Spice jet Recruitment (2011)
Join Date: Aug 2010
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the exam that spice jet conducts is easier
Join Date: Jun 2011
Location: India
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Caution: Think before you waste your money.
Another written planned on 16 June, 2011.
Only randomly selected people are being called for the exams; But all are welcome to pay the DD of Rs.20000/-.
Please use your jacks to make it to the exam and have enough money to keep bribing them at every stage.
Please follow the link:
http://www.pprune.org/south-asia-far...ml#post6501542
Only randomly selected people are being called for the exams; But all are welcome to pay the DD of Rs.20000/-. Please use your jacks to make it to the exam and have enough money to keep bribing them at every stage.Please follow the link:
http://www.pprune.org/south-asia-far...ml#post6501542
Join Date: May 2011
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Exam on 4th march
Hi, thanks for posting the questions. Well I heard that the exam was Specific for the TYpe rated Pilots on Boeing 737-NG, and the question were supposed to be asked from the FCOMs and FCTM, n QRH and some Performance. But the questions u posted were more towards CPL level.
Im a bit confused, could u clarify that pls.
Im a bit confused, could u clarify that pls.
Join Date: Jun 2011
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Questions open for discussion
The exam was way tougher from last time, the questions were a bit weird though. My guess would be around 350 people appeared cause i know a guy with roll number 325.
As for the questions, let me see-
There were some really simple questions on triangles
Then some questions on relative velocity (2 cars starting from A to B)
Some questions on conversions-
41000ft in Km
15m in feet
This all was the easy part
Lot of questions from technical and especially electrical system-
If we have to convert 28V DC to 200/115AC then what should we use
There were some questions on HP cock and LP cock????
One question from triple spool engine
Procedure for shutting down turbine engine- HP first or LP first
When thrust is reversed on Turboprop which gasses are reversed, Hot or cold
Where is fuel flow measured in a jet engine (with diagram)
Climb gradient for 2 segment
Static is blocked, what will altimeter read while descending/ascending
CG is forward of range, what will be effect on range and SFC
Metar and TAF readings
The regs part was weird though-
Can you shoot sids and stars with gps in india
What is the RNP for some GNSS approach
WHen does the air hostess need to fasten her seat belt
Whose rules does India follow- Europe, Australia, USA or ICAO Annex Sumthin
An airway is marked FL80, what does it mean?
As for the questions, let me see-
There were some really simple questions on triangles
Then some questions on relative velocity (2 cars starting from A to B)
Some questions on conversions-
41000ft in Km
15m in feet
This all was the easy part
Lot of questions from technical and especially electrical system-
If we have to convert 28V DC to 200/115AC then what should we use
There were some questions on HP cock and LP cock????
One question from triple spool engine
Procedure for shutting down turbine engine- HP first or LP first
When thrust is reversed on Turboprop which gasses are reversed, Hot or cold
Where is fuel flow measured in a jet engine (with diagram)
Climb gradient for 2 segment
Static is blocked, what will altimeter read while descending/ascending
CG is forward of range, what will be effect on range and SFC
Metar and TAF readings
The regs part was weird though-
Can you shoot sids and stars with gps in india
What is the RNP for some GNSS approach
WHen does the air hostess need to fasten her seat belt
Whose rules does India follow- Europe, Australia, USA or ICAO Annex Sumthin
An airway is marked FL80, what does it mean?
Join Date: Aug 2010
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For a given aerofoil, the AOA which results in a stall:
(a) remains constant regardless of bank, load or TAS
(b) varies directly with the degree of bank
(c) varies with the speed of airflow around aerofoil
The stall speed of an aircraft will increase with:
(a) decrease in the load factor
(b) increase in the pitch attitude for straight and level
(c) increase in the all up weight of the aircraft
The three axis of an aircraft intersect at the:
(a) centre of pressure
(b) centre of gravity
(c) midpoint of the datum line
When approaching the stall, the separation point (moves Forward)
(a) always stays in the same position
(b) moves rearward
(c) moves towards the transition point
The primary function of the rudder, while entering a turn from straight-and-level flight, is to:
(a) overcome yaw caused by lowered aileron on higher wing
(b) overcome yaw caused by lowered aileron on lower wing
(c) overcome yaw caused by raised aileron on higher wing
An aircraft is in a state of equilibrium in:
(a) a steady rate 1 turn
(b) in a steady climb
(c) during take off
Adverse aileron yaw is reduced by the use of:
(a) vortex generators
(b) frise type ailerons
(c) boundary layer fences
Flying near high ground or mountains with winds in excess of 15km, you can expect strong turbulence and down draughts. What would you do to avoid damaging the aircraft and / or loosing control?
(a) maintain your heading and speed
(b) slow down to manoeuvring speed
(c) slow down to manoeuvring speed and fly upwind of ridge
On a cold, clear, humid night with a light wind, radiation fog will form. What might form when the wind picks up to 15kts?
(a) dew
(b) frost
(c) stratus
Which clouds are the least likely to produce airframe icing?
(a) middle cloud
(b) high cloud
(c) vertical development cloud (CB)
(a) remains constant regardless of bank, load or TAS
(b) varies directly with the degree of bank
(c) varies with the speed of airflow around aerofoil
The stall speed of an aircraft will increase with:
(a) decrease in the load factor
(b) increase in the pitch attitude for straight and level
(c) increase in the all up weight of the aircraft
The three axis of an aircraft intersect at the:
(a) centre of pressure
(b) centre of gravity
(c) midpoint of the datum line
When approaching the stall, the separation point (moves Forward)
(a) always stays in the same position
(b) moves rearward
(c) moves towards the transition point
The primary function of the rudder, while entering a turn from straight-and-level flight, is to:
(a) overcome yaw caused by lowered aileron on higher wing
(b) overcome yaw caused by lowered aileron on lower wing
(c) overcome yaw caused by raised aileron on higher wing
An aircraft is in a state of equilibrium in:
(a) a steady rate 1 turn
(b) in a steady climb
(c) during take off
Adverse aileron yaw is reduced by the use of:
(a) vortex generators
(b) frise type ailerons
(c) boundary layer fences
Flying near high ground or mountains with winds in excess of 15km, you can expect strong turbulence and down draughts. What would you do to avoid damaging the aircraft and / or loosing control?
(a) maintain your heading and speed
(b) slow down to manoeuvring speed
(c) slow down to manoeuvring speed and fly upwind of ridge
On a cold, clear, humid night with a light wind, radiation fog will form. What might form when the wind picks up to 15kts?
(a) dew
(b) frost
(c) stratus
Which clouds are the least likely to produce airframe icing?
(a) middle cloud
(b) high cloud
(c) vertical development cloud (CB)
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just confused with the last one , even high clouds have very slim chances of airframe icing as they are made of ice crystals themselves and on the other hand in vertically developed clouds we are bound to find more of heavy ice ( as in hail stones etc ) , so which option should be the one closest to the correct answer ?
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The primary function of the rudder, while entering a turn from straight-and-level flight, is to:
(a) overcome yaw caused by lowered aileron on higher wing
(b) overcome yaw caused by lowered aileron on lower wing
(c) overcome yaw caused by raised aileron on higher wing
correct answer is (a)....the aileron is lowered on the up-going (higher) wing
(a) overcome yaw caused by lowered aileron on higher wing
(b) overcome yaw caused by lowered aileron on lower wing
(c) overcome yaw caused by raised aileron on higher wing
correct answer is (a)....the aileron is lowered on the up-going (higher) wing