook Page 9-31
Question :9 The correct answer Is b Jeppesen A&P Technician Airframe Textbook Page 1-32
Question :10 The correct answer Is c Example DCIO Cargo door disaster. Cargo compartment depressurised, cabin pressure caused
floor to collapse. Blow-out panels made compulsory thereafter
,Exam no 2
1. If an aircraft is yawing to the left, where would you position the trim tab on the rudder?
* a) To the left
b) To the right
c) To the centre
2. If an aircraft is flying with a left wing low, where would you move the left aileron trim tab?
* a) Up
b) Down
c) Moving the aileron trim tab will not correct the situation
3. When a Leading edge flap is fully extended, what is the slot in the wing for?
a) To increase the lift
* b) To re-energise the boundary layer
c) To allow the flap to retract into it when it retracts
4. A purpose of a cut-out in a hydraulic system
a) is to limitless of fluid in the event of pipe fracture
b) is to prevent creep in jack operated services which have several selected positions
* c) is to relieve the pump of load when the operation of services is complete and the accumulator charged with fluid
5. Hydraulic pressure can be restored by
a) the use of a pressure/heat exchanger
* b) compressing the air charge in an accumulator
c) Compressing the fluid in a Reservoir
6. Auto pilot servo brake is energised
* a) to actuate off
b) at the same time as the clutch
c) to actuate on
7. Hand held mikes are not permissible on
* a) public transport aircraft
b) public transport or aerial work
c) private aircraft only
8. Track altitude in a radio altimeter system begins at
a) 10 000ft radio alt.
* b) 2 500ft radio alt.
c) 1 000ft radio alt.
9. A fuel cross-feed valve is usually in
a) the open position
* b) the closed position
c) its last position
10. Full time yaw damper system detects
a) only low frequencies
b) All frequencies.
* c) band pass frequencies.
, now did you do'
Question : I The correct answer Is a Automatic flight control, Pallett, 4th Edition
Page 43
Question ;2 The correct answer Is a Automatic flight control, Pallett, 4th Edition Page 43
Question :3 The correct answer Is b Pallett Automatic Flight Control 2nd Edition Page 50. Jeppesen A&P Technician Airframe
Textbook Page 1-32
Question :4 The correct answer Is c CAIPs AL/3-21 5.2
Question :5 The correct answer Is b CAIPs AL/3-21 Para 7
Question :6 The correct answer Is a Pallett Aircraft Electrical Systems 3rd Edition Page 142
Question :7 The correct answer Is a ANO Article 46 Para 5
Question :8 The correct answer Is b Jeppesen Avionics Fundamentals Page 223
Question :9 The correct answer Is b Fuel cross feed valves must be closed for flight
Question :10 The correct answer Is a Pallett Automatic Flight Control 4th Edition Page 222 on.
Exam no 1
1. A lead-acid battery is considered to be fully charged when the
a) SG reaches 1.180
* b) cells begin to gas freely
c) SG and voltage remain constant for specified period
2. The preferred method of battery charging a Ni-Cad battery is constant
a) voltage
* b) current
c) power
3. Wing spoilers, when used asymmetrically, are associated with
a) elevators
b) rudder
* c) ailerons
4. In an aircraft flying control system employing servo-tabs, the installation of external ground locks to the main control surface
a) is unnecessary since the system is irreversible and therefore the control surface cannot be displaced by the wind
* b) would not prevent movement of the control column
c) would also prevent movement of the control column
5. Air above Mach 0.7 is
* a) Compressible
b) incompressible
c) compressible only when above the speed of sound
6. Supersonic air passing through a divergent duct causes the
a) pressure to increase, velocity to increase
* b) pressure to decrease, velocity to increase
c) pressure to increase, velocity to decrease
7. An aircraft flying below the tropo-pause descends at a constant True Airspeed, its Mach. No. will
a) increase
* b) decrease
c) not change
8. Spongy brakes are usually a result of
* a) air in the system
b) internal leakage
c) external leakage
9. Over inflated tyres may cause damage to the
a) wheel hub
* b) wheel flange
c) brake drum
10. Blow-out panels are fitted to floors of pressurised aircraft to
a) provide access for pressurising the aircraft
b) relieve pressure if the maximum differential is exceeded
* c) provide venting should a differential pressure build up across the floor
,now did you do'
Question : I The correct answer Is b Pallett Aircraft Electrical Systems 3rd Edition Page 23.
Question :2 The correct answer Is b CAIPs EEL/I - 5 Para 4.1
Question :3 The correct answer is c Pallett Automatic Flight Control 4th Edition Page 51. Jeppesen A&P Technician Airframe
Textbook Page 1-1.2
Question :4 The correct answer Is a Aircraft Flight Barnard and Philpot, Second Edition Page 253 (first line)
Question :5 The correct answer Is b Aircraft Flight Barnard and Philpot, Second Edition Pagel23. Mechanics of Flight AC Kermode
10th Edition Page 355
Question :6 The correct answer Is b Speed of sound INCREASES with DECREASING altitude, so mach number will decrease.
Mechanics of Flight AC Kermode 10th Edition Page 340
Question ;7 The correct answer Is b Pallett Aircraft Instruments and Integrated Systems 2nd Edition Page 111
Question :8 The correct answer Is a CAAIPs 5-8 Jeppesen A&P Technician Airframe Textbook Page 9-31
Question :9 The correct answer Is b Jeppesen A&P Technician Airframe Textbook Page 1-32
Question :10 The correct answer Is c Example DCIO Cargo door disaster. Cargo compartment depressurised, cabin pressure caused
floor to collapse. Blow-out panels made compulsory thereafter
,Exam no 2
1. If an aircraft is yawing to the left, where would you position the trim tab on the rudder?
* a) To the left
b) To the right
c) To the centre
2. If an aircraft is flying with a left wing low, where would you move the left aileron trim tab?
* a) Up
b) Down
c) Moving the aileron trim tab will not correct the situation
3. When a Leading edge flap is fully extended, what is the slot in the wing for?
a) To increase the lift
* b) To re-energise the boundary layer
c) To allow the flap to retract into it when it retracts
4. A purpose of a cut-out in a hydraulic system
a) is to limitless of fluid in the event of pipe fracture
b) is to prevent creep in jack operated services which have several selected positions
* c) is to relieve the pump of load when the operation of services is complete and the accumulator charged with fluid
5. Hydraulic pressure can be restored by
a) the use of a pressure/heat exchanger
* b) compressing the air charge in an accumulator
c) Compressing the fluid in a Reservoir
6. Auto pilot servo brake is energised
* a) to actuate off
b) at the same time as the clutch
c) to actuate on
7. Hand held mikes are not permissible on
* a) public transport aircraft
b) public transport or aerial work
c) private aircraft only
8. Track altitude in a radio altimeter system begins at
a) 10 000ft radio alt.
* b) 2 500ft radio alt.
c) 1 000ft radio alt.
9. A fuel cross-feed valve is usually in
a) the open position
* b) the closed position
c) its last position
10. Full time yaw damper system detects
a) only low frequencies
b) All frequencies.
* c) band pass frequencies.
, now did you do'
Question : I The correct answer Is a Automatic flight control, Pallett, 4th Edition
Page 43
Question ;2 The correct answer Is a Automatic flight control, Pallett, 4th Edition Page 43
Question :3 The correct answer Is b Pallett Automatic Flight Control 2nd Edition Page 50. Jeppesen A&P Technician Airframe
Textbook Page 1-32
Question :4 The correct answer Is c CAIPs AL/3-21 5.2
Question :5 The correct answer Is b CAIPs AL/3-21 Para 7
Question :6 The correct answer Is a Pallett Aircraft Electrical Systems 3rd Edition Page 142
Question :7 The correct answer Is a ANO Article 46 Para 5
Question :8 The correct answer Is b Jeppesen Avionics Fundamentals Page 223
Question :9 The correct answer Is b Fuel cross feed valves must be closed for flight
Question :10 The correct answer Is a Pallett Automatic Flight Control 4th Edition Page 222 on.
