Paper-1 CAR Rules Series I Questions
1. Instrument which has lapsed its shelf life shall be:
(a) Bench checked before use (c) Rejected from further use
(b) Overhauled before use
2. Instrument installed on aircraft has not been operated for a continuous period of six months shall be : (a)Overhauled Before use (c)Replaced with a new instrument
(b)Bench checked before use
3. Calibration and compensation of a magnetic compass shall be carried out:
(a) Every 12 months interval (c)at intervals as specified by manufacturer
(b) Every 6 months interval
4. At the time of installation of a magnetic compass, its pivot friction tolerance shall be:
(a) A maximum of two degrees (c) Within the tolerance given by the manufacturer
(b) A maximum of ten degrees
5. Where the manufacturer has not specified any periodicity for the calibration and compensation of a magnetic compass, it shall be carried out
(a) Every six months (c) Every two years/ 1000 hrs whichever is earlier
(b) Every twelve months
6. If the pivot friction tolerance of a magnetic compass is not specified by the manufacturer then it shall be taken as
(a) A maximum of two degrees (c) A maximum of twenty degrees
(b) A maximum of ten degrees
7. Aircraft instruments shall be overhauled and inspected in accordance with the requirements of
(a) CAR Series I Part 1 (c) CAR Series R Part 1
(b) CAR Series I Part 2
8. A magnetic compass fitted on aircraft shall be calibrated and compensated:
(a) At the time of initial installation (c) Both (a) & (b) are correct
(b) After heavy landing of aircraft
9. Aircraft instruments are to be stored in good condition where:
(a) Temperature is between 5° and 25°C and humidity not exceeding 70%
(b) Temperature is between 5° and 25°F and humidity 70%
(c) Temperature is between 5° and 25°C and humidity more than 70%
10. Aircraft instruments whose storage condition are not in accordance with accepted practices must be:
(a) Considered serviceable and inspected before use
(b) Considered unserviceable and overhauled before use
(c) Considered unserviceable and bench checked before use
Answers
1. (b) 2.(b) 3.(c) 4.(c) 5.(b) 6.(a) 7.(a) 8.(c) 9.(a) 10.(b)
11. The shelf life of instrument shall be reflected in the
(a) Quality Control Manual/Maintenance System Manual
(b) As in (a) & serviceability tag also
(c) As in (b) & Flight Manual also.
12. The maximum overhaul period of altimeter is:
(a) Two years (c) One year/2000 hrs whichever is earlier
(b) Two years/1000 hrs whichever is earlier
13. The maximum overhaul period of all gyro instruments shall be
(a) Two years (c) Three years/2000 hrs whichever is earlier
(b) Two years/1000 hrs whichever is earlier
14. The maximum overhaul period of Air Speed Indicator is
(a) 1000hrs/1 year whichever is earlier (c) 2000hrs/3 years whichever is earlier
(b) 2000hrs/2 years whichever is earlier
15. The routine inspection period of position indicator is:
(a) 2 years (c) bench checked every 2 years
(b) 2 years/1000hrs whichever is earlier
16. After heavy landing of an aircraft, its magnetic compass shall be:
(a) Overhauled (c) Calibrated and compensated
(b) Bench checked
17. Time pieces can be overhauled or repaired by any reputed commercial watchmaker in respect of aircraft with AUW:
(a)less than 3000kg (c)more than 3000kg
(b)less than 2000kg
18. The shelf life of instruments, other than gyro instruments shall not exceed
(a)one year (c)three years
(b) two years
19. The shelf life of gyro instruments is
(a)two years (c)two years but bearings lubricated every year
(b) one year
20. The shelf life of instruments shall be
(a)a maximum of two years (c)as per the manufacturer specified
(b)a maximum of six months
21. Radio equipment installed on aircraft registered in India shall be operated with in a license issued under :-
(a) Indian Telegraph act 1885 (c) Indian Telegraph act 1985
(b) Indian Telegraph act 1895
22. Location of ELT on an aircraft must be :-
(a) As fore as possible (c) near Wing tip
(b) As aft as possible
Answers
11. b,12.a,13.b,14.c,15.c,16.c,17.a,18.b 19.c 20.c 21.a 22.b
1. Instrument which has lapsed its shelf life shall be:
(a) Bench checked before use (c) Rejected from further use
(b) Overhauled before use
2. Instrument installed on aircraft has not been operated for a continuous period of six months shall be : (a)Overhauled Before use (c)Replaced with a new instrument
(b)Bench checked before use
3. Calibration and compensation of a magnetic compass shall be carried out:
(a) Every 12 months interval (c)at intervals as specified by manufacturer
(b) Every 6 months interval
4. At the time of installation of a magnetic compass, its pivot friction tolerance shall be:
(a) A maximum of two degrees (c) Within the tolerance given by the manufacturer
(b) A maximum of ten degrees
5. Where the manufacturer has not specified any periodicity for the calibration and compensation of a magnetic compass, it shall be carried out
(a) Every six months (c) Every two years/ 1000 hrs whichever is earlier
(b) Every twelve months
6. If the pivot friction tolerance of a magnetic compass is not specified by the manufacturer then it shall be taken as
(a) A maximum of two degrees (c) A maximum of twenty degrees
(b) A maximum of ten degrees
7. Aircraft instruments shall be overhauled and inspected in accordance with the requirements of
(a) CAR Series I Part 1 (c) CAR Series R Part 1
(b) CAR Series I Part 2
8. A magnetic compass fitted on aircraft shall be calibrated and compensated:
(a) At the time of initial installation (c) Both (a) & (b) are correct
(b) After heavy landing of aircraft
9. Aircraft instruments are to be stored in good condition where:
(a) Temperature is between 5° and 25°C and humidity not exceeding 70%
(b) Temperature is between 5° and 25°F and humidity 70%
(c) Temperature is between 5° and 25°C and humidity more than 70%
10. Aircraft instruments whose storage condition are not in accordance with accepted practices must be:
(a) Considered serviceable and inspected before use
(b) Considered unserviceable and overhauled before use
(c) Considered unserviceable and bench checked before use
Answers
1. (b) 2.(b) 3.(c) 4.(c) 5.(b) 6.(a) 7.(a) 8.(c) 9.(a) 10.(b)
11. The shelf life of instrument shall be reflected in the
(a) Quality Control Manual/Maintenance System Manual
(b) As in (a) & serviceability tag also
(c) As in (b) & Flight Manual also.
12. The maximum overhaul period of altimeter is:
(a) Two years (c) One year/2000 hrs whichever is earlier
(b) Two years/1000 hrs whichever is earlier
13. The maximum overhaul period of all gyro instruments shall be
(a) Two years (c) Three years/2000 hrs whichever is earlier
(b) Two years/1000 hrs whichever is earlier
14. The maximum overhaul period of Air Speed Indicator is
(a) 1000hrs/1 year whichever is earlier (c) 2000hrs/3 years whichever is earlier
(b) 2000hrs/2 years whichever is earlier
15. The routine inspection period of position indicator is:
(a) 2 years (c) bench checked every 2 years
(b) 2 years/1000hrs whichever is earlier
16. After heavy landing of an aircraft, its magnetic compass shall be:
(a) Overhauled (c) Calibrated and compensated
(b) Bench checked
17. Time pieces can be overhauled or repaired by any reputed commercial watchmaker in respect of aircraft with AUW:
(a)less than 3000kg (c)more than 3000kg
(b)less than 2000kg
18. The shelf life of instruments, other than gyro instruments shall not exceed
(a)one year (c)three years
(b) two years
19. The shelf life of gyro instruments is
(a)two years (c)two years but bearings lubricated every year
(b) one year
20. The shelf life of instruments shall be
(a)a maximum of two years (c)as per the manufacturer specified
(b)a maximum of six months
21. Radio equipment installed on aircraft registered in India shall be operated with in a license issued under :-
(a) Indian Telegraph act 1885 (c) Indian Telegraph act 1985
(b) Indian Telegraph act 1895
22. Location of ELT on an aircraft must be :-
(a) As fore as possible (c) near Wing tip
(b) As aft as possible
Answers
11. b,12.a,13.b,14.c,15.c,16.c,17.a,18.b 19.c 20.c 21.a 22.b
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